Problem of future development based principally upon European development, from 1915 down to date; comparison of service ceilings (in feet) of 1918 and 1930 bombers; bomb load for various ranges of action, expressed in percentages of total flying weight; fighter aircraft; altitude and ground fire.
Development of military aircraft design
Aviation
Aviation ; 30 , n 11
1931
4 pages
3 Figs.
Article (Journal)
English
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Design for military aircraft operability
TIBKAT | 1980
|Engineering Index Backfile | 1960
Engineering Index Backfile | 1961
Engineering Index Backfile | 1950
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