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Performance of a Compression-ignition Engine with a Precombustion Chamber Having High-Velocity Air Flow (1931)
NASA Technical Reports Server (NTRS) · leaf 18
N.A.C.A. Technical iTote lTo.396 Fig.3 Fig.? Automatic fuel-injection valve and single-orifice nozzle. Orifice diameter 0.050 in.NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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