Testing of a scramjet engine model in mach 6 vitiated air flow

35th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1997, Pages

  Hiraiwa, Tetsuo ^a,b   Sato, Shigeru ^a,b   Tomioka, Sadatake ^a,b   Kanda, Takeshi ^a,b   Shimura, Takashi ^a,b   Mitani, Tohru ^a,b  

^a National Aerospace Laboratory Kakuda Research Center   (Japan)

^b Ramjet Propulsion Research Division   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; AIR; COMBUSTION; ENGINES; FLOW RATE; FUELS; WALL FLOW; WATER VAPOR;

COMBUSTION PATTERNS; ENGINE PERFORMANCE; FLIGHT CONDITIONS; FUEL FLOW RATES; GAS TEMPERATURE; IGNITION CHARACTERISTICS; MAXIMUM HEAT FLUX; SCRAMJET ENGINES;

HEAT FLUX;

EID: 84983109652     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)

1. Yatsuyanagi, N., et al, "Initial Tests of a Sub-Scale Scramjct Engine," 12th ISABE, Melbourne, Australia, 1995.
2. Kanda, T., "Mach 6 Testing of a Scramjet Engine Model," AIAA paper 96-0380, 1996.
3. Tomioka, S., et al., AIAA paper 96-3240, 1996.
4. Saito, T., et al., 20th ISTS, 96-a-2-11, 1996.
5. Beach, H. L., AIAA paper 72-1179, 1972.
6. Srinivasan. S., AIAA paper 96-2719, 1995.
7. Mitani, et al., "Scramjet Engine Testing in Mach 6 Vitiated Air,1" AIAA paper 96-4555, 1996.
8. Hiraiwa, et al., 20th ISTS paper 96-d-14, 1996.