Investigation of a Rateau Supercharger for a 700-horsepower Airplane Engine (1934)
NASA Technical Reports Server (NTRS) · leaf 20
Figs. 9;iOfllf12 I.A.C.A. Technical Memorandum Ho.738 … & fa 9* $5 Q6 Q7 fa Q9 io mys o 0,i Delivery volume( intake condition) IDVL1982112QQ. 50 7/1—1—r_1—r cf,c2 T 30 m/°€ 20 ¥ M ¥ iS V 2fi 1 V P/P Figure 10•-Diagram for find- ing compression ratio from adiabatic delivery head and intake temperature. Adiahatic exponent K»l.405 4 io .fom iz Altitude 4ms…
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