Aerodynamic and Aeroacoustic Wind Tunnel Testing of the Orion Spacecraft

Author:

Ross James1,Brauckmann Greg2

Affiliation:

1. NASA Ames Research Center

2. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Cited by 8 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. Parametric studies of subsonic and supersonic reentry phases of the Orion Crew Module through numerical simulations;AIAA SCITECH 2023 Forum;2023-01-19

2. Single-Component Average Velocity Profiles in the Wake of the Orion Crew Capsule at the National Transonic Facility;AIAA SCITECH 2023 Forum;2023-01-19

3. CFD investigation of rocket exhaust thrust vector control using gas injection;PROCEEDINGS OF THE 1ST INTERNATIONAL CONFERENCE ON FRONTIER OF DIGITAL TECHNOLOGY TOWARDS A SUSTAINABLE SOCIETY;2023

4. “Numerical simulation of a blunt body to investigate drag characteristics with active and passive device”;PROCEEDINGS OF THE 1ST INTERNATIONAL CONFERENCE ON FRONTIER OF DIGITAL TECHNOLOGY TOWARDS A SUSTAINABLE SOCIETY;2023

5. Numerical Simulation of Base Pressure and Drag of Space Reentry Capsules at High Speed;Hypersonic Vehicles - Past, Present and Future Developments;2019-10-02

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