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Longitudinal aerodynamic characteristics at Mach 1.50 to 4.63 of a missile model employing various canards and a trailing edge flap control

Author
Trescot, C. D., Jr.
Published
Oct 1, 1971.
Physical Description
1 electronic document
Online Version

Availability

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Restrictions on Access
Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
Wind tunnel static longitudinal stability and control characteristics of cruciform delta winged missile with various horizontal canards and trailing-edge flap control between Mach 1.50 and 4.63
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19710026939.
Accession ID: 71N36415.
NASA-TM-X-2367.
L-6163.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15948457