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Aerodynamic characteristics of cruciform missiles at high angles of attackAn aerodynamic prediction method for missile aerodynamic performance and preliminary design has been developed to utilize a newly available systematic fin data base and an improved equivalent angle of attack methodology. The method predicts total aerodynamic loads and individual fin forces and moments for body-tail (wing-body) and canard-body-tail configurations with cruciform fin arrangements. The data base and the prediction method are valid for angles of attack up to 45 deg, arbitrary roll angles, fin deflection angles between -40 deg and 40 deg, Mach numbers between 0.6 and 4.5, and fin aspect ratios between 0.25 and 4.0. The equivalent angle of attack concept is employed to include the effects of vorticity and geometric scaling.
Document ID
19870035215
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lesieutre, Daniel J.
(Nielsen Engineering and Research, Inc. Mountain View, CA, United States)
Mendenhall, Michael R.
(Nielsen Engineering and Research, Inc. Mountain View, CA, United States)
Nazario, Susana M.
(Nielsen Engineering and Research, Inc. Mountain View, CA, United States)
Hemsch, Michael J.
(PRC Kentron, Inc. Hampton, VA, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1987
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 87-0212
Report Number: AIAA PAPER 87-0212
Accession Number
87A22489
Funding Number(s)
CONTRACT_GRANT: N00014-80-C-0700
Distribution Limits
Public
Copyright
Other

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