Measurements of aerodynamic heat transfer and boundary-layer transition on a 10° cone in free flight at supersonic Mach numbers up to 5.9
Publisher: NACA
Published: 1956
Place of publication: Washington, D.C.
Language: eng
Number of pages: 40
Subjects: Heat--Transmission; Aerodynamics--Research.
Description: <a href="http://uf.catalog.fcla.edu/uf.jsp?st=UF003854699&ix=nu&I=0&V=D&pm=1" rel="nofollow">http://uf.catalog.fcla.edu/uf.jsp?st=UF003854699&ix=nu&I=0&V=D&pm=1</a>