Effects of base bleed on thrust performance of a linear aerospike nozzle

Author:

Tomita Takeo1,Takahashi Mamoru1,Onodera Takuo1,Tamura Hiroshi1

Affiliation:

1. National Aerospace Lab., Kakuda Research Center, Japan

Publisher

American Institute of Aeronautics and Astronautics

Cited by 16 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Study on Control of Unsteadiness and Flow Asymmetry in Linear Aerospike Nozzles;Journal of Spacecraft and Rockets;2023-01

2. Numerical Analysis of Flowfield in Linear Plug Nozzle with Base Bleed;Journal of Spacecraft and Rockets;2021-11

3. Experimental Study of Impinging Plug Nozzle Jet Using a Vortex Generator;Journal of Spacecraft and Rockets;2020-11

4. Experimental Study on the Aerodynamic Performance of Clustered Linear Aerospike Nozzles;18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference;2012-09-24

5. The Influence of Different Turbulence Models on the FlowField Characteristics of an Aerospike Nozzle;Applied Mechanics and Materials;2011-10-24

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