Aerothermal tests of a 12.5⁰ cone at Mach 6.7 for various Reynolds numbers, angles of attack, and nose shapes
By: Robert J. Nowak, Cindy W. Albertson, and L. Roane Hunt.
Contributors: Albertson, Cindy W.; Hunt, L. Roane; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Series: NASA technical paper -- 2345.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch
Published: 1985
Place of publication: Washington, D.C
Language: eng
Format: Microform
Subjects: Aerodynamic heating.; Boundary layer transition.; Cones.; Flow distribution.; Laminar boundary layer.; Shock layers.; Turbulent boundary layer.
Notes: "January 1985"--Cover.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1985] 1 microfiche.