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A study of the nonlinear aerodynamics of bodies in nonplanar motionConcepts from the theory of functionals are used to develop nonlinear formulations of the aerodynamic force and moment systems acting on bodies in large-amplitude, arbitrary motions. The analysis, which proceeds formally once the functional dependence of the aerodynamic reactions upon the motion variables is established, ensures the inclusion, within the resulting formulation, of pertinent aerodynamic terms that normally are excluded in the classical treatment. Applied to the large-amplitude, slowly varying, nonplanar motion of a body, the formulation suggests that the aerodynamic moment can be compounded of the moments acting on the body in four basic motions: steady angle of attack, pitch oscillations, either roll or yaw oscillations, and coning motion. Coning, where the nose of the body describes a circle around the velocity vector, characterizes the nonplanar nature of the general motion.
Document ID
19740006628
Acquisition Source
Legacy CDMS
Document Type
Thesis/Dissertation
Authors
Schiff, L. B.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1974
Subject Category
Aerodynamics
Report/Patent Number
A-5057
NASA-TR-R-421
Report Number: A-5057
Report Number: NASA-TR-R-421
Accession Number
74N14741
Funding Number(s)
PROJECT: RTOP 501-06-01-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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