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Format: Online-Ressource (1660 p) , illustrations, tables

Edition: Online-Ausg. Chester, Vt NewsBank, inc 2008 U.S. Congressional Serial Set, 1817-1980

Series Statement: United States congressional serial set serial set no. 12096

Note: A second-order shock-expansion method applicable to bodies of revolution near zero lift, by Clarence A Syvertson and David H. Dennis, NACA [No. 1328], p. 1127 , A summary and analysis of the low-speed longitudinal characteristics of swept wings at high Reynolds numbers, by G. Chester Furlong and James G. McHugh, NACA [No. 1339], p. 1390 , A theoretical study of the aerodynamics of slender cruciform-wing arrangements and their wakes, by John R. Spreiter and Alvin H. Sacks, NACA [No. 1296], p. 81 , Aerodynamic characteristics at high speeds of related full-scale propellers having different blade-section cambers, by Julian D. Maynard and Leland B. Salters, Jr., NACA [No. 1309], p. 651 , An analysis of the effects of aeroelasticity on static longitudinal stability and control of a swept-wing airplane, by Richard B. Skoog, NACA [No. 1298], p. 125 , An evaluation of four experimental methods for measuring mean properties of supersonic turbulent boundary layer, by George J. Nothwang, NACA [No. 1320], p. 939 , An investigation of four wings of square plan form at a Mach number of 6.9 in the Langley 11-inch hypersonic tunnel, by Charles M. McLellan, Mitchel H. Bertram, and John A. Moore, NACA [No. 1310], p. 675 , An investigation of single- and duel-rotation propellers at positive and negative thrust, and in combination with an NACA 1-Series D-Type cowling at mach numbers up to 0.84, by Robert M. Reynolds, Robert I. Sammonds, and John H. Walker, NACA [No. 1336], p. 1269 , Attention in shock tube due to unsteady-boundary-layer action, by Harold Mirels, NACA [No. 1333], p. 1227 , Average properties of compressible laminar boundary layer on flat plate with unsteady flight velocity, by Franklin K. Moore and Simon Ostrach, NACA [No. 1325], p. 1037 , Basic considerations in the combustion of hydrocarbon fuels with air, by Propulsion Chemistry Division, Lewis Flight Propulsion Laboratory, NACA [No. 1300], p. 187 , Bodies of revolution having minimum drag at high supersonic airspeeds, by A.J. Eggers, Jr., Meyer M. Resnikoff, and David H. Dennis, NACA [No. 1306], p. 555 , Cloud-droplet ingestion in engine inlets with inlet velocity ratios of 1.0 and 0.7, by Rinaldo J. Brun, NACA [No. 1317], p. 785 , Comparison of several methods for obtaining the time response of linear systems to either a unit impulse or arbitrary input from frequency-response data, by James J. Donegan and Carl R. Huss, NACA [No. 1324], p. 1023 , Correlation, evaluation, and extension of linearized theories for tire motion and wheel shimmy, by Robert F. Smiley, NACA [No. 1299], p. 137 , Determination of longitudinal stability and control characteristics from free-flight model tests with results at transonic speeds for three airplane configurations, by Clarence L. Gillis and Jess L. Mitchell, NACA [No. 1337], p. 1327 , Determination of vortex paths by series expansion technique with application to cruciform wings, by Alberta Y. Alksne, NACA [No. 1311], p. 693 , Experimental and predicted longitudinal and lateral-directional response characteristics of a large flexible 35 [degree] swept-wing airplane at an altitude of 35,000 feet, by Henry A. Cole, Jr., Stuart C. Brown, and Euclid C. Holleman, NACA [No. 1330], p. 1165 , Exploratory investigation of boundary-layer transition on a hollow cylinder at a mach number of 6.9, by Mitchel H. Bertram, NACA [No. 1313], p. 723 , Far noise-field of air jets and jet engines, by Edmund E. Callaghan and Willard D. Coles, NACA [No. 1329], p. 1147 , Flight and analytical methods for determining the coupled vibration response of tandem helicopters, by John E. Yeates, Jr., George W. Brooks, and John C. Houbolt, NACA [No. 1326], p. 1049 , Flight investigation of the effectiveness of an automatic aileron trim control device for personal airplanes, by William H. Phillips, Helmut A. Kuehnel and James B. Whitten, NACA [No. 1304], p. 505 , Induced velocities near a lifting rotor with nonuniform disk loading, by Harry H. Heyson and S. Katzoff, NACA [No. 1319], p. 850 , Influence of alloying upon grain-boundary creep, by F.N. Rhines, W.E. Bond, and M.A. Kissel, Carnegie Institute of Technology, [No. 1331], p. 1205 , Influence of hot-working conditions on high-temperature properties of a heat-resistant alloy, by John F. Ewing and J.W. Freeman, University of Michigan, [No. 1341], p. 1599 , Investigation of downwash, sidewash, and Mach number distribution behind a rectangular wing at a mach number of 2.41 by David Adamson and William B. Boatright, NACA [No. 1340], p. 1541 , Investigation of the compressive strength and creep lifetime of 2024-T3 aluminum-alloy plates at elevated temperatures, by Eldon E. Mathauser and William D. Deveikis, NACA [No. 1308], p. 637 , Investigation of the laminar aerodynamic heat-transfer characteristics of a hemisphere-cylinder in the Langley 11-inch hypersonic tunnel at Mach number 6.8, by Davis H. Crawford and William D. McCauley, NACA [No. 1323], p. 1001 , Lift and center of pressure of wing-body-tail combination at subsonic, transonic, and supersonic speeds, by William C. Pitts, Jack N. Nielsen, and George E. Kaatari, NACA [No. 1307], p. 567 , Linearized lifting-surface and lifting-line evaluations of sidewash behind rolling triangular wings a supersonic speeds, by Percy J. Bobitt, NACA [No. 1301], p. 455 , List of technical reports, p. III , Measurement of aerodynamic forces for various mean angles of attack on an airfoil oscillating in pitch and on two finite-span wings oscillating in bending with emphasis on damping in the stall, by A. Gerald Rainey, NACA [No. 1305], p. 520 , Method for calculating the aerodynamic loading on an oscillating finite wing in subsonic and sonic flow, by Harry L. Runyan and Donald S. Woolston, NACA [No. 1321], p. 971 , Minimum wave drag for arbitrary arrangements of wings and bodies, by Robert T. Jones, NACA [No. 1335], p. 1263 , Near noise field of a jet-engine exhaust, by Walton L. Howes, Edmund E. Callaghan, Willard D. Coles, and Harold R. Mull, NACA [No. 1338], p. 1355 , Nonlifting wing-body combinations with certain geometric restraints having minimum wave drag at low subsonic speeds, by Harvard Lomax, NACA [No. 1297], p. 113 , On panel flutter and divergence of infinitely long unstiffened and ring-stiffened thin-walled circular cylinders, by Robert W. Leonard and John M. Hedgepeth, NACA [No. 1302], p. 475 , On slender-body theory at transonic speeds, by Keith C. Harder and E.B. Klunker, NACA [No. 1315], p. 765 , Relation of turbojet and ramjet combustion efficiency to second-order reaction kinetics and fundamental flame speed, by J. Howard Childs, Thaine W. Reynolds, and Charles C. Graves, NACA [No. 1334], p. 1249 , Seat design for crash worthiness, by I. Irving Pinkel and Edmund G. Rosenberg, NACA [No. 1332], p.1211 , Some effects on bluntness on boundary-layer transition and heat transfer at supersonic speeds, by W.E. Moeckel, NACA [No. 1312], p. 709 , Summary of scale-model thrust-reverser investigation, by John H. Povolny, Fred W. Steffen and Jack G. McArdle, NACA [No. 1314], p. 751 , Table of contents, p. II , Theoretical calculation for the power spectra of the rolling and yawing moments of a wing in random turbulence, by John M. Eggleston and Franklin W. Diederich, NACA [No. 1321], p. 951 , Three-dimensional transonic flow theory applied to slender wings and bodies, by Max A. Heaslet and John R. Spreiter, NACA [No. 1318], p. 820 , Torsional stiffness of thin-walled shells having reinforcing cores and rectangular, triangular, or diamond cross section, by Harvey G. McComb, Jr., NACA [No. 1316], p. 771 , Wind-tunnel investigation of a number of total-pressure tubes at high angles of attack - subsonic, transonic, and supersonic speeds, by William Gracey, NACA [No. 1303], p. 495 , theoretical and experimental investigation of the subsonic-flow fields beneath swept and unswept wings with tables of vortex-induced velocities, by William J. Alford, Jr., NACA [No. 1327], p. 1083 , © 2008 by NewsBank, Inc. All rights reserved

Language: English

URL: Volltext  (Deutschlandweit zugänglich)

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Format: Online-Ressource (1503 p) , illustrations, tables

Edition: Online-Ausg. Chester, Vt NewsBank, inc 2008 U.S. Congressional Serial Set, 1817-1980

Series Statement: United States congressional serial set serial set no. 12180

Note: A comparative analysis of the performance of long-range hypervelocity vehicles, by Alfred J. Eggers, Jr., H. Julian Allen, and Stanford E. Neice, NACA [No. 1382], p. 1141 , A correlation of results of a flight investigation with results of an analytical study of effects of wing flexibility on wing strains due to gusts, by C.C. Shufflebarger, Chester B. Payne, and George L. Cahen, NACA [No. 1365], p. 669 , A low-speed experimental investigation of the effect of a sandpaper type of roughness on boundary layer transition, by Albert F. Von Doenhoff and Elmer A. Horton, NACA [No. 1349], p. 239 , A method for simulating the atmospheric entry of long-range ballistic missiles, by A.J. Eggers, Jr., NACA [No. 1378], p. 1009 , A method of computing the transient temperature of thick walls form arbitrary variation of adiabatic-wall temperature and heat-transfer coefficient, by P.R. Hill, NACA [No. 1372], p. 877 , A phenomenological relation between stress, strain rate, and temperature for metals at elevated temperatures, by Elbridge Z. Stowell, NACA [No. 1343], p. 125 , A simplified method for approximating the transient motion in angles of attack and sideslip during a constant rolling maneuver, by Leonard Sternfield, NACA [No. 1344], p. 131 , A study of the motion and aerodynamic heating of ballistic missiles entering the earth's atmosphere at hight supersonic speeds, by H. Julian Allen and A.J. Eggers, Jr. NACA [No. 1381], p. 1125 , A summary of preliminary investigations into the characteristics of combustion screech in ducted burners, by Lewis Laboratory Staff, NACA [No. 1384], p. 1195 , A theoretical and experimental study of planing surfaces including effects of cross section and plan form, by Charles L. Shuford, Jr., NACA [No. 1355], p. 373 , A variational theorem for creep with applications to plates and columns, by J. Lyell Sanders, Jr., Harvey G. McComb, Jr., and Floyd R. Schlechte, NACA [No. 1342], p. 117 , A wind-tunnel investigation of the aerodynamic characteristics of a full-scale supersonic-type three-blade propeller at Mach numbers to 0.96, by Albert J. Evans and George Liner, NACA [No. 1375], p. 933 , An analysis of pressure studies and experimental and theoretical downwash and sidewash behind five pointed-tip wings at supersonic speeds, by William B. Boatright, NACA [No. 1380], p. 1067 , An experimental investigation of sting-support effects on drag and a comparison with jet effects at transonic speeds, by Maurice S. Cahn, NACA [No. 1353], p. 327 , Approximate analysis of effects of large deflections and initial twist on torsional stiffness of a cantilever plate subjected to thermal stresses, by Richard R. Heldenfels and Louis F. Vosteen, NACA [No. 1361], p. 593 , Area-suction boundary-layer control as applied to the trailing-edge flaps of a 35 [degree] swept-wing airplane, by Woodrow L. Cook, Seth B. Anderson, and George E. Cooper, NACA [No. 1370], p. 823 , Blowing-type boundary-layer control as applied to the trailing-edge flaps of a 25 [degree] swept-wing airplane, by Mark W. Kelly, Seth B. Anderson, and Robert C. Innis, NACA [No. 1369], p. 799 , Boron and zirconium from crucible refractories in a complex heat-resistant alloy, by R.F. Decker, John P. Rowe, and J.W. Freeman, University of Michigan, [No. 1392], p. 1457 , Calculated and measured stresses in simple panels subject to intense random acoustic loading including the near noise field of a turbojet engine, by Leslie W. Lassiter and Robert W. Hess, NACA [No. 1367], p. 703 , Characteristics of the Langley 8-foot transonic tunnel with slotted test section, by Ray H. Wright, Virgil S. Ritchie, and Albin O. Pearson, NACA [No. 1389], p. 1297 , Compressible laminar boundary layer over a yawed infinite cylinder with heat transfer and arbitrary Prandtl number, by Eli Reshotku and Ivan E. Beckwith, NACA [No. 1379], p. 1016 , Differential equations of motion for combined flapwise vending, chordwise bending, and torsion of twisted non-uniform rotor blades, by John C. Houbolt and George W. Brooks, NACA [No. 1346], p. 179 , Ditching investigations of dynamic models and effects of design parameters on ditching characteristics, by Lloyd J. Fisher and Edward L. Hoffman, NACA [No. 1347], p. 197 , Drag minimization for wings and bodies in supersonic flow, by Max A. Heaslet and Franklyn B. Fuller, NACA [No. 1385], p. 1213 , Effect of chord size on weight and cooling characteristics of air-cooled turbine blades, by Jack B. Esgar, Eugene F. Schum, and Arthur N. Curren, NACA [No. 1354], p. 359 , Effect of fuel variables on carbon formation in turbojet-engine combustors, by Edmund R. Jonash, Jerrold D. Wear, and William P. Cook, NACA [No. 1352], p. 309 , Elliptic cones alone and with wings at supersonic speeds, by Leland H. Jorgensen, NACA [No. 1376], p. 975 , Experimental determination of effects of frequency and amplitude on the lateral stability derivatives for a delta, a swept, and an unswept wing oscillating in yaw, by Lewis R. Fisher, NACA [No. 1357], p. 461 , Full-scale investigation of several jet-engine noise-reduction nozzles, by Willard D. Coles and Edmund E. Callaghan, NACA [No. 1387], p. 1249 , Ground simulator studies of the effects of valve friction, stick friction, flexibility, and backlash on power control system quality, by B. Porter Brown, NACA [No. 1348], p. 225 , Growth of disturbances in a flame-generated shear region, by Perry L. Blackshear, Jr., NACA [No. 1360], p. 546 , Incompressible flutter characteristics of representative aircraft wings, by C.H. Wilts, California Institute of Technology, [No. 1390], p. 1385 , Investigation of a nonlinear control system, by I. Flugge-Lotz, C.F. Taylor, and H.E. Lindberg, Stanford University, [No. 1391], p. 1423 , Investigation of separated flows in supersonic and subsonic streams with emphasis on the effect of transition, by Dean R. Chapman, Donald M. Kuehn, and Howard K. Larson, NACA [No. 1356], p. 419 , Investigation of some wake vortex characteristics of an inclined ogive-cylinder body at Mach number 2, by Leland H. Jorgensen and Edward W. Perkins, NACA [No. 1371], p. 857 , Investigation of the drag of various axially symmetric nose shapes of fineness ratio 3 for Mach numbers from 1.24 to 7.4, by Edward W. Perkins, Leland H. Jorgensen, and Simon C. Sommer, NACA [No. 1386], p. 1231 , List of technical reports, p. III , Measurement of static pressure on aircraft, by William Gracey, NACA [No. 1364], p. 643 , Measurements of free-space oscillating pressures near propellers at flight Mach numbers to 0.72, by Max C. Kurbjun and Arthur W. Vogeley, NACA [No. 1377], p. 999 , Methods for obtaining desired helicopter stability characteristics and procedures for stability predictions, by F.B. Gustafson and Robert J. Topscott, NACA [No. 1350], p. 255 , NACA Research on slurry fuels, by M.L. Pinns, W.T. Olson, H.C. Barnett, and R. Breitwieser, NACA [No. 1388], p. 1273 , On flow of electrically conducting fluids over a flat plate in presence of a transverse magnetic field, by Vernon J. Rossow, NACA [No. 1358], p. 489 , Origin and prevention of crash fires in turbojet aircraft, by I. Irving Pinkel, Solomon Weiss, G. Merritt Preston, and Gerard J. Pesman, NACA [No. 1363], p. 623 , Survey of hydrogen combustion properties, by Isadore L. Drell and Frank E. Belles, NACA [No. 1383], p. 1161 , Systemic two-dimensional cascade tests of NACA 65-Series compressor blades at low speeds, by James C. Emery, L. Joseph Herrig, John R. Erwin, and A. Richard Felix, NACA [No. 1368], p. 713 , Table of contents, p. II , The mechanism of thermal-gradient mass transfer in the sodium hydroxide - nickel system, by Charles E. May, NACA [No. 1366], p. 683 , The response of an airplane to random atmospheric disturbances, by Franklin W. Diederich, NACA [No. 1345], p. 142 , The similarity rules for second-order subsonic and supersonic flow, by Milton D. Van Dyke, NACA [No. 1374], p. 925 , Theoretical analysis of total-pressure loss and airflow distribution for tubular turbojet combustors with constant annulus- and liner cross-sectional areas, by Charles C. Graves and Jack S. Grobman, NACA [No. 1373], p. 899 , Theoretical combustion performance of several high-energy fuels for ramjet engines, by Leonard K. Tower, Roland Breitwieser, and Benson E. Gammon, NACA [No. 1362], p. 605 , Theory of self-excited mechanical oscillations of helicopter rotors with hinged blades, by Robert P. Coleman and Arnold M. Feingold, NACA [No. 1351], p. 267 , Thin airfoil theory based on approximate solution of the transonic flow equation, by John R. Spreiter and Alberta Y. Alksne, NACA [No. 1359], p. 509 , © 2008 by NewsBank, Inc. All rights reserved

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Format: 2 ungezählte Seiten , 17,8 x 10,8 cm

Edition: Online-Ausgabe Berlin Staatsbibliothek zu Berlin - Preußischer Kulturbesitz 2022 1 Online-Ressource Einblattdrucke digital

Note: Rückseite: Grundsätze des Kriegsgefangenenrechts (Laut Haager Konvention 1907, Genfer Konvention 1929) , Beiseitig bedrucktes Blatt; Vorderseite auf rotem Untergrund gedruckt , Von den Amerikanern/Engländern an die deutschen Soldaten gerichtet , SBB-PK Berlin

Additional Edition: Elektronische Reproduktion von SBB-PK Berlin -- Einbl. 1939/45, 4724. 561 A-1944 Passierschein - Der deutsche Soldat, der diesen Passierschein vorzeigt, benutzt ihn als Zeichen seines ehrlichen Willens, sich zu ergeben... [Erscheinungsort nicht ermittelbar], 1944

Language: German

Keywords: Einblattdruck ; Flugblatt

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Author information: Eisenhower, Dwight D. 1890-1969

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Edition: Online-Ausg. Berlin Staatsbibliothek zu Berlin - Preußischer Kulturbesitz 2015 Online-Ressource (Text) Einblattdrucke digital

Edition: Historische Drucke digital

Content: nur Text

Note: Datiert: 5. Juni 1945 , Textbeginn: Die deutschen Streitkräfte zu Lande, zu Wasser und in der Luft sind vollständig geschlagen und haben bedingungslos kapituliert, , SBB-PK Berlin

Additional Edition: Druckausg. Unterzeichnung der Deklaration über die Niederlage Deutschlands und die Uebernahme höchster Autorität hinsichtlich Deutschlands durch die Regierungen der Union der Sozialistischen Sowjetrepubliken, des Vereinigten Königreichs, der Vereinigten Staaten von Amerika und der Provisorischen Regierung der Französischen Republik [Berlin], 1945

Language: German

Keywords: Zweiter Weltkrieg ; Kriegsende ; Kapitulation Deutschlands ; Einblattdruck

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Author information: Žukov, Georgij Konstantinovič 1896-1974

Author information: Montgomery of Alamein, Bernard Law Montgomery Viscount 1887-1976

Author information: Eisenhower, Dwight D. 1890-1969

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Format: Online-Ressource (1011 p) , illustrations, tables

Edition: Online-Ausg. Chester, Vt NewsBank, inc 2008 U.S. Congressional Serial Set, 1817-1980

Series Statement: United States congressional serial set serial set no. 12003

Note: A reevaluation of data on atmospheric turbulence and airplane gust loads for application in spectral calculations, by Harry Press, May T. Meadows, and Ivan Hadlock, NACA [No. 1272], p. 489 , A special method for finding body distortions that reduce the wave drag of wing and body combinations at supersonic speeds, by Harvard Lomax and Maz A. Heaslet, NACA [No. 1282], p. 709 , A study of the zero-lift drag-rise characteristics of wing-body combinations near the speed of sound, by Richard T. Whitcomb, NACA [No. 1273], p. 519 , A theory for stability and buzz pulsation amplitude in ram jets and an experimental investigation including scale effects, by Robert L. Trimpi, NACA [No. 1265], p. 295 , A thermal equation for flame quenching, by A.E. Potter, Jr., and A.L. Berlad, NACA [No. 1264], p. 287 , A wind-tunnel test technique for measuring the dynamic rotary stability derivatives at subsonic and supersonic speeds, by Benjamin H. Beam, NACA [No. 1258], p. 165 , An analysis of the stability and ultimate compressive strength of short sheet-stringer panels with special reference to the influence of the riveted connection between sheet and stringer, by Joseph W. Semonian and James P. Peterson, NACA [No. 1255], p. 113 , Axially symmetric shapes with minimum wave drag, by Max. A. Heaslet and Franklyn B. Fuller, NACA [No. 1256], p. 131 , Charts for estimating performance of high-performance helicopters, by Alfred Gessow and Robert J. Tapscott, NACA [No. 1266], p. 319 , Contributions on the mechanics of boundary-layer-transition, by G.B. Schubauer and P.S. Kelbanoff, National Bureau of Standards, [No. 1289], p. 853 , Cooperative investigation of relationship between static and fatigue properties of wrought N-155 alloy at elevated temperatures, by NACA Subcommittee on Power-Plant Materials, [No. 1288, p. 817 , Development of craze and impact resistance in glazing plastics by multiaxial stretching, by G.M. Kline, I. Wolock, B.M. Axilrod, M.A. Sherman, D.A. George, and V. Cohen, National Bureau of Standards, [No. 1290], p. 865 , Effect of interaction on landing-gear behavior and dynamic leads in a flexible airplane structure, by Francis E. Cook and Benjamin Milwitzky, NACA [No. 1278], p. 619 , Extrapolation techniques applied to matrix methods in neutron diffusion problems, by Robert R. McCready, NACA [No. 1283], p. 747 , Flight determination of drag of normal-shock nose inlets with various cowling profiles at Mach numbers from 0.9 to 1.5, by R.I. Sears, C.F. Merlet, and L.W. Putland, NACA [No. 1281], p. 689 , Friction, wear, and surface damage of metals as affected by solid surface films, by Edmond E. Bisson, Robert L. Johnson, Max A. Swikert and Douglas Godfrey, NACA [No. 1254], p. 91 , Interaction of a free flame front with a turbulence field, by Maurice Tucker, NACA [No. 1277], p. 599 , Investigation of the aerodynamic characteristics of a model wing-propeller combination and of the wing and propeller separately at angles of attack up to 90 [degrees], by Richard E. Kuhn and John W. Draper, NACA [No. 1263], p. 247 , Lift hysteresis at stall as an unsteady boundary-layer phenomenon, by Franklin K. Moore, NACA [No. 1291], p. 881 , List of technical reports, p. III , On boattail bodies of revolution having minimum wave drag, by Keith C. Harder and Conrad Rennemann, Jr., NACA [No. 1271], p. 479 , On the kernel function of the integral equation relating lift and downwash distributions of oscillating wings in supersonic flow, by Charles E. Watkins and Julian H. Berman, NACA [No. 1287], p. 147 , Plastic deformation of aluminum single crystals at elevated temperatures, by R.D. Johnson, A.P. Young, and A.D. Schwope, Battelle Memorial Institute, [No. 1267], p. 353 , Propagation of free flame in a turbulent gas stream, by William R. Mickelsen and Norman E. Ernstein, NACA [No. 1286], p. 773 , Review of experimental investigations of liquid-metal heat transfer, by Bernard Lubarsky and Samuel J. Kaufman, NACA [No. 1270], p. 445 , Second-order subsonic airfoil theory including edge effects, by Milton D. Van Dyke, NACA [No. 1274], p. 541 , Some possibilities of using gas mixtures other than air in aerodynamic research, by Dean R. Chapman, NACA [No. 1259], p. 179 , Spark ignition of flowing gases, by Clyde C. Swett, Jr., NACA [No. 1287], p. 799 , Studies of the speed stability of a tandem helicopter in forward flight, by Robert J. Tapscott and Kenneth B. Amer, NACA [No. 1260], p. 201 , Summary of derived gust velocities obtained from measurements within thunderstorms, by H.B. Tolefson, NACA [No. 1285], p. 765 , Table of contents, p. II , The near noise field of static jets and some model studies of devises for noise reduction, by Leslie W. Lassiter and Harvey H. Hubbard, NACA [No. 1261], p. 213 , The proper combination of lift loading for least drag on a supersonic wing, by Frederick C. Grant, NACA [No. 1275], p. 565 , Theoretical analysis of incompressible flow through a radial-inlet centrifugal impeller at various weight flows, by James J. Kramer, Vasily D. Prian, and Chung-Hua Wu, NACA [No. 1279], p. 649 , Theoretical and experimental investigation of the effect of tunnel walls on the forces on an oscillating airfoil in two-dimensional subsonic compressible flow, by Harry L. Runyan, Donald S. Woolston, and A. Gerald Rainey, NACA [No. 1262], p. 225 , Theoretical calculations of the pressures, forces, and moments at supersonic speeds due to various lateral motions actin on thin isolated vertical tails, by Kenneth Margolis and Percy J. Bobbitt, NACA [No. 1268], p. 385 , Theoretical investigation of flutter of two-dimensional flat panels with one surface exposed to supersonic potential flow, by Herbert C. Nelson and Herbert J. Cunningham, NACA [No. 1280], p. 665 , Theoretical span load distributions and rolling moments for sideslipping wings of arbitrary plan form in incompressible flow, by M.J. Queijo, NACA [No. 1269], p. 429 , Theory of wing-body drag at supersonic speeds, by Robert T. Jones, NACA [No. 1284], p. 757 , Wind-tunnel and flight investigations of the use of leading-edge area suction for the purpose of increasing the maximum lift coefficient of a 35 [degree] swept-wing airplane, by Curt A. Helzhauser and Richard S. Bray, NACA [No. 1276], p. 575 , © 2008 by NewsBank, Inc. All rights reserved

Language: English

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Edition: Online-Ausg. Berlin Staatsbibliothek zu Berlin - Preußischer Kulturbesitz 2013 Online-Ressource (Text) Einblattdrucke digital

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Note: Aufführungsdatum: 22.02.1848 , Art der Aufführung: 25ste Abonnements-Vorstellung , Mad. Viardot-Garcia als vorletzte Gastrolle , Aufführungsort: Berlin , SBB-PK Berlin , Sprache der Aufführung: deutsch

Additional Edition: Druckausg. Königliche Schauspiele zu Berlin Iphigenia in Tauris Berlin, 1848

Language: German

Keywords: Staatstheater Berlin ; Preußische Staatstheater ; Königliches Nationaltheater ; Berlin ; Literatur ; Deutsch ; Programmheft ; Einblattdruck ; Theaterzettel

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Author information: Sander, Johann Daniel 1759-1825

Author information: Viardot-García, Pauline 1821-1910

Author information: Krause, Julius 1810-1881

Author information: Guillard, Nikolas François 1752-1814

Author information: Litfaß, Ernst 1816-1874

Author information: Schneider, Louis 1805-1878

Author information: Gluck, Christoph Willibald 1714-1787

Author information: Mantius, Eduard 1806-1874

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Edition: Online-Ausg. Berlin Staatsbibliothek zu Berlin - Preußischer Kulturbesitz 2013 Online-Ressource (Text) Einblattdrucke digital

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Note: Aufführungsdatum: 03.02.1848 , Art der Aufführung: 21ste Schauspielhaus-Abonnements-Vorstellung , Aufführungsort: Berlin , SBB-PK Berlin , Sprache der Aufführung: deutsch

Additional Edition: Druckausg. Königliche Schauspiele zu Berlin Die Quitzows Berlin, 1848

Language: German

Keywords: Staatstheater Berlin ; Preußische Staatstheater ; Königliches Nationaltheater ; Berlin ; Literatur ; Deutsch ; Programmheft ; Einblattdruck ; Theaterzettel

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Author information: Wauer, Carl 1783-1857

Author information: Crelinger, Auguste 1795-1865

Author information: Rott, Moritz 1796-1867

Author information: Grua, Franz 1799-1867

Author information: Niehr, Friedrich 1673-

Author information: Gern, Albert Leopold 1789-1869

Author information: Mickler, August 1800-1876

Author information: Schneider, Louis 1805-1878

Author information: Litfaß, Ernst 1816-1874

Author information: Franz, Emil Karl Friedrich 1808-1875

Author information: Henning, Carl Wilhelm 1784-1867

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Format: Online-Ressource (1386 p) , illustrations, tables

Edition: Online-Ausg. Chester, Vt NewsBank, inc 2008 U.S. Congressional Serial Set, 1817-1980

Series Statement: United States congressional serial set serial set no. 11917

Note: A correlation by means of transonic similarity rules of experimentally determined characteristics of a series of symmetrical and cambered wings of rectangular plan form, by John B. McDevitt, NACA [No. 1253], p. 1355 , A flight evaluation of the longitudinal stability characteristics associated with the pitch-up of a swept-wing airplane in maneuvering flight at transonic speeds, by Seth B. Anderson and Richard S. Bray, NACA [No. 1237], p. 843 , A free-flight wind tunnel for aerodynamic testing at hypersonic speeds, by Alvin Seiff, NACA [No. 1222], p. 381 , A method for the design of swept-back wings warped to produce specified flight characteristics at supersonic speeds, by Warren A. Tucker, NACA [No. 1226], p. 459 , A theoretical and experimental investigation of the lift and drag characteristics of hydrofoils at subcritical and supercritical speeds, by Kenneth L. Wadlin, Charles L. Shuford, Jr., and John R. McGehee, NACA [No. 1232], p. 661 , A unified two-dimensional approach to the calculation of three-dimensional hypersonic flows, with application to bodies of revolution, by A.J. Eggers, Jr., and Raymond C. Savin, NACA [No. 1249], p. 1189 , An experimental study of applied ground loads in landing, by Benjamin Milwitzky, Dean C. Lindquist, and Dexter M. Potter, NACA [No. 1248], p. 1155 , An investigation of the effects of heat transfer on boundary-layer transition on a parabolic body of revolution (NACA RM-10) at a Mach number of 1.61, by K.R. Czarnecki and Archibald R. Sinclair, NACA [No. 1240], p. 929 , An investigation of the maximum lift of wings at supersonic speeds, by James J. Gallagher and James N. Mueller, NACA [No. 1227], p. 477 , Analog study of interacting and non-interacting multiple-loop control systems for turbojet engines, by George J. Pack and W.E. Philips, Jr., NACA [No. 1212], p. 97 , Analysis and calculation by integral methods of laminar compressible boundary layer with heat transfer and with and without pressure gradient, by Morris Morduchow, Polytechnic Institute of Brooklyn, [No. 1245], p. 1065 , Analysis of turbulent heat transfer, mass transfer, and friction in smooth tubes at high Prandtl and Schmidt numbers, by Robert G. Diessler, NACA [No. 1210], p. 69 , Arrangement of fusiform bodies to reduce the wave drag at supersonic speeds, by Morris D. Friedman and Doris Cohen, NACA [No. 1236], p. 835 , Calculated spanwise lift distributions, influence functions, and influence coefficients for unswept wings in subsonic flow, by Franklin W. Diederich and Martin Zlotnick, NACA [No. 1228], p. 505 , Calculation of laminar heat transfer around cylinders of arbitrary cross section and transpiration-cooled walls with application to turbine blade cooling, by E.R.G. Eckert and J.N.B. Livingood, NACA [No. 1220], p. 339 , Characteristics of turbulence in a boundary layer with zero pressure gradient, by P.S. Klebanoff, National Bureau of Standards, [No. 1247], p. 1135 , Charts for estimating tail-rotor contribution to helicopter directional stability and control in low-speed flight, by Kenneth B. Amer and Alfred Gessow, NACA [No. 1216], p. 185 , Determination of lateral -stability derivatives and transfer-function coefficients from frequency-response data for lateral motions, by James J. Donegan, Samuel W. Robinson, Jr., and Ordway B. Gates, Jr., NACA [No. 1225], p. 439 , Effect of ground interference on aerodynamic and flow characteristics of a 42 [degree] sweptback wing Reynolds numbers up to 6.8X10(6), by G. Chester Furlong and Thomas V. Bollech, NACA [No. 1218], p. 251 , Effects of wing position and fuselage size on the low-speed static and rolling stability characteristics of a delta-wing model, by Alex Goodman and David F. Thomas, NACA [No. 1224], p. 407 , Error in airspeed measurement due to the static-pressure field ahead of an airplane at transonic speeds, by Thomas C. O'Bryan, Edward C.B. Danforth, and J. Ford Johnston, NACA [No. 1239], p. 915 , Exact solutions of laminar-boundary-layer equations with constant property values for porous wall with variable temperature, by Patrick L. Donoughe and John N.B. Livingood, NACA [No. 1229], p. 573 , Experimental investigation of free-convection heat transfer in vertical tube at large Grashof numbers, by E.R.G. Eckert and A.J. Diaguila, NACA [No. 1211], p. 83 , Free-stream boundaries of turbulent flows, by Stanley Corrsin and Alan L. Kistler, The Johns Hopkins University, [No. 1244], p. 1033 , Generalized indicial forces on deforming rectangular wings in supersonic flight, by Harvard Lomax, Franklyn B. Fuller, and Loma Sluder, NACA [No. 1230], p. 595 , High-resolution autoradiography, by George C. Towe, Henry J. Gomberg, and J.W. Freeman, University of Michigan, [No. 1243], p. 979 , Impingement of cloud droplets on a cylinder and procedure for measuring liquid-water content and droplet sized in supercooled clouds by rotating multicylinder method, by R.J. Brun, W. Lewis, P.J. Perkins, and J.S. Serafini, NACA [No. 1215], p. 139 , Investigation at supersonic speeds of 22 triangular wings representing two airfoil sections for each of 11 apex angles, by Eugene S. Love, NACA [No. 1238], p. 855 , List of technical reports, p. III , Measurement and analysis of wing and tail buffeting loads on fighter airplane, by Wilber B. Huston and T.H. Skopinski, NACA [No. 1219], p. 311 , Minimum-drag ducted and pointed bodies of revolution based on linearized supersonic theory, by Hermon M. Parker, NACA [No. 1213], p. 111 , NACA transonic wind-tunnel test sections, by Ray H. Wright and Vernon G. Ward,NACA [No. 1231], p. 623 , On the kernel function of the integral equation relating the lift of downwash distributions of oscillating finite wings in subsonic flow, by Charles E. Watkins, Harry L. Runyan, and Donald S. Woolston, NACA [No. 1234], p. 703 , Quasi-cylindrical theory of wing-body interference at supersonic speeds and comparison with experiment, by Jack N. Nielsen, NACA [No. 1252], p. 1299 , Shock-turbulence interaction and the generation of noise, by H.S. Ribner, NACA [No. 1233], p. 682a , Standard atmosphere - tables and data for altitudes to 65,800 feet, by International Aviation Organization and NACA, [No. 1235], p. 719 , Statistical measurements on contact conditions of 478 transport-airplane landings during routine daytime operations, by Norman S. Silsby, NACA [No. 1214], p. 121 , Stress-analysis of circular semimonocoque cylinders with cutouts, by Harvey G. McComb, NACA [No. 1251], p. 1243 , Table of contents, p. II , The dynamic-response characteristics of a 35 [degree] swept-wing airplane as determined from flight measurements, by William C. Triplett, Stuart C. Brown, and G. Allan Smith, NACA [No. 1250], p. 1217 , The hydrodynamic characteristics of modified rectangular flate plates having aspect rations of 1.00, 0.25, and 0.125 and operating near a free water surface, by Kenneth L. Wadlin, John A. Ramsen, and Victor L. Vaughan, Jr., NACA [No. 1246], p. 1085 , Theoretical and analog studies of the effects of nonlinear stability derivatives on the longitudinal motions of an aircraft in response to step control deflections and to the influence of proportional automatic control, by Howard J. Curfman, Jr., NACA [No. 1241], p. 941 , Theoretical and experimental investigation of heat transfer by laminar natural convection between parallel plates, by A.F. Lietzke, NACA [No. 1223], p. 399 , Theoretical prediction of pressure distributions on nonlifting airfoils at high subsonic speeds, by John R. Spreiter and Alverta Alksne, NACA [No. 1217], p. 207 , Theoretical study of the tunnel-boundary lift interference due to slotted walls in the presence of the trailing -vortex system of the lifting model, by Clarence W. Matthews, NACA [No. 1221], p. 361 , Transonic flow past cone cylinders, by George E. Solomon, California Institute of Technology, [No. 1222], p. 963 , © 2008 by NewsBank, Inc. All rights reserved

Language: English

URL: Volltext  (Deutschlandweit zugänglich)

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Format: Online-Ressource (Text)

Edition: Online-Ausg. 2018 Einblattdrucke digital

Edition: Theaterzettel digital

Note: Aufführungsdatum: 21.09.1892 , Aufführungsort: Berlin

In: Königliche Schauspiele zu Berlin, Theaterzettel - Königliche Schauspiele. Opernhaus - 187. Vorstellung. 1892-09-21, [Berlin] : Ernst Litfaß' Erben, 1892, Stück 2

In: year:1892

In: pages:2

Additional Edition: Druckausg. Königliche Schauspiele zu Berlin Das schlecht bewachte Mädchen 1892

Language: German

URL: Volltext  (kostenfrei)

Author information: Taglioni, Paul 1808-1884

Author information: Hertel, Peter Ludwig 1817-1899

Author information: Bercher, Jean 1742-1806

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Format: 1 Bl.

Edition: Online-Ausg. Berlin Staatsbibliothek zu Berlin - Preußischer Kulturbesitz 2013 Online-Ressource (Text) Einblattdrucke digital

Edition: Historische Drucke digital

Note: Aufführungsdatum: 03.09.1848 , Titel in Vorlageform: Don Juan , Art der Aufführung: 95ste Abonnements-Vorstellung , Person in Vorlage: Instrumentiert von J.P. Schmidt , Aufführungsort: Berlin , SBB-PK Berlin

Additional Edition: Druckausg. Königliche Schauspiele zu Berlin Don Giovanni Berlin, 1848

Language: German

Keywords: Staatstheater Berlin ; Preußische Staatstheater ; Königliches Nationaltheater ; Berlin ; Literatur ; Deutsch ; Programmheft ; Einblattdruck ; Theaterzettel

URL: Volltext  (kostenfrei)

Author information: Zschiesche, August 1800-1876

Author information: Schmidt, Johann Philipp Samuel 1779-1853

Author information: Da Ponte, Lorenzo 1749-1838

Author information: Stawinsky, Karl 1794-1866

Author information: Mickler, August 1800-1876

Author information: Mozart, Wolfgang Amadeus 1756-1791

Author information: Krause, Julius 1810-1881

Author information: Litfaß, Ernst 1816-1874

Author information: Mantius, Eduard 1806-1874

Author information: Marx, Pauline 1819-1881