Testing of a scramjet engine with a strut in M8 flight conditions

34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 1998, Pages

  Tomioka, Sadatake ^a,b   Kanda, Takeshi ^a,b   Tani, Kouichiro ^a,b   Mitani, Tohru ^a,b   Shimura, Takashi ^a,b   Chinzei, Nobuo ^a  

^a KAKUDA RESEARCH CENTER   (Japan)

^b Ramjet System Section   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; COMBUSTION; COMBUSTORS; ENGINES; FUELS; PROPULSION; STRUTS;

BOUNDARY-LAYER COMBUSTION; FLIGHT CONDITIONS; FUEL FLOW RATES; FUEL INJECTORS; PREDICTION METHODS; PRESSURE INCREMENTS; SCRAMJET ENGINES; TOTAL TEMPERATURES;

RAMJET ENGINES;

EID: 85088057017     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-3134     Document Type: Conference Paper

References (12)

1. F. S. Billig, “Inlet-combustor Interface Problems in Scramjet Engines,” 1st ISABE, June 1972.
2. G. B. Northam, “Supersonic Combustion Ramjet Research at Langley,” AIAA paper 86-0159, 1986.
3. T. Saito, et al., “Mach 8 Testing of a Scramjet Engine Model,” ISTS paper 96-a-2-11, 1996.
4. T. Kanda, et al., “Mach 8 Testing of a Scramjet Engine Model,” submitted to the 37th Aerospace Sciences Meetings and Exhibit.
5. T. Kanda, et al., “Mach 6 Testing of a Scramjet Engine Model,” Journal of Propulsion and Power, Vol. 13, No. 4, pp. 543-551, 1997.
6. T. Mitani, et al., “Comparison of Scramjet Engine Performance in Mach 6 Vitiated and Storage-Heated Air,” Journal of Propulsion and Power, Vol. 13, No. 5, pp. 635-642, 1997.
7. S. Sato et al., “Scramjet Engine Test at Mach 6 Flight Condition,” AIAA paper 97-3021, 1997.
8. T. Sunami, et al., “Mach 4 Tests of a Scramjet Engine - Effects of Isolator,” ISABE paper 97-7088, 1997.
9. S. Tomioka, et al., “Auto Ignition in a Supersonic Combustor with Perpendicular Injection behind Backward- Facing Step,” AIAA paper 97-2889, 1997.
10. F. S. Billig, “Research on Supersonic Combustion,” Journal of Propulsion and Power, Vol. 9, No. 4, pp. 499-514, 1993.
11. P. J. Waltrup and F. S. Billig, “Prediction of Precombustion Wall Pressure Distributions in Scramjet Engines,” Journal of Spacecraft and Rocket, Vol. 19, No. 9, pp. 620-622, 1973.
12. G. Sullins and G. McLafferty, “Experimental Results of Shock Trains in Rectangular Ducts,” AIAA paper 92-5103, 1992.