Differential canard deflection for generation of yawing moment on the X-31 with and without the vertical tail
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Author
Contributions
- United States. National Aeronautics and Space Administration. - Contributor
Publication
1996 - National Technical Information Service, distributor, [Washington, DC, District of Columbia
Language
English
Word Count
0 words, Guess
Page Count
0 pages
Physical Format
Microform
Identifiers
- Open LibraryOL17796404M
- OCLC Control Number35270882
Subjects
Topics
Other Editions
- Differential canard deflection for generation of yawing moment on the X-31 with and without the vertical tail
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