Mach 8 testing of scramjet engine models

37th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1999, Pages

  Kanda, Takeshi ^a,b   Wakamatsu, Yoshio ^a,b   Ono, Fumiei ^a,b   Kudo, Kenji ^a,b   Murakami, Atsuo ^a,b   Izumikavva, Muneo ^a,b  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^b KAKUDA RESEARCH CENTER   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; BOUNDARY LAYERS; COMBUSTION; ENGINES; FUEL INJECTION; RAMJET ENGINES;

COMBUSTION CONDITION; COMBUSTION EFFICIENCIES; ENGINE GEOMETRY; FLIGHT CONDITIONS; LOW VELOCITY REGION; PRESSURE INCREASE; SCRAMJET ENGINES; SCRAMJET MODEL;

FUELS;

EID: 84983113526     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (24)

1. Yatsuyanagi, N., Chinzei, N., Mitani, T., Wakamatsu, Y, Masuya, G., Iwagami, S., Endo, M., and Hanus, G., “Ramjet Engine Test Facility (RJTF) in NAL-KRC, Japan,” AIAA paper 98-1511, 1998.
2. Saito, T., Wakamatsu, Y., Mitani, T., Chinzei, N., Shimura, T., and Kanda, T., “Mach 8 Testing of a Scramjet Engine Model,” Proceedings of the 20th International Symposium on Space Technology and Science, Vol. 1, Gifu, Japan, 1996, pp 58-63.
3. Tomioka, S., Kanda, T., Tani, K., Mitani, T., Shimura, T., and Chinzei, N., “Testing of a Scramjet Engine with a Strut at Mach 8 Flight Condition,” AIAA paper 98-3134, Jul 1998.
4. Hiraiwa, T., Mitani, T., Izumikawa, M., and Ono, F., “Calibration Studies of Nozzle Flow in Ramjet Engine Test Facility,” The Twentieth International Symposium on Space Technology and Science Paper 96-d-14, Gifu, Japan, May 1996.
5. Sato, S., Izumikawa, M., Tomioka, S., and Mitani, T, “Scramjet Engine Test at Mach 6 Flight Condition,” AIAA paper 97-3021, 1997.
6. Tani, K., Kanda, T, Sunami, T, Hiraiwa, T, and Tomioka, S., “Geometrical Effects to Aerodynamic Performance of Scramjet Engine,” AIAA paper 973018, 1997.
7. Mitani, T., Takahashi, M., Tomioka, S., Hiraiwa, T., and Tani, K., “Analyses and Application of Gas Sampling to Scramjet Engine Testing,” Journal of Propulsion and Power, in printing.
8. Tani, K., Kanda, T. and Tokunaga, T., “Starting Characteristics of Scramjet Inlets,” Proceedings of the Eleventh International Symposium on Air Breathing Engines, AIAA, Tokyo, Japan, 1993, pp 1071-1080.
9. Holden, M. S., “Shock Wave-Turbulent Boundary Layer Interaction in Hypersonic Flow,” AIAA paper 72-24, 1972.
10. Mitani, T. and Shimura, T., private communication, 1998.
11. Kanda, T., Hiraiwa, T., Mitani, T, Tomioka, S., and Chinzei, N., “Mach 6 Testing of a Scramjet Engine Model,” Journal of Propulsion and Power, Vol. 13, No.4, 1997, pp 543-551.
12. Beckwith, I. E., and Gallagher, J. J., “Local Heat Transfer and Recovery Temperature on a Yawed Cylinder at a Mach Number of 4.15 and High Reynolds Number,” NASA TR R-104, 1958.
13. Cohen, L. S., Coulter, L. J., and Egan, W. J., “Penetration and Mixing of Multiple Gas Jets Subjected to a Cross Flow,” AAIA Journal, Vol. 9, No. 4, 1971, pp 718-724.
14. Mitani, T., private communication, 1998.
15. Kodera, M., Nakahashi, K., Hiraiwa, T., Kanda, T., and Mitani, T., “Scramjet Inlet Flow Computations by Hybrid Grid Method,” AIAA paper 98-0962, Jan. 1998.
16. Heiser, W. H, Pratt, D. T., Daley, D. H, and Mehta, U. B., “Hypersonic Airbreathing Propulsion,” AIAA Education Series, AIAA, Washington, DC, 1994, pp 280-313
17. Waitz, I. A., Marble, F. E., and Zukoski, E. E., “Investigation of a Contoured Wall Injector for Hypervelocity Mixing Augmentation,” AIAA Journal, Vol. 31, No. 6, 1993, pp 1014-1021.
18. Tomioka, S., Izumikawa, M., Hiraiwa, T., and Sato, S., “Enhancement of Ignition Ability in a Model Scramjet Engine,” Proceedings of 20th International Symposium on Space Technology and Science, Vol. 1, Gifu, Japan, 1967 pp 76-81.
19. Zukoski, E. E., “Turbulent Boundary-Layer Separation in Front of a Forward-Facing Step,” AIAA Journal, Vol. 5, No. 10, 1967, pp 1746-1753.
20. Mager, A., “On the Model of the Free, Shock-Separated, Turbulent Boundary Layer,” Journal of Aeronautical Sciences, Vol. 23, 1956, pp 181-184.
21. Sunami, T., Sakuranaka, N., Tani, K., Hiraiwa, T., and Shimura, T., “Mach 4 Tests of a Scramjet Engine -Effect of Isolator,” Proceedings of 13lh International Symposium on Air Breathing Engines, Sep. 1997, pp 615-625.
22. Garrison, T. J, Settles, G. S., Narayanswami, N., and Knight, D. D., “Structure of Crossing-Shock-Wave/Turbulent-Boundary-Layer Interactions,” AIAA Journal, Vol. 31, No. 12, 1993, pp 2204-2211.
23. Sullins, G., and McLafferty, G., “Experimental Results of Shock Trains in Rectangular Ducts,” AIAA paper 92-5103, Dec 1992.
24. Komuro, T., Satoh, K., Kanda, T., and Tani, K., “Hysteretic Characteristics of Starting of Scramjet Inlets,” Proceedings of 34th Conference on Aerospace Propulsion, Jan 1994, pp 92-97. (in Japanese)