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The Influence of Non-linear Longitudinal Aerodynamic Characteristics on the Power Spectral Response of Aircraft to Atmospheric Turbulence

Published online by Cambridge University Press:  07 June 2016

P A T Christopher  and
J M H Dunn
P A T Christopher
Affiliation:
Cranfield Institute of Technology
J M H Dunn
Affiliation:
Delaney Gallay Ltd
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Summary

The power spectral technique has been extended to show the effect of aerodynamic non-linearities on the normal acceleration response of a rigid aircraft in the cruise configuration. Non-linearities in the normal force and pitching moment variations with incidence have been considered. The resulting changes from the linear root-mean-square values of normal acceleration were only 3 to 5½% for a root-mean-square vertical gust velocity of 20 m/s.

Type
Research Article
Information
Aeronautical Quarterly , Volume 24 , Issue 4 , November 1973 , pp. 284 - 294
Copyright
Copyright © Royal Aeronautical Society. 1973

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References

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