Разномодульная теория упругости - Амбарцумян С.А.
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Tunnels, NACA, L-74, 1946.
Rhode R. V., Correlation of Flight Data on Limit Pressure
Coefficients and Their Relation to High-Speed Burbling and
Critica
Tail Loads, NACA, L-269, 1946.
Stack John, Shock-Stalled Flows for Supersonic Type Airfoils at
Transonic Speeds, Sixth International Congress for Applied Mechanics,
1946, Paris.
Hilton W. F. and P r u d e n F. W., Subsonic and Supersonu. High-Speed
Tunnel Tests of a Faired Double-Wedge Aerofoil, R 8t M, No. 2057,
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L a i t о n e E. V., Exact and Approximate Solutions of Two-Dimensional
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p. 25, January 1947.
Du Mоnd J. W. M. et al., A Determination of the Wave Forms and Laws of
Propagation and Dissipation of Ballistic Shock Waves, Acoustical Soc.
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СВЕРХЗВУКОВАЯ АЭРОДИНАМИКА
Р f г i е ш Н., The Laws of Reflection of Two-Dimensional Pressure Waves
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Martin М. H., A Problem in the Propagation of Shock Quart. Appl. Math,
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G u d e r 1 у G., Starke kugelige und zylindrische Verdichtungsstosse in
der Nahe des Kugelmittelpunktes bzw. Zilinderachse, Luftfahr-forschung,
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Emmons H. W., Shock Waves in Aerodynamics, Journal of the Aeronautical
Sciences, vol. 12, No. 2, pp. 188-194, April 1945.
Charters A. C., Some Ballistic Contributions to Aerodynamics, Journal of
the Aeronautical Sciences, vol. 14, No. 3, p. 155, March 1947.
Smelt R., Longitudinal Stability and Trim Changes Through the Speed of
Sound, Sixth International Congress for Applied Mechanics, 1946, Paris.
Cope W. F., Calculation of Reynolds Number Effect on Projectiles at
Supersonic Speeds, Sixth International Congress for Applied Mechanics,
1946, Paris.
T s i e n H. S. and К u о Y. H., Two-Dimensional Irrotational Mixed
Subsonic and Supersonic Flow of a Compressible Fluid and the Upper
Critical Mach Number, NACA T. N., No. 995 May 1946.
T s i e n H. S., the "Limiting Line" in Mixed Subsonic and Supersonic
Flow of Compressible Fluids, NACA T. N., No. 961, 1944.
Molenbrok P., Ober einige Bewegungen eines Gases mit Annahme eines
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Tollmien W., Grenzlinien adiabatischer Potentialstromungen, ZAMM, Bd. 21,
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T s i e n H. S., Two-Dimensional Subsonic Flow of Compressible Fluids,
Journal of the Aeronautical Sciences, vol. 6, No. 10, pp. 399. ff.,
August 1939.
Lin С. C., On the Extension of the von Karman-Tsien Method to Two-
Dimensional Subsonic Flows with Circulation Around Closed Profiles,
Quart. Appl. Math., vol. 4, No. 3, October 1946.
Coburn N.. the Karman-Tsien Pressure-Volume Relation in the Two-
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ЛИТЕРАТУРА
91
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университета. Отд. Физ-Мат'., 1904, вып. 21, стр. 1-121. Перепеч. в
полном собр. трудов С. А. Чаплыгина, 1933, т. II, изд. АН СССР, М.- Л.
В е г s L., Velocity Distribution on Wing Sections of Arbitrary Shape in
Compressible Potential Flow, NACA T. N., No. 1006, 1946, также T. N., No.
1012, 1946.
Bergman S. A., On Two-Dimensional Flows of Compressible Fluids, NACA T.
N.. No. 972, 1945.
Bergman S., Methods for Determination and Computation of Flow Patterns of
a Compressible Fluid, NACA T. N., No. 1018, 71 p., September 1946.
Garrick I. E. and Kaplan C., On the Flow of a Compressible Fluid by the
Hodograph Method: I - Unification and Extension of Present-Day Results,
NACA, L-127, 41 p., March 1944;
II - Fundamental Set of Particular Flow Solutions of the Chaplygin
Differential Equation, NACA, L-147, November 1944.
Pinl М., Zur Theorie der kompessiblen Potentialstromungen, III. ZAMM, Bd.
22 S. 305-311, December 1942.
Busemann A., Die achsensymmetrische kegelige Oberschallstromung,
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