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Comprehensive missile aerodynamics programs for preliminary designTwo different classes of missile aeroprediction programs have been recently developed. The first class of programs provides rapid engineering predictions and includes MISSILE1 and MISSILE2 applicable to missile configurations with axisymmetric bodies. The second class of programs consists of the DEMON series, including a simplified version NSWCDM, designed to calculate detailed loadings acting on supersonic missiles which may have non-circular body cross sections. Both classes account for high angles of attack and track vortices from canard or wing section to the tail section. Extensive comparisons with experimental data are presented including nonlinear effects of canard control.
Document ID
19820043571
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dillenius, M. F. E.
(Nielsen Engineering and Research, Inc. Mountain View, CA, United States)
Hemsch, M. J.
(Nielsen Engineering and Research, Inc. Mountain View, CA, United States)
Sawyer, W. C.
(Nielsen Engineering and Research, Inc. Mountain View, CA, United States)
Allen, J. M.
(Nielsen Engineering and Research, Inc. Mountain View, CA, United States)
Blair, A. B., Jr.
(NASA Langley Research Center Supersonic Aerodynamics Branch, Hampton, VA, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1982
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 82-0375
Meeting Information
Meeting: Aerospace Sciences Meeting
Location: Orlando, FL
Start Date: January 11, 1982
End Date: January 14, 1982
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
82A27106
Distribution Limits
Public
Copyright
Other

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