Numerical Analysis Of Supersonic Flow Through Curved Channels

Item

Title
Numerical Analysis Of Supersonic Flow Through Curved Channels
Date
1963
Index Abstract
Not Available
Photo Quality
Not Needed
Report Number
ARL 63-117
Creator
Der, J., Jr.
Mullings, B. N.
Hoffman, G. H.
Brown, B. N. Pridmore
Corporate Author
Northrop Aircraft Inc Hawthorne Calif
Laboratory
Aeronautical Research Laboratories
Extent
280
Identifier
AD0419309
Access Rights
OTS
Distribution Classification
1
Contract
AF 33(657)-8851
DoD Project
7065
DoD Task
706501
DTIC Record Exists
No
Distribution Change Authority Correspondence
None
Report Availability
Full text available by request
Date Issued
1963-07
Abstract
The abstract for this report is either unavailable or has yet to be entered
Type
report
Provenance
Lockheed Martin Missiles & Fire Control

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