02132cam a2200445Ia 4500100167824MiAaHDL20250726000000.0m d cr bn ---auaua110308s1955 dcua b f000 0 eng d(MiU)990128617800106381sdr-miu.990128617800106381(MiU)MIU01000000000000012861780-goog(OCoLC)706166997(MiU)Aleph012861780CSLTEFNACARUtOrBLWNACATL709.5.C6C63 1955Y 3.N21/5:15/E54L28aCochran, Reeves P.Static sea-level performance of an axial-flow-compressor turbojet engine with an air-cooled turbine /by Reeves P. Cochran and Robert P. Dengler.Washington [D.C.] :National Advisory Committee for Aeronautics,[1955]41 p. :ill. ;27 cm.texttxtrdacontentunmediatednrdamediavolumencrdacarrierNACA research memorandum ;E54L28a"Declassified February 10, 1959.""March 15, 1955."Cover title.Includes bibliographical references (p. 25-26).Mode of access: Internet.Air-cooled engines.http://id.loc.gov/authorities/subjects/sh85002622AirplanesTurbojet enginesCompressorsTesting.AirplanesTurbojet enginesBladesCoolingTesting.Dengler, Robert P.Cochran, Reeves P.Lewis Flight Propulsion Laboratory.http://id.loc.gov/authorities/names/no2015026965http://id.loc.gov/rwo/agents/no2015026965http://viaf.org/viaf/314909134United States.National Adviosry Committee for Aeronautics.NACA research memorandum.United States.National Advisory Committee for Aeronautics.http://id.loc.gov/authorities/names/n79060141http://id.loc.gov/rwo/agents/n79060141Technical Report Archive & Image Library (TRAIL)3901508646357010016782420241218070801.020250726000000.020260319165526.02026-03-20T08:30:39Z2024-05-05T17:30:02ZSDR-MIUmiuALMAprepare.pl-004-009BKsdr-miu.990128617800106381MiUSDRGWLA012861780mdp.39015086463570MIU990128617800106381MIUGWLA20260320googlemdp.390150864635701955pdbibUS fed doc