Lee, Y.-K. and Raghunathan, Srinivasan and Bénard, Emmanuel and Kim, Heuy-Dong and Setoguchi, Toshiaki Control of plume interference effects on axisymmetric afterbodies. (2004) Aeronautical Journal, vol. 108 (n° 1082). pp. 185-196. ISSN 0001-9240
(Document in English)
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Plume interference effects on the axisymmetric flowfields around powered missiles are investigated using computational techniques. The study is mainly to understand the physics of the plume-induced shock and separation particularly at high plume to exit pressure ratios with and without shock-turbulent boundary layer control methods.
|Additional Information:||Thanks to The Royal Aeronautical Society editor. The definitive version is available at http://www.raes.org.uk/|
|Audience (journal):||International peer-reviewed journal|
|Institution:||Université de Toulouse > Institut Supérieur de l'Aéronautique et de l'Espace - ISAE (FRANCE)|
Other partners > Andong National University (KOREA)
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Other partners > Saga University (JAPAN)
|Deposited By:||Emmanuel Benard|
|Deposited On:||07 Apr 2011 10:29|
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