Experimental flutter boundaries with unsteady pressure distributionsfor the NACA 0012 Benchmark Model
32nd Structures, Structural Dynamics, and Materials Conference ; 1991 ; Baltimore , MD , U.S.A.
01.01.1991
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Unsteady transonic pressures on a NACA-0012 Airfoil and their effect on flutter stability
British Library Conference Proceedings | 1993
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