Nozzle flowfield analysis with particular regard to 3D-plug cluster configurations

Author:

Hagemann G.1,Schley C.-A.1,Odintsov E.2,Sobatchkine A.2

Affiliation:

1. DLR, Hardthausen, Germany

2. Computational Aerodynamics Systems Co., Moscow, Russia

Publisher

American Institute of Aeronautics and Astronautics

Reference17 articles.

Cited by 12 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

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3. Shock Vector Control Technique for Aerospike Nozzles;AIAA Scitech 2020 Forum;2020-01-05

4. Numerical Analysis of Curved Thrusters for Multichamber Aerospike Engines in Flight Conditions;Journal of Propulsion and Power;2017-07

5. Development and Flight-Testing of Liquid Propellant Aerospike Engines;40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2004-06-26

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