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Wind-tunnel investigation of the aerodynamic characteristics of the Standard Dynamics Model in coning motion at Mach 0.6A series of wind-tunnel tests have been conducted on the Standard Dynamics Model (a simplified generic fighter-aircraft shape) undergoing coning motion at Mach 0.6. Six-component force and moment data are presented for a range of angles of attack, sideslip and coning rates. At the relatively low nondimensional coning rates employed, the lateral aerodynamic charactersitics generally show a linear variation with coning rate.
Document ID
19850061718
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Jermey, C.
(Department of Defence Weapons Systems Research Laboratory, Adelaide, Australia)
Schiff, L. B.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1985
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 85-1828
Meeting Information
Meeting: Atmospheric Flight Mechanics Conference
Location: Snowmass, CO
Start Date: August 19, 1985
End Date: August 21, 1985
Accession Number
85A43869
Distribution Limits
Public
Copyright
Other

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