Transient wall pressures in an overexpanded and large area ratio nozzle
Author:
Publisher
Springer Science and Business Media LLC
Subject
Fluid Flow and Transfer Processes,General Physics and Astronomy,Mechanics of Materials,Computational Mechanics
Link
http://link.springer.com/content/pdf/10.1007/s00348-013-1468-8.pdf
Reference21 articles.
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2. Arens M, Spiegler E (1963) Shock-induced boundary layer separation in overexpanded conical exhaust nozzles. AIAA J 1(3):578–581
3. Baars WJ, Tinney CE, Ruf JH (2011) Time-frequency analysis of rocket nozzle wall pressures during start-up transients. J Phys Conf Ser 318(9):1–10
4. Baars WJ, Tinney CE, Ruf JH, Brown AM, McDaniels DM (2012a) Wall pressure unsteadiness and side loads in overexpanded rocket nozzles. AIAA J 50(1):61–73
5. Baars WJ, Tinney CE, Wochner MS (2012b) Nonlinear noise propagation from a fully expanded mach 3 jet. In: 50th AIAA aerospace sciences meeting and exhibit, Nashville, TN. AIAA 2012-1177
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