Current correction methods give unsatisfactory results when used to establish standard air performance of modern high speed airplanes; advent of gas turbine jet propelled airplane has further emphasized need for more suitable method; performance correction method suggested allows for effects of Mach Number on airplane, propeller, and engine characteristics. Before Inst Aeronautical Sciences.
Reduction of flight-test performance data to standard air conditions by temperature altitude method
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 13 , n 10 ; p 543-555
1946
13 pages
Bibliography
Article (Journal)
English
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