An investigation of the effect of a laminar body boundary layer on the body interference pressures of a wing-body combination at mach number 1.9
By: by T.R. Rhees and W.P. Crenshaw
Contributors: Crenshaw, W. P.
Publisher: University of Michigan
Published: 1954
Language: eng
Subjects: Aeronautics
Notes: Thesis (MS)--University of Michigan, 1954.