Experimental investigation of a pulse detonation engine with a 2D ejector

AIAA Paper

Volumn , Issue , 2004, Pages 9661-9676

  Allgood, Daniel ^a   Gutmark, Ephraim ^a   Rasheed, Adam ^b   Dean, Anthony J ^b  

^a 705 Engineering Research Center   (United States)

^b GE GLOBAL RESEARCH   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COHERENT STRUCTURE VELOCIMETRY (CSV); FLAME LUMINOSITY IMAGING; PULSE DETONATION ENGINE (PDE); SHOCK STRUCTURES;

AIR EJECTORS; CHEMICAL ANALYSIS; CORRELATION METHODS; INTAKE SYSTEMS; NOZZLES; QUENCHING; SENSITIVITY ANALYSIS; SPACECRAFT PROPULSION; VECTORS; VELOCITY MEASUREMENT;

SPACE RESEARCH;

EID: 2942717070     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (11)

1. Porter, J.L. and Squyers, R.A., "A Summary/Overview of Ejector Augmentor Theory and Performance," ATC Report No. R-91100/CR-47A, Vought Corporation Advanced Technology Center, Dallas, Texas, 1979.
2. th AIAA Joint Propulsion Meeting and Exhibit, Indianapolis, IN, July 7-10, 2002.
3. th AIAA Joint Propulsion Meeting and Exhibit, Indianapolis, IN, July 7-10, 2002.
4. Johnson, W.S. and Yang, T., "A Mathematical Model for the Prediction of the induced Flow in a Pulsejet Ejector with Experimental Verification", ASME Paper 68-WA/FE-33, 1968.
5. th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, January 14-17, 2002.
6. th AIAA Jet Propulsion Conference, Huntsville, Alabama, July 21-23, 2003.
7. th AIAA Jet Propulsion Conference, Huntsville, Alabama, July 21-23, 2003.
8. th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, January 14-17, 2002.
9. th AIAA Joint Propulsion Meeting, Indianapolis, IN, July 7-10, 2002.
10. th AIAA Jet Propulsion Conference, Huntsville, Alabama, July 21-23, 2003.
11. th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Indianapolis, IN July 7-10, 2002.