Stability and control characteristics of a monoplanar missile configuration with triform-tail-fin arrangements at mach numbers from 1.70 to 2.86
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Author
Contributions
- United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch. - Contributor
- Langley Research Center. - Contributor
Publication
1981 - National Aeronautics and Space Administration, Scientific and Technical Information Branch, Washington, D.C, District of Columbia
Language
English
Subjects
Topics
Series Statement
- NASA technical memorandum -- 83223.
Other Editions
- Stability and control characteristics of a monoplanar missile configuration with triform-tail-fin arrangements at mach numbers from 1.70 to 2.86
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