By Th. Von Kármán
Advances in Aeronautical Sciences, quantity 1 comprises the lawsuits of the 1st overseas Congress within the Aeronautical Sciences, held in Madrid, Spain in September 1958.
The e-book is produced from survey papers and unique contributions that debate universal difficulties in aeronautics and in house expertise. The reader also will locate attention-grabbing articles that disguise themes at the rules of inertial advice; boundary layer keep watch over; VTOL/STOL airplane; warmth resisting fabric; warmth move and warmth barrier; and jet noises and human elements in aeronautics. Hypersonic speeds; propulsion tools in area and magneto-fluid dynamics are mentioned as well.
Aeronautics engineers and scientists in allied fields will locate the publication insightful.
Read Online or Download Advances in Aeronautical Sciences. Proceedings of the First International Congress in the Aeronautical Sciences, Madrid, 8–13 September 1958 PDF
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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
C. Lin for their assistance in collecting the material treated in this lecture. Professor Libby collected the papers dealing with supersonic wing theory, slender aircraft, inter ference effects, higher approximations, hypersonic flow and boundary layer theory, C. C. Lin those dealing with the theory of turbulence. The choice of authors mentioned in the paper is somewhat arbitrary. I am also indebted to Professor Wallace D. Hayes for letting me have the galley proofs of his book on hypersonic flow written jointly with R.
S. Tsien brought these considerations into closer contact with the physics of gases as based on kinetic theory. At speeds approaching 20,000 feet per second, we may of course dis pense with aerodynamic lift for cruising. However, there are indications 48 Ml? ROBERT T . 0 LIFT-DRAG RATIO,^FIG. 11 Effect of lift—drag ratio on maximum deceleration for recovery of satellite. that aerodynamic forces however small will play an important role in recovery from purely dynamic orbits or trajectories. Figure 11, prepared from calculations made by D.
490, 1951. W . HEISENBERG, Z u r Statistischen T h e o r i e der T u r b u l e n z , Z. , Vol. 124, p . 628, 1948. J. K A M P É DE F É R I È T , C. R. Acad. , Paris, Vol. 227, p . 760, 1948. T . VON K A R M Ä N and L . H O W A R T H , O n the Statistical T h e o r y of Isotropie T u r bulence, Proc. Roy. Soc, A, Vol. 164, p . 192, 1938. T . VON K A R M Ä N and C. C. L I N , O n the Concept of Similarity in t h e T h e o r y of Isotropie T u r b u l e n c e , Adv. Appl. , Vol. 2, p . 1, 1951. A.