Modelling Side Loads in Separated Rocket Nozzles
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Publisher
American Institute of Aeronautics and Astronautics
Reference36 articles.
1. 1Nave, L. and Coffey, G. "Sea Level Side Loads in High-Area-Ratio Rocket Engines," AIAA Paper 73-1284, AIAA/SAE 9th Propulsion Conference, Jun 1973.
2. 2Frey, M. and Hagemann, G. "Status of Flow Separation Prediction in Rocket Nozzles," AIAA Paper 1998-3619, 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, May 1998.
3. 3Terhadt, M. and Hagemann, G. "Flow Separation and Side-load Behavior of Truncated Ideal Rocket Nozzles," AIAA Paper 2001-3686, 37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Aug 2001.
4. 4Baars, W. J., Tinney, C. E., Ruf, J. H., Brown, A. M., and McDaniels, D. M. "On the Unsteadiness associated with Shock-Induced Separation in Overexpanded Rocket Nozzles," AIAA Papers 2010-6728, 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Nashville, TN, July 25-28,Aug 2010, ref 16.
5. 5Ruf, J. H., McDaniels, D. M., and Brown, A. M. "Details of Side Load Test Data and Analysis for a Truncated Ideal Contour Nozzle and a Parabolic Contour Nozzle," AIAA-2010-6813 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Nashville, TN, July25-28,2010.
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