An investigation of the effect of a turbulent boundary layer upon the lift of a wing-body combination with a gap between wing and body at mach number 1.9

An investigation of the effect of a turbulent boundary layer upon the lift of a wing-body combination with a gap between wing and body at mach number 1.9

Bibliographic Details
Main Authors: Cartwright, B. J., Wood, Robert C.
Language:en_US
Published: Monterey, California: U.S. Naval Postgraduate School 2012
Online Access:http://hdl.handle.net/10945/14306

Internet

http://hdl.handle.net/10945/14306

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