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Summary of transformation equations and equations of motion used in free flight and wind tunnel data reduction and analysisBasic formulations for developing coordinate transformations and motion equations used with free-flight and wind-tunnel data reduction are presented. The general forms presented include axes transformations that enable transfer back and forth between any of the five axes systems that are encountered in aerodynamic analysis. Equations of motion are presented that enable calculation of motions anywhere in the vicinity of the earth. A bibliography of publications on methods of analyzing flight data is included.
Document ID
19720018825
Document Type
Special Publication (SP)
Authors
Gainer, T. G.
(NASA Langley Research Center Hampton, VA, United States)
Hoffman, S.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1972
Subject Category
Aerodynamics
Report/Patent Number
NASA-SP-3070
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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