Kooperativer Bibliotheksverbund

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ISBN: 9780791886281

In: ASME International Design Engineering Technical Conferences and Computers and Information in Engineering Conference (2022 : Saint Louis, Mo.), Proceedings of ASME 2022 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference (IDETC-CIE 2022) ; Volume 7: 46th Mechanisms and Robotics Conference (MR), New York, N.Y. : the American Society of Mechanical Engineers, 2022, (2022), 9780791886281

In: year:2022

Language: English

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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

URL: Volltext  (Deutschlandweit zugänglich)

UID:

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

URL: Volltext  (Deutschlandweit zugänglich)

UID:

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)

UID:

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)