Unsteadiness of Flow Separation and End-Effects Regime in a Thrust-Optimized Contour Rocket Nozzle

Author: Nguyen Anh   Deniau H.   Girard S.   Alziary de Roquefort T.  

Publisher: Springer Publishing Company

ISSN: 1386-6184

Source: Applied Scientific Research, Vol.71, Iss.1-4, 2003-01, pp. : 161-181

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Abstract