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The transformation of aerodynamic stability derivatives by symbolic mathematical computationThe formulation of mathematical models of aeronautical systems for simulation or other purposes, involves the transformation of aerodynamic stability derivatives. It is shown that these derivatives transform like the components of a second order tensor having one index of covariance and one index of contravariance. Moreover, due to the equivalence of covariant and contravariant transformations in orthogonal Cartesian systems of coordinates, the transformations can be treated as doubly covariant or doubly contravariant, if this simplifies the formulation. It is shown that the tensor properties of these derivatives can be used to facilitate their transformation by symbolic mathematical computation, and the use of digital computers equipped with formula manipulation compilers. When the tensor transformations are mechanised in the manner described, man-hours are saved and the errors to which human operators are prone can be avoided.
Document ID
19750063165
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Howard, J. C.
(NASA Ames Research Center Moffett Field, Calif., United States)
Date Acquired
August 8, 2013
Publication Date
May 1, 1975
Publication Information
Publication: Aeronautical Quarterly
Volume: 26
Subject Category
Aerodynamics
Accession Number
75A47237
Distribution Limits
Public
Copyright
Other

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