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Response of Rotor Blades to Random Loads under Forward Flight Conditions

Published online by Cambridge University Press:  07 June 2016

C Lakshmikantham  and
K S Aravamudan
C Lakshmikantham
Affiliation:
Army Materials and Mechanics Research Center, Watertown, Massachusetts
K S Aravamudan
Affiliation:
Massachusetts Institute of Technology
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Summary

This paper contains results for the response of a helicopter rotor blade under stationary random excitation when the helicopter is in forward flight. The blade model takes into account the bending and torsional modes as well as the root-rigidity conditions. The resulting linear dynamical system equations with periodic coefficients are treated within the framework of the filtering theory to yield matrix ordinary differential equations for the required response-statistics themselves.

Type
Research Article
Information
Aeronautical Quarterly , Volume 24 , Issue 4 , November 1973 , pp. 252 - 260
Copyright
Copyright © Royal Aeronautical Society. 1973

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References

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