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
Method for calculation of pressure distributions on thin conical bodies of arbitrary cross section in supersonic stream
Document ID
19930082277
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Maslen, Stephen H
Date Acquired
August 16, 2013
Publication Date
July 1, 1948
Report/Patent Number
NACA-TN-1659
Report Number: NACA-TN-1659
Accession Number
93R11567
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
THEORIES - FLOW
SUPERSONIC
FLOW - CONES
PRESSURE DISTRIBUTION - BODIES
THEORIES - FLOW LINEAR
FLOW - BODIES SUPERSONIC

Related Records

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