Reynolds number effects on supersonic asymmetrical flows over a coneat high angle of attack
9th Applied Aerodynamics Conference ; 1991 ; Baltimore , MD , U.S.A.
01.01.1991
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Reynolds Number Effects on Supersonic Asymmetrical Flows over a Cone
Online Contents | 1993
|PLUNGING AIRFOIL: REYNOLDS NUMBER AND ANGLE OF ATTACK EFFECTS
TIBKAT | 2020
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