Preliminary Flight Tests of the N.A.C.A. Roots Type Aircraft Engine Supercharger (1928)
NASA Technical Reports Server (NTRS) · leaf 6
m the carburetor duct to the float chamber. Free flow through this line is necessary for the instantaneous balancing of pressures. An ordinary Bourdon tube gage is used to indicate the differential fuel pressure. The ine is led from the carburetor duct Bourdon tube is connected to the fuel supply… … characl erisl lc of experimental installations only, as a combined engine throttle and by-pass control and lubrication by the engine oiling system would be incorporated in a service installation. A complete description of the supercharger is given in Reference 1; its displacement was 0.51 cubic…
NASA Technical Reports Server (NTRS)
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