Based on slipstream theory and blade theory, certain requirements for obtaining high degree of thrust are determined; possibilities of minimizing disadvantages resulting from high degree of thrust, discussed.
Physical limitations of attainable propeller thrust
Physikalische Grenzen des erroichbaren Standschubs
1938
Article (Journal)
German
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Wing design with attainable thrust considerations
AIAA | 1984
|Wing design with attainable thrust considerations
NTRS | 1984
|