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Aerodynamic side-force alleviator meansAn apparatus for alleviating high angle of attack side force on slender pointed cylindrical forebodies such as fighter aircraft, missiles and the like is described. A symmetrical pair of helical separation trips was employed to disrupt the leeside vortices normally attained. The symmetrical pair of trips starts at either a common point or at space points on the upper surface of the forebody and extends along separate helical paths along the circumference of the forebody.
Document ID
19810006453
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Rao, D. M.
(Old Dominion Univ.)
Date Acquired
September 4, 2013
Publication Date
September 30, 1980
Subject Category
Aerodynamics
Report/Patent Number
Patent Number: NASA-CASE-LAR-12326-1
Patent Application Number: US-PATENT-APPL-SN-019541
Patent Number: US-PATENT-4,225,102
Accession Number
81N14968
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-LAR-12326-1|US-PATENT-4,225,102
Patent Application
US-PATENT-APPL-SN-019541
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