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.
Practical Structural Design Problems of Supersonic Aircraft
Aircraft Engineering and Aerospace Technology ; 29 , 7 ; 206-215
1957-07-01
10 pages
Article (Journal)
Electronic Resource
English
Practical structural design problems of supersonic aircraft
Engineering Index Backfile | 1957
|Unique structural problems in supersonic aircraft design
Engineering Index Backfile | 1956
|Structural problems of supersonic aircraft
Engineering Index Backfile | 1960
|Engineering Index Backfile | 1953
|SUPERSONIC AND TRANSONIC AIRCRAFT PROBLEMS
SAE Technical Papers | 1950
|