Computational Analyses in Support of Sub-Scale Diffuser Testing for the A-3 Facility. Part 1: Steady Predictions-Reference-Cited by-同舟云学术

Computational Analyses in Support of Sub-Scale Diffuser Testing for the A-3 Facility. Part 1: Steady Predictions

Published:2009-08-02 Issue: Volume: Page:
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Container-title:45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Allgood Daniel,Graham Jason,Ahuja Vineet,Hosangadi Ashvin

Publisher

American Institute of Aeronautics and Astronautics

Reference18 articles.

1. Dumbacher, D. "A New Heavy-Lift Capability for Space Exploration: NASA's Ares V Cargo Launch Vehicle," AIAA Space 2006 Conference, San Jose, CA, Sep.19-21,2006.

2. Greenwood, T., Twichell, W., Ferrari, D., and Kuck, F. "Shuttle Derived In-Line Heavy Lift Vehicle," AIAA-2005-3816, 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Tucson, Arizona, July10-13,2005.

3. Murphy, T. "RS-68 and Linear Aerospike," 50th International Astronautical Federation Congress, Liquid Rocket Propulsion, Oct. 1999.

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1. Reduction of Altitude Diffuser Jet Noise Using Water Injection;50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2012-01-09

2. Computational Analyses in Support of Sub-Scale Diffuser Testing for the A-3 Facility. Part 3: Aero-Acoustic Analyses and Experimental Validation;45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2009-08-02

3. Computational Analyses in Support of Sub-Scale Diffuser Testing for the A-3 Facility. Part 2: Unsteady Analyses and Risk;45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2009-08-02