Experimental hypersonic flow research in Europe

JSME International Journal, Series B: Fluids and Thermal Engineering

Volumn 41, Issue 2, 1998, Pages 397-407

  Groenig, Hans ^a   Olivier, Herbert ^a  

^a RWTH AACHEN UNIVERSITY   (Germany)

Author keywords

Experimental technique; High enthalpy; Model testing; Wind tunnels

Indexed keywords

ENTHALPY; EXPERIMENTS; MATHEMATICAL MODELS; TECHNOLOGY; WIND TUNNELS;

MODEL TESTING;

HYPERSONIC FLOW;

ENTHALPY; HYPERSONIC FLOW; WIND TUNNEL;

EID: 0032071222     PISSN: 13408054     EISSN: None     Source Type: Journal    
DOI: 10.1299/jsmeb.41.397     Document Type: Article

References (23)

1. Wendt, J.F. and Muylaert, J.M., Status of Hypersonic Testing Capabilities in Europe, Proceedings of 2nd European Symposium on Aerothermodynamics for Space Vehicles, ESA SP-367 (1995), p. 165.
2. Johnson, R.H., A Hypersonic Helium Tunnel for Mach Numbers above Twenty, GE Res. Lab., Report No. 58-RL-2089, 1958.
3. Bloxsom, D.E.Jr., Physics of High Temperature, High Pressure Gas Sources, AEDC-TN-56-17, 1956.
4. Resler, E.L., Lin, S.C. and Kantrowitz, A., The Production of High Temperature Gases in Shock Tubes, J. Appl. Phys., Vol.23 (1952), p. 1390.
5. Hollyer, R.N., Hunting, A.C., Laporte, O., Schwarcz, E.N. and Turner, E.B., Luminous Effects in the Shock Tube, Phys. Rev., Vol. 87 (1952), p. 911.
6. Hertzberg, A., A Shock Tube Method for Generating Hypersonic Flows, J. Aero. Sei., Vol. 18 (1951), p. 803.
7. Hertzberg, A., Wittliff, Ch.E. and Hall, J.G., Summary of Shock Tunnel Development and Application to Hypersonic Research, Cornell Aeron. Lab., AFOSR TR 60-139, 1961.
8. Stalker, R.J., Development of a Hypervelocity Wind Tunnel, J. Roy. Aeron. Soc., Vol. 76 (1972), p. 376.
9. Itoh, A., Design and Construction of HIEST (High Enthalpy Shock Tunnel), NAL Research Progress, NAL, Abe, M., Nayuki, T., Yoshida, M. and Matsuo, Y. (Editors) (1996), p.20.
10. Arnold, J. and Wendt, J.F., Test Facilities. Hypersonic Experimental and Computational Capability, Improvement and Validation, AGARD Advisory Report 319, Vol. I, Serie W.S., Muylaert, J. and Dujarric, Ch. (Editors) (1996), Chapter VÜI.
11. Stalker, R.J., A Mass Flux Probe to Use in Short Duration Hypersonic Flows. The High Temperature Aspects to Hypersonic Flow, Nelson, W.C. (Editor) (1964), p. 271, Pergamon Press, Oxford.
12. Störkmann, V., Olivier, H., Grönig, H. and Paris, S., Force Measurements on ELAC la and on a Reentry Capsule in Short Duration Hypersonic Facilities, Presented at the 21st International Symposium on Shock Waves, Great Keppel Island, Australia, 1997.
13. Nagamatsu, H.T., Geiger, R.E. and Sheer, R.R., Real Gas Effects in Flow over Blunt Bodies at Hypersonic Speed, J. Aeron. Sei., Vol.27 (1960), p. 241.
14. Olivier, H., Kindl, H., Zhao, H., Muylaert, J., Wong, H. and Walpot, L., Conventional Flow Diagnostics in Shock Tunnels, Presented at the 21st International Symposium on Shock Waves, Great Keppel Island, Australia, 1997.
15. Krek, R.M., Eitelberg, G. and Beck, W.H., Hyperboloid Flare Experiments in the HEG, Proceedings of 20th International Symposium on Shock Waves, Sturtevant, B., Shepherd, J.E. and Hornung, H.G. (Editors) (1997), p. 185, World Scientific Publishing.
16. Wollenhaupt, M., Rosenhauer, T., Müller, T., . Beck, W.H. and Scheer, M., Spatially and Spectrally Resolved Laser-Induced Fluorescence Measurements in the HEG, Proceedings of 20th International Symposium on Shock Waves, Sturtevant, B., Shepherd, J.E. and Hornung, H.G. (Editors) (1997), p. 281, World Scientific Publishing.
17. Olivier, H., Grönig, H. and Le Bozec, A., Hypersonic Model Testing in a Shock Tunnel, AIAA J., Vol.33 (1995), p. 262.
18. Koschel, W.W., Hypersonic Educational Activities in German Universities, AIAA Paper, No. 956141, 1995.
19. Olivier, H., Schulte-Rödding, J.-H., Grönig, H. and Vetlutsky, V.N., Measurements with the ELAC 1 - Configuration at Mach 7, J. Flight Sei. and Space Res., Vol. 20 (1996), p. 53.
20. Vetlutsky, V.N., private communication.
21. Anfimov, N.A., Kislykh, V.V. and Krapivnoy, K. V., Nonisentropic Multicascade Gas Compression in Piston Gas Dynamic Units (PGU) U-ll and RHYFL-Development Outlook, ZFW, Vol.16, No.3 (1992), p. 169.
22. Anonymous, Wind Tunnel AT 303, Institute of Theoretical and Applied Mechanics, Siberian Branch of the Russian Academy of Sciences, International Center of Aerophysical Research, Novosibirsk.
23. Kharitonov, A.M., private communication, 1996.