General problems associated with design of propellers for gas turbines and application of turbine propeller power plants to high speed airplanes; conclusion reached that at speeds of 600 to 700 mph propeller efficiencies of over 70% appear possible, particularly with unconventional configurations, such as swept-back blades and small diameter multi-blade propellers. Before Inst Aeronautical Sciences.
Propellers for aircraft gas turbines
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 13 , n 9
1946
Article (Journal)
English
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SAE Technical Papers | 1929
|Engineering Index Backfile | 1929
|Engineering Index Backfile | 1929
|NTIS | 1940