Th. Von Kármán's Advances in Aeronautical Sciences. Proceedings of the Second PDF

By Th. Von Kármán

ISBN-10: 0080065503

ISBN-13: 9780080065502

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Extra info for Advances in Aeronautical Sciences. Proceedings of the Second International Congress in the Aeronautical Sciences, Zürich, 12–16 September 1960

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Les propriétés du gaz de Lighthill ont été étudiées à l'équilibre par Lighthill(50) lui même, et hors d'équilibre par Freemann (22) . A la suite de ces deux auteurs, ce schéma commode a été utilisé avantageusement dans plusieurs études (2ï 4 ' 2 2 } 49). II—APPROXIMATION NEWTONIENNE Lorsque la couche de choc, comprise entre l'onde de choc et l'obstacle, est très mince, on peut faire usage d'une méthode d'investigation connue sous le nom d'approximation newtonienne. Avant de discuter les principes généraux de sa mise en oeuvre, il en faut discuter les conditions générales de validité.

It is given by the integral: φ= ' "- IIIdqi 'aq* ' — ■dq™ 'dpi 'dp2 ' ··· * dp ™ which can be divided into a spatial factor Φ'5Ρ= . . -dî8N and a momentum factor ^mom = ... / / / Φ ι * àp2 · ... · άρ3Ν as coordinates and momenta are independent.

F. and HORNIG, D . E . , / . Chem. Phys. 21, (1953), 617. 20. SHERMAN, F. , Low Density Wind-Tunnel Study of Shock-Wave Structure and Relaxation Phenomena in Gases. NACA T N 3298 (1955). 21. PATTERSON, G. , Molecular Flow of Gases. J. Wiley and Sons Ltd. New York, 1956. 113. 22. MOTT-SMITH, H. , The Solution of the Boltzmann Equation for a Shock-Wave. Physical Review 82, (1951), 885. 23. , Ueber thermische Effekte in Resonanzrohren. Mitteilungen aus dem Institut für Aerodynamik ETH. N r 21 (1954), 18-35.

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Advances in Aeronautical Sciences. Proceedings of the Second International Congress in the Aeronautical Sciences, Zürich, 12–16 September 1960 by Th. Von Kármán


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