Subsonic drag of spheres at Reynolds numbers from 200 to 10,000.
GOIN, K. L. /SANDIA CORP., AERO- THERMODYNAMICS DEPT., EXPERIMENTAL AERODYNAMICS DIV., ALBUQUERQUE,, LAWRENCE, W. R. /ARO, INC., ARNOLD ENGINEERING DEVELOPMENT CENTER, VON KARMAN GAS DYNAMICS FACILITY,
AIAA Journal ; 6 , 5 ; 961-962
1968
Article (Journal)
Electronic Resource
English
Partial Cavity Drag Reduction at High Reynolds Numbers
Online Contents | 2010
|AIAA | 1965
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