Search

list

1 item

full text unavailable
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
Author(s): Durgin, F. H., Noz, W. C., Jr.
Corporate Author(s): Massachusetts Institute of Technology Naval Supersonic Facility
Laboratory: Flight Control Laboratory
Report number: ASD TR 61-295 Part I

Refine your search

Refine your search