Transition of the laminar boundary layer on a delta wing with 74 degree sweep in free flight at mach numbers from 2.8 to 5.3 /
by Gary T. Chapman.

Description

Main Author: Chapman, Gary T.
Related Names: United States. National Aeronautics and Space Administration.
Language(s): English
Published: Washington, D.C. : National Aeronautics and Space Administration : [1961]
Subjects: Fluid mechanics.
Aerodynamics, missiles and space vehicles.
Aerodynamics, aircraft.
Note: Cover title.
"August 1961."
Aerodynamics, aircraft; Aerodynamics, missiles and space vehicles; Fluid mechanics.
Physical Description: 42 p. : ill. ; 26 cm.
Locate a Print Version: Find in a library

Item Link	Original Source
Full view	University of Illinois at Urbana-Champaign