Experimental and computational wake structure study for a wide-angle cone

Journal of Spacecraft and Rockets

Volumn 33, Issue 4, 1996, Pages 476-482

  Danckert, A ^a,b   Legge, H ^a,b,c  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

^b Institute for Fluid Mechanics

^c AIAA ^*

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; DEGREES OF FREEDOM (MECHANICS); HYPERSONIC AERODYNAMICS; MATHEMATICAL MODELS; MOLECULAR DYNAMICS; MONTE CARLO METHODS; VORTEX FLOW; WIND TUNNELS;

MOLECULAR DISTRIBUTION FUNCTION; MOLECULAR NUMBER FLUXES; NONEQUILIBRIUM FLOW; PATTERSON PROBE MEASUREMENT; WIDE ANGLE CONE;

WAKES;

EID: 0030194337     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/3.26788     Document Type: Article

References (15)

1. Anon., Capsule Aerothermodynamics, edited by J. Muylaert, AGARD-FDP-VKI Lecture Series 1995-06, von Kármán Inst. for Fluid Dynamics, Rhode Saint Genèse, Belgium, March 1995.
2. Legge, H., "Experiments on a 70 Degree Blunted Cone in Rarefied Hypersonic Flow," AIAA Paper 95-2140, June 1995.
3. Kastell, D., Horvarth, T. J., and Eitelberg, G., "Recompression of Nonequilibrium Flow in the Wake of a Blunted Body," Proceedings of the 20th International Symposium on Shock Waves, edited by B. Sturtevant, World Scientific Publishing, Singapore (to be published).
4. Bird, G. A., Molecular Gas Dynamics and the Direct Simulation of Gas Flows, Oxford Univ. Press, Oxford, England, UK, 1994.
5. Moss, J. N., Price, J. M., Dogra, V. K., and Hash, D. B., "Comparison of DSMC and Experimental Results for Hypersonic External Flows," AIAA Paper 95-2028, June 1995.
6. Patterson, G. N., "Theory of Free-Molecule, Orifice-Type Pressure Probes in Isentropic and Nonisentropic Flows," Inst. of Aerophysics, Univ. of Toronto, UTIA Rept. 412, Toronto, ON, Canada, Nov. 1956.
7. Hughes, P. C., "Theory for the Free Molecular Impact Probe at an Arbitrary Angle of Attack," Inst. for Aerospace Studies, Univ. of Toronto, UTIAS Rept. 103, Toronto, ON, Canada, May 1965.
8. Koppenwallner, G., "The Free Molecular Pressure Probe with Finite Slot Orifice," Proceedings of the 14th Symposium on Rarefied Gas Dynamics, edited by Ed. H. Oguchi, Vol. 1, Univ. of Tokyo Press, Tokyo, Japan, 1984, pp. 415-422.
9. Legge, H., "Patterson Probe Measurements in the Wake of a 70 Deg Half Angle Cone in Hypersonic Rarefied Flow," German Aerospace Research Establishment, DLR-IB 223-94 A 15, Göttingen, Germany, Dec. 1994.
10. Bartz, J. A., and Vidal, R. J., "Experimental Study of Pseudo Transpiration at an Orifice in Rarefied Flow," Proceedings of the 6th Symposium on Rarefied Gas Dynamics, edited by L. Trilling and H. Y. Wachmann, Vol. 1, Academic, New York, 1969, pp. 639-653.
11. Legge, H., "Modelling Free Molecular Plume Flow and Impingement by an Ellipsoidal Distribution Function," Rarefied Gas Dynamics: Space-Related Studies, edited by E. P. Muntz, D. P. Weaver, and D. H. Campbell, Vol. 116, Progress in Astronautics and Aeronautics, AIAA, Washington, DC, 1989, pp. 189-203.
12. Koppenwallner, G., "The Free Molecular Pressure Probe with Finite Length Slot Orifice," German Aerospace Research Establishment, IB 222-84 A 15, Göttingen, Germany, May 1984.
13. Dietrich, S., and Boyd, I. D., "Parallel Implementation on the IBM SP-2 of the Direct Simulation Monte Carlo Method," AIAA Paper 95-2029, June 1995.
14. Borgnakke, C., and Larsen, P. S., "Statistical Collision Model for Monte Carlo Simulation of Polyatomic Gas Mixture," Journal of Computational Physics, Vol. 18, No. 4, 1995, pp. 405-420.
15. Bergemann, F., and Boyd, I. D., "New Discrete Vibrational Energy Model for the Direct Simulation Monte Carlo Method," Rarefied Gas Dynamics: Experimental Techniques and Physical Systems, edited by B. D. Shizgal and D. P. Weaver, Vol. 158, Progress in Astronautics and Aeronautics, AIAA, Washington, DC, 1994, pp. 174-183.