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.
01.01.1971
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
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
|