Stability and control characteristics of a monoplanar missile configuration with two low-profile tail arrangements at Mach numbers from 1.70 to 2.86 /

An experimental wind tunnel investigation has been made to determine the longitudinal and lateral aerodynamic stability and control characteristics of two tail fin arrangements of a monowing missile model. Both a conventional cruciform and a low profile tail arrangement were tested. The results indi...

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Bibliographic Details
Main Author: Blair, A. B.
Corporate Author: United States. National Aeronautics and Space Administration.
Format: Government Document Book
Published: Washington : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1977.
Series:NASA technical note ; NASA TM X-3533.

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Call Number: NAS 1.15:X-3533