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.
1991-01-01
Conference paper
Electronic Resource
English
Unsteady transonic pressures on a NACA-0012 Airfoil and their effect on flutter stability
British Library Conference Proceedings | 1993
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