Characterization of thrust augmentation by unsteady ejectors

39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2003, Pages

  Gröschel, Elmar ^a   Tsuei, Hsin Hua ^a   Xia, Guoping ^a   Merkle, Charles L ^a  

^a UNIVERSITY OF TENNESSEE SPACE INSTITUTE   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL MODEL; PERIODIC BEHAVIOR; PHYSICAL MECHANISM; PULSED DETONATION ENGINE; REPETITION RATE; SHOCK DYNAMICS; THRUST AUGMENTATION; UNSTEADY EFFECTS;

INLET FLOW; PROPULSION;

EJECTORS (PUMPS);

EID: 84897746520     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (12)

1. nd Aerospace Sciences Meeting and Exhibit, January 10-13, 1994, Reno, NV.
2. Tillman, T. G. and Presz, W. M., "Thrust Characteristics of a Supersonic Mixer Ejector, " Journal of Propulsion and Power, Vol. 11, No. 5, September-October, 1995, pp. 931-937.
3. Heiser, W. H., and Pratt, D. T., "Hypersonic Airbreathing Propulsion, " AIAA Education Series, AIAA, Washington, D. C., 1994.
4. Kailasanath, K., "Review of Propulsion Applications of Detonation Waves, " AIAA Journal, Vol. 38, No. 9, September, 2000, pp. 1698-1708.
5. th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 7-10 July 2002, Indianapolis, Indiana.
6. th Aerospace Sciences Meeting and Exhibit, 6-9 January 2003, Reno, NV.
7. st Aerospace Sciences Meeting and Exhibit, 6-9 January, 2003, Reno, NV.
8. th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 7-10 July 2002, Indianapolis, Indiana.
9. th Aerospace Sciences Meeting and Exhibit, Reno, Nevada, January 14-17, 2002.
10. th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 7-10 July 2002, Indianapolis, Indiana.
11. st Aerospace Sciences Meeting and Exhibit, 6-9 January 2003, Reno, Nevada.
12. rd AIAA Fluid Dynamics Conference and Exhibit, Orlando, FL, June 23-26, 2003.