Performance Comparison of a Full-Length and a Truncated Aerospike Nozzle-Reference-Cited by-同舟云学术

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Performance Comparison of a Full-Length and a Truncated Aerospike Nozzle

Published:2010-07-25 Issue: Volume: Page:
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Container-title:46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Ladeinde Temitayo,Chen Hsun

Publisher

American Institute of Aeronautics and Astronautics

Reference5 articles.

1. Bertin,John.J.,2001,"Aerodynamics for Engineers," 4thed.,PrenticeHall,pp.568-569.

2. Bird, R. Byron, Stewart, Warren E., and Lightfoot, Edwin N., 2001, "Transport Phenomena," 2nded.John Wiley&Sons, NewYork,pp.75,78, 313.

3. Sutton, GeorgeP.and Biblarz, Oscar, 2001,"Rocket Propulsion Elements," John Wiley&Sons, NewYork,pp.28.

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1. Theories and methods for designing hypersonic high-enthalpy flow nozzles;Chinese Journal of Aeronautics;2022-01

2. In Silico Studies on Truncated Aero Spike Nozzles with Concave-Shaped Backward-Facing Ramp for Thrust Augmentation;AIAA Propulsion and Energy 2021 Forum;2021-07-28

3. In Silico Studies on Contour Optimization of Environmental Friendly Annular Aerospike Nozzle with Multiple Chevron;AIAA Propulsion and Energy 2021 Forum;2021-07-28

4. Development and Testing of Conventional and Additively Manufactured Aerospike Nozzles for Small Satellite Propulsion;AIAA Propulsion and Energy 2019 Forum;2019-08-16

5. Study of Conical Aerospike Nozzles with Base-Bleed and Freestream Effects;Journal of Spacecraft and Rockets;2019-07

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