Aerodynamic performances of a combined cycle inlet

Journal of Propulsion and Power

Volumn 22, Issue 4, 2006, Pages 900-904

  Kubota, Shinji ^a,c,d   Tan, Kouichiro ^b,e,f   Masuya, Goro ^a,c,f  

^a TOHOKU UNIVERSITY   (Japan)

^b JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^c Department of Aerospace Engineering ^*  (Japan)

^d TOSHIBA CORPORATION   (Japan)

^e Engine System Subgroup   (Japan)

^f AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; BOUNDARY LAYERS; INTAKE SYSTEMS; JET ENGINES; SHRINKAGE;

AERODYNAMIC PERFORMANCES; COMBINED CYCLE INLET; COWL LEADING EDGE; KANTROWITZ-DONALDSON LIMIT; RAMP-COMPRESSION-TYPE INLETS;

COMBINED CYCLE POWER PLANTS;

EID: 33746865303     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/1.17777     Document Type: Article

References (9)

1. Russell, D., and Corin, S., "Combined Rocket and Airbreathing Propulsion Systems for Space-Launch Applications," Journal of Propulsion and Power, Vol. 14, No. 5, 1998, pp. 605-612.
2. Kanda, T., and Kudo, K., "Cooling Requirement of the Combined Cycle Engine in Descending Flight," Proceedings of 24th International Symposium on Space Technology and Science, Japan Society for Aeronautical and Space Sciences and Organized Committee of 24th ISTS, Tokyo, 2004, pp. 39-44.
3. Koide, S, Griesel, C. J. W., and Stollery, J. L., "Correlation of Shock Angles Caused by Rhombic Delta Wing," AIAA Journal, Vol. 34, No. 9, 1996, pp. 1958-1960.
4. Crocco, L., "One-Dimensional Treatment of Steady Gas Dynamics," Fundamentals of Gas Dynamics, 2nd ed., edited by H. W. Emmons, Princeton Univ. Press. Princeton, NJ, 1967, pp. 184-190.
5. Van Wie, D. M., Kwok, F. T., and Walsh, R. F., "Starting Characteristics of Supersonic Inlet," AIAA Paper 96-2914, July 1996.
6. Mager, A., "On the Model of the Free, Shock-Separated, Turbulent Boundary Layer," Journal of the Aeronautical Sciences, Vol. 23, Feb. 1956, pp. 182-184.
7. Tani, K., Kanda, T., and Tokunaga, T., "Starting Characteristics of Scramjet Inlets," Proceedings of 11th ISABE, 1993, pp. 1071-1080.
8. Tani, K., Kanda, T., Kudo, K., Murakami, A., Komuro, T., and Itoh, K., "Aerodynamics Performance of Scramjet Inlet Models with a Single Strut," AIAA Paper 93-0741, Jan. 1993.
9. Waltrup, P. J., Billig, F. S., and Stockbridge, D., "Engine Sizing and Integration Requirements for Hypersonic Airbreathing Missile Applications," CP-307, AGARD, March 1982.