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.
Heath, W. and Heath, B. (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/eb032851Download as .RIS
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