NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Turbulent boundary-layer temperature recovery factors in two-dimensional supersonic flow
Document ID
19930082955
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Tucker, Maurice
Maslen, Stephen H
Date Acquired
August 29, 2013
Publication Date
February 1, 1951
Report/Patent Number
NACA-TN-2296
Report Number: NACA-TN-2296
Accession Number
93R12245
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
BOUNDARY LAYER - PLATES TURBULENT
BOUNDARY LAYER - TEMPERATURE
HEAT TRANSMISSION - BOUNDARY LAYER, TURBULENT
FLOW - PLATES SUPERSONIC
No Preview Available