Approximate bridging relations in the transitional regime between continuum and free-molecule flows

Journal of Spacecraft and Rockets

Volumn 8, Issue 1, 1971, Pages 35-40

  Mattin, Fred W ^a  

^a NASA AMES RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS, HEAT TRANSFER; JSCRA; RE-ENTRY; SPACE VEHICLES;

EID: 0014974457     PISSN: 00224650     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.30214     Document Type: Article

References (14)

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2. Matting, F. W. and Chapman, D. R., "Analysis of Surface Ablation of Noncharring Materials with Description of Associated Computing Program," TN D-3758, 1966, NASA
3. Vidal, R. J. and Bartz, J. A., "Experimental Studies of Low- Density Effects in Hypersonic Wedge Flows," Advances in Applied Mechanics, Supplement 3, Vol. I, 1965, Rarefied Gas Dynamics, Fourth Symposium, edited by J. H. de Leeuw, Academic Press, New York, pp. 467-486
4. Page, L., Introduction to Theoretical Physics, 2nd ed., Van Nostrand, N.Y., 1935
5. Abramowitz, M. and Stegun, I. A., Handbook of Mathematical Functions with Formulas, Graphs, and Mathematical Tables, U.S. Department of Commerce, National Bureau of Standards Applied Mathematics Series 55, Washington, D.C., June 1964
6. Ferri, A. and Zakkay, V., "Measurements of Stagnation Point Heat Transfer at Low Reynolds Numbers," Journal of the Aerospace Sciences, Vol. 29, No. 7, July 1962, pp. 847-850
7. Kennard, E. H., Kinetic Theory of Gases, McGraw-Hill, New York, 1938
8. Detra, R. W., Kemp, N. H., and Riddell, F. R., "Addendum to Heat Transfer to Satellite Vehicles Reentering the Atmosphere," Jet Propulsion, Vol. 27, No. 12, Dec. 1957, pp. 1256-1257
9. Cheng, H. K., "Viscous Hypersonic Blunt-Body Problems and the Newtonian Theory," Proceedings of the International Symposium on Fundamental Phenomena in Hypersonic Flow, edited by J. Gordon Hall, 1966, Cornell University Press, Ithaca, N.Y., pp. 90-132
10. Sherman, F. S., "A Survey of Experimental Results and Methods for the Transition Regime of Rarefied Gas Dynamics," Advances in Applied Mechanics, Supplement 2, Vol. II, 1963, Rarefied Gas Dynamics, Third Symposium, edited by J. A. Laurmann, Academic Press, New York, pp. 228-260
11. Yang, H.-T. and Lees, L., "Plane Couette Flow at Low Mach Number According to the Kinetic Theory of Gases," Proceedings of the Fifth Midwestern Conference on Fluid Mechanics, The Engineering Research Institute, 1957, pp. 41-65
12. Masson, D. J., Morris, D. N., and Bloxsom, D. E., "Measurements of Sphere Drag from Hypersonic Continuum to Free- Molecule Flow," Advances in Applied Mechanics, Supplement 1, 1961, Rarefied Gas Dynamics, Second Symposium, edited by L. Talbot, Academic Press, New York, pp. 643-661
13. Rott, N. and Whittenbury, C. G., "A Flow Model for Hypersonic Rarefied Gas Dynamics with Applications to Shock Structure and Sphere Drag," Rept. SM-38524, May 1961, Douglas Aircraft
14. Wegener, P. P. and Ashkenas, H., "Wind Tunnel Measurements of Sphere Drag at Supersonic Speeds and Low Reynolds Numbers," Journal of Fluid Mechanics, Vol. 10, Pt. 4, June 1961, pp.550-560