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
Three-dimensional flow calculation by the method of characteristics.Characteristic method computer program for calculating three-dimensional supersonic flow around blunt and pointed bodies of revolution in reasonable time
Document ID
19670060158
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Rakich, J. V.
Date Acquired
August 3, 2013
Publication Date
October 1, 1967
Publication Information
Publication: AIAA JOURNAL
Subject Category
Aerodynamics
Accession Number
67A38887
Distribution Limits
Public
Copyright
Other
Keywords
SUPERSONIC FLOW
THREE-DIMENSIONAL FLOW
CHARACTERISTIC METHOD
BODY OF REVOLUTION
COMPUTER PROGRAM
BLUNT BODY

Available Downloads

There are no available downloads for this record.

Related Records

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