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The Static Aeroelastic Deformation of Slender Configurations

PART IV: Manoeuvre Theory

Published online by Cambridge University Press:  07 June 2016

G. J. Hancock
G. J. Hancock*
Affiliation:
Department of Aeronautical Engineering, Queen Mary College, University of London
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Summary

The concept of the manoeuvre margin is discussed, and definitions are suggested which are applicable to all types of configurations. Calculations are presented for the manoeuvre characteristics of simplified flexible models representing conventional and slender integrated aircraft. Linear aerodynamics only are assumed.

Type
Research Article
Information
Aeronautical Quarterly , Volume 14 , Issue 4 , November 1963 , pp. 311 - 330
Copyright
Copyright © Royal Aeronautical Society. 1963

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References

1. Hancock, G. J. The Static Aeroelastic Deformation of Slender Configurations. Part I— Some Elementary Considerations. Aeronautical Quarterly, Vol. XII, p. 293, August 1961.CrossRefGoogle Scholar
2. Hancock, G. J. The Static Aeroelastic Deformation of Slender Configurations. Part II— Calculations on Slender Plate Aircraft, Including Non-Linear Aerodynamics. Aeronautical Quarterly, Vol. XII, p. 372, November 1961.CrossRefGoogle Scholar
3. Hancock, G. J. The Static Aeroelastic Deformation of Slender Configurations. Part III— Static Stability. Aeronautical Quarterly, Vol. XIV, p. 75, February 1963.CrossRefGoogle Scholar
4. Gates, S. B. and Lyon, H. M. A Continuation of Longitudinal Stability and Control. Part I—General Theory. R.& M. 2027, 1944 Google Scholar