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The Effects of Body Camber on Body Pressure Distributions and Wing Forces for Mach Numbers from 2.0 to 7.6: Part I: Experimental Data

Report Number: ASD TR 61-295 Part I
Author: Durgin, F. H.
Author: Noz, W. C., Jr.
Corporate Author: Massachusetts Institute of Technology Naval Supersonic Facility
Laboratory: Flight Control Laboratory
Pages: 83
Contract: AF 33(616)-7246
Project: 8219
Task: 821901

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