An experimental investigation of the effects of Mach number and Reynolds number on the side forces induced on a slender body of revolution at high angles of attack was conducted. The tests were carried out in the Air Force Flight Dynamics Laboratory's Trisonic Gasdynamic Facility. (DePo)
An experimental investigation of steady asymmetric Vortex shedding from a slender body of revolution at high angles of attack
Experimentelle Untersuchung einer stationaeren asymmetrischen Wirbelabloesung bei schlanken Drehkoerpern und einem steilen Angriffswinkel
US Government Research Reports ; Dec ; 1-64
1977
64 Seiten
Report
English
An Investigation of Vortex Shedding on Slender Body at High Incidence
British Library Conference Proceedings | 1994
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