Comparison of 4 different gas turbines incorporating free turbine, as applied to rotary wing aircraft; consideration of ratio of free turbine shaft horsepower to primary gas flow rate, main compressor turbine shaft horsepower, specific fuel consumption, airflow ratio, and duct pressure and temperature; conclusions summarized.
Free turbine systems in rotary wing aircraft
Aerospace Eng
Aerospace Engineering ; 20 , n 1
1961
5 pages
Aufsatz (Zeitschrift)
Englisch
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Free turbine systems in rotary wing aircraft
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