NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

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

Back to Results
An experimental investigation of the effect of surface heating on boundary-layer transition on a flat plate in supersonic flow
Document ID
19930083026
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Higgins, Robert W
Pappas, Constantine C
Date Acquired
August 16, 2013
Publication Date
April 1, 1951
Report/Patent Number
NACA-TN-2351
Report Number: NACA-TN-2351
Accession Number
93R12316
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
REYNOLDS NUMBER
PLATES, FLAT - TEMPERATURES
SUPERSONIC
BOUNDARY LAYER - PLATES, FLAT
AERODYNAMICS WITH HEAT
FLOW, LAMINAR
SKIN FRICTION
WIND TUNNEL TESTS - AAL - HEAT TRANSFER, SUPERSONIC (6 INCHES)
FLOW, TURBULENT
BOUNDARY LAYER TRANSITION - PLATES, FLAT
FLOW - PLATES, FLAT
BOUNDARY LAYER - VELOCITY DISTRIBUTION

Related Records

There are no records associated with this record.
No Preview Available