TY  - JOUR
AB  - 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.
VL  - 29
IS  - 7
SN  - 0002-2667
DO  - 10.1108/eb032851
UR  - https://doi.org/10.1108/eb032851
AU  - Heath W.G.
AU  - Heath B.O.
PY  - 1957
Y1  - 1957/01/01
TI  - Practical Structural Design Problems of Supersonic Aircraft
T2  - Aircraft Engineering and Aerospace Technology
PB  - MCB UP Ltd
SP  - 206
EP  - 215
Y2  - 2024/09/22
ER  -