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Pressure distribution and damping in steady roll at supersonic Mach numbers of flat swept-back wing with subsonic edges

Author: Ballantyne, Mary B
Physical Description: 1 electronic document
Additional Creators: Walker, Harold J

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Restrictions on Access: Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Collection: NASA Technical Reports Server (NTRS) Collection.
Note: Document ID: 19930082702.
Accession ID: 93R11992.
NACA-TN-2047.
Terms of Use and Reproduction: No Copyright.

View MARC record | catkey: 15434714