Aeroelastic Problems of Low Aspect Ratio Wings: Part V. Application of the Structural and Aeroelastic Matrices to the Solution of Steady State Aeroelastic Problems
Abstract
This final paper of the series deals with the application of the structural and aerodynamic matrices to determine the final steady state loading on the wing, with a view to the requirements of the stress analyst. It is also shown how the stability derivatives of the elastic wing may be obtained, if a system of unit loads is employed in the calculations. Finally the occurrence of wing divergence and control surface reversal speeds are discussed in the light of the proposed methods.
Citation
Farbridge, J.E.F., Woodward, F.A. and Thomann, G.E.A. (1956), "Aeroelastic Problems of Low Aspect Ratio Wings: Part V. Application of the Structural and Aeroelastic Matrices to the Solution of Steady State Aeroelastic Problems", Aircraft Engineering and Aerospace Technology, Vol. 28 No. 6, pp. 196-198. https://doi.org/10.1108/eb032701
Publisher
:MCB UP Ltd
Copyright © 1956, MCB UP Limited