02380cam a2200445Ia 4500100903384MiAaHDL20250726000000.0m d cr bn ---auaua110216s1944 dcua tb f000 0 eng d(MiU)990139479240106381sdr-miu.990139479240106381(MiU)MIU01000000000000013947924-goog(OCoLC)702135022(MiU)Aleph013947924LHLLHLLHLOCLCOTRAALUtOrBLWMAINY 3.N 21/5:11/E5NACA ACR E4L21NACA WR E5King, J. Austin.Performance of NACA eight-stage axial-flow compressor at simulated altitude /J. Austin King and Owen W. Regan.NACA Wartime Reports. Series E.Washington, D.C. :National Advisory Committee for Aeronautics,[1944]7, [10] p. :ill. ;27 cm.texttxtrdacontentunmediatednrdamediavolumencrdacarrierWartime Report / National Advisory Committee for Aeronautics ;no. E5Prepared at the Aircraft Engine Research Laboratory, Cleveland, Ohio.Originally issued as NACA as Advance Confidential Report E4L21 (December 1944).NACA Wartime Report E-5.Includes bibliographical references.An investigation has been conducted by the NACA to determine the design-performance characteristics of the NACA eight-stage axial-flow compressor and the effect of altitude on the performance. The compressor was tested at simulated altitudes of 50,000; 36,000; and 27,000 feet at rotor speeds corresponding to compressor Mach numbers of 0.80, 0.85, 0.90, and 0.95 wit varying air flow at each speed.Mode of access: Internet.Axial flow compressorsAltitude, influence of.CompressorsTesting.Axial flow compressorsPerformance.Regan, Owen W.Aircraft Engine Research Laboratory.http://id.loc.gov/authorities/names/no2006105898http://id.loc.gov/rwo/agents/no2006105898http://viaf.org/viaf/123526082United States.National Advisory Committee for Aeronautics.http://id.loc.gov/authorities/names/n79060141http://id.loc.gov/rwo/agents/n79060141Technical Report Archive & Image Library (TRAIL)3901509501433110090338420241217210333.020250726000000.020260226140657.02026-02-27T09:08:37Z2024-04-02T17:30:02ZSDR-MIUmiuALMAprepare.pl-004-009BKsdr-miu.990139479240106381MiUSDRGWLA013947924mdp.39015095014331MIU990139479240106381MIUGWLA20260227googlemdp.390150950143311944pdbibUS fed doc