Kooperativer Bibliotheksverbund

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Format: Online-Ressource (3 p)

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. 11378

Note: © 2008 by NewsBank, Inc. All rights reserved

Language: English

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Format: Online-Ressource (987 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. 11554

Note: A radar method of calibrating airspeed installations on airplanes in maneuvers at high altitudes and at transonic and supersonic speeds, by John A. Zalcovcik [No. 985], p. 661 , An analysis of supersonic aerodynamic heating with continuous fluid injection, by E.B. Klunker and H. Reese Ivey [No. 990], p. 701 , An introduction to the physical aspects of helicopter stability, by Alfred Gessow and Kenneth B. Amer [No. 993], p. 739 , Analysis of spanwise temperature distribution in three types of air-cooled turbine blade, by John N.B. Livingood and W. Byron Brown [No. 994], p. 753 , Appendices, p. 100 , Application of radial-equilibrium condition to axial-flow compressor and turbine design, by Chung-Hua Wu and Lincoln Wolfenstein [No. 955], p. 165 , Attainable circulation about airfoils in cascade, by Arthur W. Goldstein and Artur Mager [No. 953], p. 117 , Blockage corrections for three-dimensional-flow closed-throat wind tunnels, with consideration of the effect of compressibility, by John G. Herriot [No. 995], p. 771 , Calculation of the aerodynamic loading of swept and unswept flexible wings of arbitrary stiffness, by Franklin W. Diederich [No. 1000], p. 909 , Comparative drag measurements at transonic speeds of rectangular and sweptback NACA 65-109 airfoils mounted on a freely falling body, by Charles W. Mathews and Jim Rogers Thompson [No. 988], p. 685 , Critical stress of ring-stiffened cylinders in torsion, by Manuel Stein, J. Lyell Sanders, Jr., and Harold Crate [No. 989], p. 693 , Determination of plate compressive strengths at elevated temperatures, by George J. Heimerl and William M. Roberts [No. 960], p. 251 , Direct method of design and stress analysis of rotating disks with temperature gradient, by S.S. Manson [No. 952], p. 103 , Elastic and plastic buckling of simply supported solid-core sandwich plates in compression, by Paul Seide and Elbridge Z. Stowell [No. 967], p. 357 , Equilibrium operating performance of axial-flow turbojet engines by means of idealized analysis, by John C. Sanders and Edward C. Chapin [No. 987], p. 673 , Flight investigation of the effect of various vertical-tail modifications on the directional stability and control characteristics of a propeller-driven fighter airplane, by Harold L. Johnson [No. 973], p. 453 , Flutter of a uniform wing with an arbitrarily placed mass according to a differential-equation analysis and a comparison with experiment, by Harry L. Runyan and Charles E. Watkins [No. 966], p. 339 , Free-space oscillating pressures near the tips of rotating propellers, by Harvey H. Hubbard and Arthur A. Regier [No. 996], p. 785 , Frequency response of linear systems from transient data, by Melvin E. Laverne and Aaron S. Boksenbom [No. 977], p. 547 , Fundamental effects of aging on creep properties of solution-treated low-carbon N-155 alloy, by D.N. Frey, J.W. Freeman, and A.E. White [No. 1001], p. 939 , Further experiments on the flow and heat transfer in a heated turbulent air jet, by Stanley Corrsin and Mahinder S. Uberoi [No. 998], p. 859 , General algebraic method applied to control analysis of complex engine types, by Aaron S. Boksenbom and Richard Hood [No. 980], p. 581 , Icing-protection requirements for reciprocating-engine induction systems, by Willard D. Coles, Vern G. Rollin, and Donald R. Mulholland [No. 982], p. 611 , Investigation at low speeds of the effect of aspect ratio and sweep on rolling stability derivatives of untapered wings, by Alex Goodman and Lewis R. Fisher [No. 968], p. 367 , Investigation of the NACA 4-(3)(08)-03 and NACA 4-(3)(08)-045 two-blade propellers at forward mach numbers to 0.725 to determine the effects of compressibility and solidity on performance, by John B. Delano and Lewis Feldman [No. 999], p. 877 , Investigation with an interferometer of the turbulent mixing of a free supersonic jet, by Paul B. Gooderum, George P. Wood, and Maurice J. Brevoort [No. 963], p. 289 , Laminar mixing of a compressible fluid, by Dean R. Chapman [No. 958], p. 231 , Line-vortex theory for calculation of supersonic downwash, by Harold Mirels and Rudolph C. Haefeli [No. 983], p. 635 , Linear theory of boundary effects in open wind tunnels with finite jet lengths, by S. Katzoff, Clifford S. Gardner, Leo Diesendruck, and Bertram J. Eisenstadt [No. 976], p. 509 , Linearized compressible-flow theory for sonic flight speeds, by Max A. Heaslet, Harvard Lomax, and John R. Spreiter [No. 956], p. 195 , Method for determining the frequency-response characteristics of an element or system from the system transient output response to a known input function, by Howard J. Curfman, Jr. and Robert A. Gardiner [No. 984], p. 651 , Method of designing cascade blades with prescribed velocity distributions in compressible potential flows, by George R. Costello [No. 978], p. 559 , On stability of free laminar boundary layer between parallel streams, by Martin Lessen [No. 979], p. 571 , On the theory of oscillating airfoils of finite span in subsonic compressible flow, by Eric Reissner [No. 1002], p. 969 , One-dimensional flows of an imperfect diatomic gas, by A.J. Eggers [No. 959], p. 239 , Small bending and stretching of sandwich-type shells, by Eric Reissner [No. 975], p. 483 , Some theoretical low-speed span loading characteristics of swept wings in roll and sideslip, by John D. Bird [No. 969], p. 379 , Summary of information relating to gust loads on airplanes, by Philip Donely [No. 997], p. 807 , Table of contents, p. II , The aerodynamic forces on slender plane and cruciform-wing and body combinations, by John R. Spreiter [No. 962], p. 271 , The application of Green's theorem to the solution of boundary-value problems in linearized supersonic wing theory, by Max A. Heaslet and Harvard Lomax [No. 961], p. 257 , The application of the statistical theory of extreme values to gust-load problems, by Harry Press [No. 991], p. 711 , The calculation of downwash behind supersonic wings with an application to triangular plan forms, by Harvard Lomax, Loma Sluder, and Max A. Heaslet [No. 957], p. 211 , The effect of torsional flexibility on the rolling characteristics at supersonic speeds of tapered unswept wings, by Warren A. Tucker and Robert L. Nelson [No. 972], p. 425 , The effects of variations in Reynolds Number between 3.0 X 10 [to the sixth power] and 2.5 X 10 [to the sixth power] upon the aerodynamic characteristics of a number of NACA 6-Series airfoil sections, by Laurence K. Loftin, Jr. and William J. Bursnall [No. 964], p. 307 , The longitudinal stability of elastic swept wings at supersonic speed, by C.W. Frick and R.S. Chubb [No. 965], p. 327 , The reversibility theorem for thin airfoils in subsonic and supersonic flow, by Clinton E. Brown [No. 986], p. 669 , The supersonic axial-flow compressor, by Arthur Kantrowitz [No. 974], p. 473 , Theoretical analysis of various thrust-augmentation cycles for turbojet engines, by Bruce T. Lundin [No. 981], p. 593 , Theoretical comparison of several methods of thrust augmentation for turbojet engines, by Eldon W. Hall and E. Clinton Wilcox [No. 992], p. 727 , Theoretical lift and damping in roll and supersonic speeds of thin sweptback tapered wings with streamwise tips, subsonic leading edges, and supersonic trailing edges, by Frank S. Malvestuto, Jr., Kenneth Margolis, and Herbert S. Ribner [No. 970], p. 395 , Theoretical stability derivatives of thin sweptback wings tapered to a point with sweptback or sweptforward trailing edges for a limited range of supersonic speeds, by Frank S. Malvestuto, Jr. and Kenneth Margolis [No. 971], p. 411 , Two-dimensional compressible flow in centrifugal compressors with straight blades, by John D. Stanitz and Gaylord O. Ellis [No. 954], p. 141 , Use of source distributions for evaluating theoretical aerodynamics of thin finite wings at supersonic speeds, by John C. Evvard [No. 951], p. 71 , © 2008 by NewsBank, Inc. All rights reserved

Language: English

URL: Volltext  (Deutschlandweit zugänglich)

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Format: Online-Ressource (490 p) , illustrations, maps, 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. 11780

Note: Appendices, p. 14 , Applied systematics: The usefulness of scientific names of animals and plants, by Waldo L. Schmitt, p. 323 , Barro Colorado -- tropical island laboratory, by Lloyd Glenn Ingles, p. 361 , Charles Bird King, painter of Indian visitors to the nation's capital, by John C. Ewers, p. 463 , Climate and race, by Carleton Coon, p. 277 , Genetics and the world today, by Curt Stern, p. 263 , Index, p. 475 , Kinreizuka -- the "Golden Bells Tomb" of Japan, by Motosaburo Hirano and Hiroshi Takiguchi, p. 437 , List of plates, p. IV , Norsemen in North America before Columbus, by Johannes Brondsted, p. 367 , Radioisotopes -- new keys to knowledge, by Paul C. Aebersold, p. 219 , Recent progress on astronomical photography, by C.E. Kenneth Mees, p. 205 , Science, art, and education, by R.E. Gibson, p. 169 , Table of contents, p. III , The archeology of colonial Williamsburg, by Thomas J. Wertenbaker, p. 447 , The coelacanth fishes, by Errol White, p. 351 , The geological history and evolution of insects, by F.M. Carpenter, p. 339 , The mountain village of Dahr, Lebanon, by Raymond E. Crist, p. 407 , The problem of dating the Dead Sea Scrolls, by John C. Trever, p. 425 , The push-button factory, by Frank K. Shallenberger, p. 241 , The science of musical instruments, by E.G. Richardson, p. 253 , The story of the Declaration of Independence desk and how it came to the National Museum, by Margaret W. Brown, p. 455 , Vegetation management for rights-of-way and roadsides, by Frank E. Egler, p. 299 , © 2008 by NewsBank, Inc. All rights reserved

Language: English

URL: Volltext  (Deutschlandweit zugänglich)

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Format: Online-Ressource (247 p) , illus , 22cm

Edition: Online-Ausg. Alexandria, VA Alexander Street Press 2006 Latino literature

Note: Includes bibliography , Text in English or Spanish

Language: English

URL: Volltext

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Format: 1 Online-Ressource (1v.)

Language: Undetermined

URL: Volltext

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Format: Online-Ressource (1452 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. 11595

Note: A comparison of theory and experiment for high-speed free-molecule flow, by Jackson R. Stalder, Glen Goodwin, and Marcus O. Creager [No. 1032], p. 735 , A general integral form of the boundary-layer equation for incompressible flow with an application to the calculation of the separation point of turbulent boundary layers, by Neal Tetervin and Chia Chiao Lin [No. 1046], p. 1067 , A lift-cancellation technique in linearized supersonic-wing theory, by Harold Mirels [No. 1004], p. 65 , A numerical method for the stress analysis of stiffened-shell structures under nonuniform temperature distributions, by Richard R. Heldenfels [No. 1043], p. 1019 , A recurrence matrix solution for the dynamic response of aircraft in gusts, by John C. Houbolt [No. 1010], p. 145 , A small-deflection theory for curved sandwich plates, by Manuel Stein and J. Mayers [No. 1008], p. 129 , A study of effects of viscosity on flow over slender inclined bodies of revolution, by H. Julian Allen and Edward W. Perkins [No. 1048.], p. 1103 , A study of the use of experimental stability derivatives in the calculation of the lateral disturbed motions of a swept-wing airplane and comparison with flight results, by John D. Bird and Byron M. Jaquet [No. 1031], p. 709 , A summary of lateral-stability derivatives calculated for wing plan forms in supersonic flow, by Arthur L. Jones and Alberta Alksne [No. 1052], p. 1211 , A theoretical analysis of the effect of time lag in an automatic stabilization system on the lateral oscillatory stability of an airplane, by Leonard Sternfield and Ordway B. Gates, Jr. [No. 1018], p. 291 , An analysis of base pressure at supersonic velocities and comparison with experiment, by Dean R. Chapman [No. 1051], p. 1187 , Analysis of means of improving the uncontrolled lateral motions of personal airplanes, by Marion O. McKinney, Jr. [No. 1035], p. 795 , Analysis of plane-plastic-stress problems with axial symmetry in strain-hardening range, by M.H. Lee Wu [No. 1021], p. 359 , Analysis of the effects of boundary-layer control on the take-off and power-off landing performance characteristics of a liaison type of airplane, by Elmer A. Horton, Laurence K. Loftin, Jr., Stanley F. Racisz, and John H. Quinn, Jr. [No. 1057], p. 1353 , Analysis of thrust augmentation of turbojet engines by water injection at compressor inlet including charts for calculating compression processes with water injection, by E. Clinton Wilcox and Arthur M. Trout [No. 1006], p. 97 , Analysis of turbulent free-convection boundary layer on flat plate, by E.R.G. Eckert and Thomas W. Jackson [No. 1015], p. 255 , Analytical determination of coupled bending-torsion vibrations of cantilever beams by means of station functions, by Alexander Mendelson and Selwyn Gendler [No. 1005], p. 77 , Buckling of thin-walled cylinder under axial compression and internal pressure, by Hsu Lo, Harold Crate, and Edward B. Schwartz [No. 1027], p. 647 , Calculation of the lateral control of swept and unswept flexible wings of arbitrary stiffness, by Franklin W. Diederich [No. 1024], p. 413 , Comparison between theory and experiment for wings at supersonic speeds, by Walter G. Vincenti [No. 1033], p. 757 , Comparison of theoretical and experimental heat-transfer characteristics of bodies of revolution at supersonic speeds, by Richard Scherrer [No. 1055], p. 1301 , Compressive strength of flanges, by Elbridge Z. Stowell [No. 1029], p. 675 , Correlation of physical properties with molecular structure for some dicyclic hydrocarbons having high thermal-energy release per unit volume, by P.H. Wise, K.T. Serijan, and I.A. Goodman [No. 1003], p. 55 , Diffusion of chromium in alpha cobalt-chromium solid solutions, by John W. Weeton [No. 1023], p. 397 , Dynamics of a turbojet engine considered as a quasi-static system, by Edward W. Otto and Burt L. Taylor, III [No. 1011], p. 177 , Effect of aspect ratio on the air forces and moments of harmonically oscillating thin rectangular wings in supersonic potential flow, by Charles E. Watkins [No. 1028], p. 657 , Effect of tunnel configuration and testing technique on cascade performance, by John R. Erwin and James C. Emery [No. 1016], p. 263 , Effects of wing flexibility and variable air lift wing bending moments during landing impacts of a small seaplane, by Kenneth F. Merten and Edgar B. Beck [No. 1013], p. 221 , Equations and charts for the rapid estimation of hinge-moment and effectiveness parameters for trailing-edge controls having leading and trailing edges swept ahead of the mach lines, by Kennith L. Goin [No. 1041], p. 937 , Experimental and theoretical studies of area suction for the control of the laminar boundary layer on an NACA 64A010 airfoil, by Albert L. Braslow, Dale L. Burrows, Neal Tetervin, and Fioravante Visconti [No. 1025], p. 433 , Experimental investigation of the effect of vertical-tail size and length and of fuselage shape and length on the static lateral stability characteristics of a model with 45 [degree] sweptback wing and tail surfaces, by M.J. Queijo and Walter D. Wolhart [No. 1049], p. 1117 , Experimental investigation of the effects of viscosity on the drag and base pressure of bodies of revolution at a mach number of 1.5, by Dean R. Chapman and Edward W. Perkins [No. 1036], p. 805 , Formulas for the supersonic loading, lift, and drag of flat swept-back wings with leading edges behind the mach lines, by Doris Cohen [No. 1050], p. 1146 , General method and thermodynamic tables for computation of equilibrium composition and temperature of chemical reactions, by Vearl N. Huff, Sanford Gordon, and Virginia E. Morrell [No. 1037], p. 829 , Horizontal tail loads in maneuvering flight, by Henry A. Pearson, William A. McGowan, and James J. Donegan [No. 1007], p. 117 , Influence of chemical composition on rupture properties at 1200 [degrees] F. of forged chromium-cobalt-nickel-iron base alloys in solution-treated and aged condition, by E.E. Reynolds, J.W. Freeman, and A.E. White [No. 1058], p. 1385 , Integrals and integral equations in linearized wing theory, by Harvard Lomax, Max A. Heaslet, and Franklyn B. Fuller [No. 1054], p. 1267 , Investigation of frequency-response characteristics of engine speed for a typical turbine-propeller engine, by Burt L. Taylor, III, and Frank L. Oppenheimer [No. 1017], p. 279 , Investigation of fretting by microscopic observation, by Douglas Godfrey [No. 1009], p. 135 , Investigation of separation of the turbulent boundary layer, by G.B. Schubauer and P.S. Klebanoff, National Bureau of Standards [No. 1030], p. 689 , Investigation of spoiler ailerons for use as speed brakes or glide-path controls on two NACA 65 series wings equipped with full-span slotted flaps, by Jack Fischel and James M. Watson [No. 1034], p. 769 , Investigation of the NACA 4-(5)(08)-03 and NACA 4-(10)(08)-03 two-blade propellers at forward mach numbers to 0.725 to determine the effects of camber and compressibility on performance, by James B. Delano [No. 1012], p. 189 , Investigation of turbulent flow in a two-dimensional channel, by John Laufer, California Institute of Technology [No. 1053], p. 1247 , Measurements of average heat-transfer and friction coefficients for subsonic flow of air in smooth tubes at high surface and fluid temperatures, by Leroy V. Humble, Warren H. Lowdermilk, and Leland G. Desmon [No. 1020], p. 343 , NACA investigation of fuel performance in piston-type engines, by Henry C. Barnett [No. 1026], p. 453 , On the particular integrals of the Prandtl-Busemann iteration equations for the flow of a compressible fluid, by Carl Kaplan [No. 1039], p. 909 , Relation between inflammables and ignition sources in aircraft environments, by Wilfred E. Scull [No. 1019], p. 303 , Some effects of nonlinear variation in the directional-stability and damping-in-yawing derivatives on the lateral stability of an airplane, by Leonard Sternfield [No. 1042], p. 1009 , Spectra and diffusion in a round turbulent jet, by Stanley Corrsin and Mahinder S. Uberoi, Johns Hopkins University [No. 1040], p. 915 , Study of effects of sweep on the flutter of cantilever wings, by J.G. Barmby, H.J. Cunningham, and I.E. Garrick [No. 1014], p. 229 , Supersonic flow around circular cones at angles of attack, by Antonio Ferri [No. 1045], p. 1055 , Table of contents, p. II , Temperature distribution in internally heated walls of heat exchangers composed of non-circular flow passages, by E.R.G. Eckert and George M. Low [No. 1022], p. 381 , The method of characteristics for the determination of supersonic flow over bodies of revolution at small angles of attack, by Antonio Ferri [No. 1044], p. 1039 , The stability of the compression cover of box beams stiffened by posts, by Paul Seide and Paul F. Barrett [No. 1047], p. 1087 , Theoretical antisymmetric span loading for wings of arbitrary plan form at subsonic speeds, by John DeYoung [No. 1056], p. 1317 , Wind-tunnel investigation of air inlet and outlet openings on a streamline body, by John V. Becker [No. 1038], p. 887 , © 2008 by NewsBank, Inc. All rights reserved

Language: English

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Format: Online-Ressource (viii, 197 p.) , 23 cm

Content: "The Midcentury White House Conference on Children and Youth bases its concern for children on the primacy of spiritual values, democratic practice, and the dignity and worth of every individual. Accordingly, the purpose of the Conference shall be to consider how we can develop in children the mental, emotional, and spiritual qualities essential to individual happiness and to responsible citizenship, and what physical, economic, and social conditions are deemed necessary to this development. To do this the Conference shall: (a) bring together in usable form pertinent knowledge related to the development of children and indicate areas in which further knowledge is needed; (b) examine the environment in which children are growing up, with a view to determining its influence upon them; (c) study the ways in which the home, the school, the church, the law, health and welfare agencies, and other social institutions, individually and cooperatively, are serving the needs of children; (d) formulate, through cooperative efforts of laymen and specialists, proposals for the improvement of parental, environmental, and institutional influences on children; (e) suggest means whereby these proposals may be communicated to the people and put into action"--Book. (PsycINFO Database Record (c) 2014 APA, all rights reserved)

Note: Published in 1950 under title: For every child a healthy personality. - Electronic reproduction; Washington, D.C; American Psychological Association; 2014; Available via World Wide Web; Access limited by licensing agreement; s2014 dcunns

Language: English

Keywords: Konferenzschrift

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