NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Shock wave-boundary layer interactions in laminar transonic flow.
Document ID
19730032162
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Brilliant, H. M.
Adamson, T. C., Jr. (Michigan, University Ann Arbor, Mich., United States)
Date Acquired
August 7, 2013
Publication Date
January 1, 1973
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 73-239
Meeting Information
Meeting: Aerospace Sciences Meeting
Location: Washington, DC
Start Date: January 10, 1973
End Date: January 12, 1973
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
73A16964
Funding Number(s)
CONTRACT_GRANT: NGR-23-005-523
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.

Related Records

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