Advances in Aeronautical Sciences. Proceedings of the First by Th. Von Kármán

By Th. Von Kármán

Advances in Aeronautical Sciences, quantity 1 includes the complaints of the 1st foreign Congress within the Aeronautical Sciences, held in Madrid, Spain in September 1958.

The booklet is produced from survey papers and unique contributions that debate universal difficulties in aeronautics and in house expertise. The reader also will locate fascinating articles that hide issues at the ideas of inertial counsel; boundary layer regulate; VTOL/STOL plane; warmth resisting fabric; warmth move and warmth barrier; and jet noises and human components in aeronautics. Hypersonic speeds; propulsion tools in house and magneto-fluid dynamics are mentioned as well.

Aeronautics engineers and scientists in allied fields will locate the booklet insightful.

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Extra info for Advances in Aeronautical Sciences. Proceedings of the First International Congress in the Aeronautical Sciences, Madrid, 8–13 September 1958

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5, pp. 430-1, June 1954. S. M. BOGDONOFF and A. G. HAMMITT, Fluid Dynamic Effects at Speeds from M = 11 to 15, J. Aero. , Vol. 23, No. 2, pp. 108-116, February 1956. A. G. HAMMITT and S. M. BOGDONOFF, Hypersonic Studies of the Leading-Edge Effect on the Flow Over a Flat Plate, J. Amer. Rocket Soc, Vol. 26, No. 4, pp. 241-6, April 1956. F. K. MOORE, Three-Dimensional Boundary Layer Theory, Adv. Appl. , Vol. 4, pp. 159-228, Academic Press, 1956. E. RESHOTKO and I. E. BECKWITH, Compressible Laminar Boundary Layer over a Yawed Infinite Cylinder with Heat Transfer and Arbitrary Prandtl Number, NACA T N 3986, June 1957.

Technical Report N o . 54, February 1958. VI. Boundary Layer D . R. CHAPMAN and M . W. RUBESIN, Temperature and Velocity Profiles in the Compressible Laminar Boundary Layer with Arbitrary Distribution of Surface Temperature, J. Aero. , Vol. 16, N o . 9, pp. 547-65, September 1949. C. CROWN, T h e Laminar Boundary Layer at Hypersonic Speeds, N A V O R D Report 2299, 1952. G. B. W . Y O U N G and E. JANSSEN, T h e Compressible Boundary Layer, J. Aero. , Vol. 19, N o . 4, p p . 229-36, 288, April 1952.

1, p p . 6 7 - 8 , January 1957. A N O N , Conical C a m b e r , Aviat. Age, Vol. 24, N o . 2, p . 62, A u g u s t 1957. Some Significant Developments in Aerodynamics since 1946 27 II. Slender Wings and Aircraft H. S. T S I E N , Supersonic Flow over an Inclined Body of Revolution, J. Aero. , Vol. 5, pp. 4 8 0 - 3 , 1938. M. J. LIGHTHILL, Supersonic Flow Past Bodies of Revolution, A R C Reports and Memoranda 2003, 1945. J. B. BRODERICK, Supersonic Flow Round Pointed Bodies of Revolution, Quart.

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