Studies of three engine configurations made for flight conditions from sea level static to 600 mph at 40,000 ft; it was concluded that turbine frontal area, stress, and pressure ratio requirements made exhaust area adjustment desirable.
Compressor and turbine matching considerations in turboprop engines
Soc Automotive Engrs -- Paper
Society of Automotive Engineers -- Meeting ; 1956 Turbine propeller
1956
11 pages
Aufsatz (Konferenz)
Englisch
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Compressor and Turbine Matching Considerations in Turboprop Engines
SAE Technical Papers | 1957
|Elsevier | 1986
|