Apr 30 1929: Design of airplane to navigate in stratosphere; possibility of utilizing dense air at lower altitude for take-off and landing, and reduced density of higher altitudes for reduction of air resistance and for increase in speed with means available at present; increasing speed 50 per cent at present power loading; arrangement of power plant and technical possibility of climbing to high altitude; mechanically driven supercharger useless; Rateau turbo-supercharger. (Aeronautical Eng. Sec.)
The high altitude airplane
Aviation
Aviation ; 26 , n 16
1929
8 pages
5 Figs.
Aufsatz (Zeitschrift)
Englisch
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