Practical Structural Design Problems of Supersonic Aircraft
W.G. Heath
(Assistant Chief Stressman, A. V. Roe & Co. Ltd., Manchester.)
B.O. Heath
(Principal Engineer, New Design Office, English Electric Co. Ltd., Warton.)
183
Abstract
BEFORE a detailed consideration of internal stresses may be made, it is necessary to define external loadings which are possibly critical. This involves the consideration of manoeuvres throughout the altitude range of the aeroplane, to a severity fixed by aerodynamic or specification values of speed and normal acceleration.
Citation
Heath, W.G. and Heath, B.O. (1957), "Practical Structural Design Problems of Supersonic Aircraft", Aircraft Engineering and Aerospace Technology, Vol. 29 No. 7, pp. 206-215. https://doi.org/10.1108/eb032851
Publisher
:MCB UP Ltd
Copyright © 1957, MCB UP Limited