Numerical Study on the Flow Mechanism of Base Aerodynamic Force Acting on the Vertical Landing Rocket

Author:

Fujimatsu Nobuyoshi,Suzuki Kojiro

Publisher

Japan Society for Aeronautical and Space Sciences

Reference7 articles.

1. 1) Gaubatz, W. A.: The road from Delta-Clipper experimental to operational SSTO, 20th International Symposium on Space Technology and Science, Gifu, 96-f-24v, 1996.

2. Status of "Delta Clipper SSTO" and Its Future.

3. 5) Krothapalli, A., Rajkuperan, F. Alvi and Lourenco, L.: Flow Field and Noise Characteristics of a Supersonic Impinging Jet, J. Fluid Mech., 392 (1999), pp. 155–181.

4. 6) Wang, T. S.: DC-X In-Ground Effect on Base Flow and Heating Environment, AIAA Paper 97-2550, 1997.

5. 8) Shima, E. and Jounouchi, T.: Role of CFD in Aeronautical Engineering (No. 14)—AUSM Type Upwind Schemes—, Proceedings of 14th NAL Symposium on Aircraft Computational Aerodynamics, NAL-SP30, 1996, pp. 7–12.

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1. Investigation of Effect of Ground Downstream of Overexpanded Dual-Bell Nozzle During Vertical Takeoff and Landing;46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2010-07-25

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