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Nonlinear problems in flight dynamicsA comprehensive framework is proposed for the description and analysis of nonlinear problems in flight dynamics. Emphasis is placed on the aerodynamic component as the major source of nonlinearities in the flight dynamic system. Four aerodynamic flows are examined to illustrate the richness and regularity of the flow structures and the nature of the flow structures and the nature of the resulting nonlinear aerodynamic forces and moments. A framework to facilitate the study of the aerodynamic system is proposed having parallel observational and mathematical components. The observational component, structure is described in the language of topology. Changes in flow structure are described via bifurcation theory. Chaos or turbulence is related to the analogous chaotic behavior of nonlinear dynamical systems characterized by the existence of strange attractors having fractal dimensionality. Scales of the flow are considered in the light of ideas from group theory. Several one and two degree of freedom dynamical systems with various mathematical models of the nonlinear aerodynamic forces and moments are examined to illustrate the resulting types of dynamical behavior. The mathematical ideas that proved useful in the description of fluid flows are shown to be similarly useful in the description of flight dynamic behavior.
Document ID
19840017580
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chapman, G. T.
(NASA Ames Research Center Moffett Field, CA, United States)
Tobak, M.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1984
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-85940
A-9707
NAS 1.15:85940
Report Number: NASA-TM-85940
Report Number: A-9707
Report Number: NAS 1.15:85940
Meeting Information
Meeting: Berkeley-Ames Conf. on Nonlinear Probl. in Control and Fluid Dyn.
Location: Berkeley, CA
Country: United States
Start Date: May 31, 1983
End Date: June 10, 1983
Accession Number
84N25648
Funding Number(s)
PROJECT: RTOP 505-31-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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