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Shock-Tube Measurements of Step-Blast Loads on a NASA 64A010 Airfoil

Report Number: ASD TR 61-219
Author(s): J. Ray Ruetenik; Walter Herrmann
Corporate Author: Massachusetts institute of Technology
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1962-02
Pages: 51
Contract: AF 33(616)-6195
Project: 1350
Task: 14045
AD Number: AD0275496

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