Preliminary assessment of exhaust systems for high Mach (4 to 6) fighter aircraft-Reference-Cited by-同舟云学术

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Preliminary assessment of exhaust systems for high Mach (4 to 6) fighter aircraft

Published:1989-07-12 Issue: Volume: Page:
ISSN:
Container-title:25th Joint Propulsion Conference
language:
Short-container-title:

Author:

KUCHAR A.¹,WOLF J.¹

Affiliation:

1. GE Aircraft Engines, Cincinnati, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1989-2356

Reference2 articles.

1. AIM-88-3069,"High Speed Airbreathing

2. AIM-87-2941."High Mach Propulsion System Installation and Exhaust System Design Considerations," D.J. Dusa. AIM-81-1490,"Development of Exhaust Nozzle Internal Perfomance Prediction Techniques for Advanced Aircraft Applications,"D.W.Speir,J.T. Blozy.

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1. Multi-objective nozzle design optimization for maximum thrust vectoring performance;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2022-06-09

2. Parametrical analysis of near-term air-breathing engine concepts for first stage space plane acceleration missions;36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2000-07-24

3. Nozzle design optimization by method-of-characteristics;26th Joint Propulsion Conference;1990-07-16

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