Transient Heat Load Estimate for the A3 Subscale Supersonic Rocket Diffuser Using Surface Temperature Measurement
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American Institute of Aeronautics and Astronautics
Reference8 articles.
1. 1Saunders, G. P. and Yen, J. C. "A3 Subscale Rocket Hot Fire Testing," AIAA-2009-5099, AIAA 2009-5099, AIAAJoint Propulsion Conference, Denver,Colorado August, 2009.
2. Reduction of data from thin-film heat-transfer gages - A concise numerical technique.
3. 3Yen, J. C., Saunders, G. P., and Wagner, D. A. "Error Analysis of the Surface Heat Flux Calculation for the A3 Subscale Supersonic Diffuser," AIAA 2009-5011, AIAA Joint Propulsion Conference, Denver,Colorado August, 2009.
4. 4Saunders, G. P. "A3 Subscale Diffuser Test Article Design", AIAA-2009-5010,AIAA 2009-5010, AIAA Joint Propulsion Conference, Denver, ColoradoAugust, 2009.
5. 5Saunders, G. P., Varner, D.G., and Grover, J.B. "Description and Operation of the A3 Subscale Facility", AIAA2009-5097, AIAA2009-5097,AIAAJointPropulsion Conference, Denver, ColoradoAugust, 2009.
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