Thrust augmentation with mixer/ejector systems

40th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2002, Pages

  Presz Jr , Walter M ^a   Reynolds, Gary ^b   Hunter, Craig ^c  

^a WESTERN NEW ENGLAND UNIVERSITY   (United States)

^b Stage III Technologies   (United States)

^c NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 57749117126     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (19)

1. Heiser, William H., Thrust Augmentation, ASME Paper #66-GT-l 16, 1966.
2. Presz, W., Morin B., and Gousy, R., Forced Mixer Lobes in Ejector Designs, Paper No. 86-1614, AIAA 22nd Joint Propulsion Conference, June, 1986.
3. Presz, W., Morin, B., and Blinn, R, Short Efficient Ejector Systems, Paper No. 87-1837, AIAA 23rd Joint Propulsion Conference, June, 1987.
4. Skebe, S., McCormick, D., and Presz, W., Parameter Effects on Mixer-Ejector Pumping Performance, Paper No. 88-7018, AIAA 26th Aerospace Science Meeting, January, 1988.
5. Tillman, G., and Presz, W., Thrust Characteristics of a Supersonic Mixer Ejector, Paper No. 93-4345, 15th AIAA Aeroacoustical Conference, October, 1993.
6. Presz, W., Reynolds, G. and McMormick, D., Thrust Augmentation Using Mixer / Ejector / Diffuser Systems, Paper No. 94-0020, AIAA 32-Aerospace Science Meeting, January 1994.
7. Presz, W., Mixer/Ejector Noise Suppressors, Paper No. 91-2243, AIAA 27th Joint Propulsion Conference, June, 1991.
8. Presz, W. and Reynolds, G., Alternating Lobed Mixer/Ejector Concept Suppressor, ALMEC Suppressor, United States Patent 5,884,472, March, 1999
9. Presz, W., and Greitzer, E., A Useful Similarity Principle for Jet Engine Exhaust System Performance, Paper No. 88-3001, AIAA 24th Joint Propulsion Conference, July 1988.
10. Hoerner, S.F., Fluid Dynamic Drag, published by author, Library of Congress No. 64,19666, 1965.
11. Bernstein, A., Heiser, W. and Hevenor, C., Compound Compressible Nozzle Flow, Paper No. 66-663, AIAA 2nd Propulsion Joint Specialist Conference, June, 1966.
12. Presz, W and Zecca J., Application of Multi-Stage Hyper-Mixers to Combustors, Final Report, FTS/NASA SBIR Contract NAS3-98069, August, 1998.
13. Kozlowski, H. and Larkin, M., Energy Efficient Engine Exhaust Mixer Model Technology Report, NASA Report No. NASA-CR-165459, June, 1981.
14. Pao, S.P., and Abdol-Hamid, K.S., Numerical Simulation of Jet Aerodynamics Using a Three Dimensional Navier Stokes Method (PAB3D), NASA TP-3596, September 1996.
15. Abdol-Hamid, K.S. Implementation of Algebraic Stress Models in a General 3-D Navier-Stokes Method (PAB3D), NASA CR-4702, December 1995.
16. Abdol-Hamid, K.S., Lakshmanan, B., and Carlson, J.R., Application of the Navier-Stokes Code PAB3D with k-e Turbulence Models to Attached and Separated Flows, NASA TP-3480, January 1995.
17. Carlson, J.R., High Reynolds Number Analysis of Flat Plate and Separated Afterbody Flow Using Non-Linear Turbulence Models, AIAA 96-2544, July 1996.
18. Hunter, C.A., Experimental, Theoretical, and Computational Investigation of Separated Nozzle Flows, AIAA 98-3107, July 1998.
19. Hunter, C.A. and Deere, K.A., Computational Simulation of Fluidic Counterflow Thrust Vectoring, AIAA 99-2669, June 1999.