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Pressure distributions over a wing-fuselage model at Mach numbers of 0.4 to 0.99 and at 1.2.

Author: Matthews, Clarence W
Physical Description: 1 electronic document

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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: 19930085535.
Accession ID: 93R14825.
NACA-RM-L8H06.
Terms of Use and Reproduction: No Copyright.

View MARC record | catkey: 15432378