Characterization of the influence of a favorable pressure gradient on the basic structure of a Mach 5.0 high Reynolds number supersonic turbulent boundary layer /

Bibliographic Details

Main Author:	Tichenor, Nathan R.
Other Authors:	Bowersox, Rodney D. W. (Thesis advisor)
Format:	Thesis eBook
Language:	English
Published:	[College Station, Tex.] : [Texas A&M University], [2010]
Subjects:	Major Aerospace Engineering. Mach 5.0 favorable pressure gradient hypersonic
Online Access:	Link to OAK Trust copy