Flight test base pressure results at hypersonic Mach numbers and highReynolds numbers in turbulent flow - Implications to ground test simulation requirements
9th Aerospace Sciences Meeting ; 1971 ; New York , NY , U.S.A.
1971-01-01
Conference paper
Electronic Resource
English
FLUID DYNAMICS - Role of Turbulent Prandtl Numbers on Heat Flux at Hypersonic Mach Numbers
Online Contents | 2007
|Transition measurements at hypersonic Mach numbers.
NTRS | 1967
|