Computational study of flow in a rocket-based combined cycle (RBCC) engine inlet

Author:

Reddy D.R.,Sree D.

Publisher

Elsevier BV

Subject

General Engineering,General Computer Science

Reference23 articles.

1. Trefny CJ. An air-breathing launch vehicle concept for single-stage-to-orbit. AIAA Paper # 99-2730, June 1999.

2. Escher WJD. Synerjet for earth/orbit propulsion: revisiting the 1996 NASA/Marquardt composite (air-breathing/rocket) propulsion system study. SAE Paper # 851163, May 1985.

3. DeBonis JR, Trefny CJ, Steffen Jr CJ. inlet development for a rocket-based combined cycle, single-stage-to-orbit vehicle using computational fluid dynamics. AIAA Paper # 99-2239, June 1999.

4. DeBonis JR, Trefny CJ. Supersonic wind-tunnel tests of a half-axisymmetric, 12 degree-spike inlet to an RBCC propulsion system, NASA TM (Technical Memorandum) No. 2001-210567, February 2001.

5. NPARC Alliance Technical Team. A User’s Guide to NPARC, NPARC Alliance Technical Team, Arnold Engineering Development Center, Arnold Airforce Base, TN, 1994.

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