Performance estimation and initial design of Armstrong-Siddeley gas turbines for propeller and rotor drive; particulars of "P.181" for helicopter propulsion and "P.182"; sea level static performance figures for two engines given in table.
1000 H.P. aircraft turbines
Engineer
Engineer ; 205 , n 5326
1958
2 pages
Aufsatz (Zeitschrift)
Englisch
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