THE DESIGN OF AIRPLANE-ENGINE SUPERCHARGERS (1937)
NASA Technical Reports Server (NTRS) · leaf 15
R.A.C.A* Technical Memcrandum !To. 839 FlgB. 1,3,3,4 … wall at back of wheels performance of an engine (sea impeller closed at both sides level output * 100 percent) at by walls. critical altitudes up to 12 tan. (7.5 mi.). 10 fm 9 8 7 6 5 0,5 QJ5 0,7 0.0 Figure 3.-Critical altitude attainable without interceding as a function of the internal adiabatlc…
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