Wednesday, May 1, 2013

Comparison of theoretical and experimental steady wing loads on a space shuttle configuration at Mach numbers of 0.6 and 1.4

Comparison of theoretical and experimental steady wing loads on a space shuttle configuration at Mach numbers of 0.6 and 1.4
Author: John S Preisser
Edition:
Binding: Unknown Binding
ISBN: B0006WPNUY



Comparison of theoretical and experimental steady wing loads on a space shuttle configuration at Mach numbers of 0.6 and 1.4 (NASA technical memorandum ; NASA TM X-3404)


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