Note shows that propeller can be designed to give satisfactory aerodynamic characteristics for flight at 50,000 ft, that it will give relatively poor performance at low altitudes, that take-off will be fair, but that weight will be excessive; equations and formulas included.
Speculations on propellers for stratosphere airplanes
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 4 , n 11
1937
4 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
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