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bodies with noncircular cross sections and bank-to-turn missilesA development status evaluation is presented for the aerodynamics of missile configurations with noncircular cross-sections and bank-to-turn maneuvering systems, giving attention to cases with elliptical and square cross-sections, as well as bodies with variable cross-sections. The assessment of bank-to-turn missile performance notes inherent stability/control problems. A summary and index are provided for aerodynamic data on monoplanar configurations, including those which incorporate airbreathing propulsion systems.
Document ID
19920057211
Document Type
Conference Proceedings
Authors
Jackson, C. M., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Sawyer, W. C.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1992
Subject Category
AERODYNAMICS
Distribution Limits
Public
Copyright
Other