02072nam a2200409Ka 4500100167866MiAaHDL20250726000000.0m d cr bn ---auaua121101s1957 dcua b f000 0 eng d(MiU)990128618230106381sdr-miu.990128618230106381(MiU)MIU01000000000000012861823-goog(OCoLC)815650091(MiU)Aleph012861823NACARNACARUtOrBLWNACAY 3.N21/5:15/E56J16Rohlik, Harold E.Investigation of a 0.6 hub-tip radius-ratio transonic turbine designed for secondary-flow study.[Part] I,, Design and experimental performance of standard turbine /Harold E. Rohlik, William T. Wintucky and Herbert W. Scibbe..Design and experimental performance of standard turbineWashington, D.C. :National Advisory Committee for Aeronautics,1957.31 p. :ill. ;27 cm.texttxtrdacontentunmediatednrdamediavolumencrdacarrierNational Advisory Committee for Aeronautics research memorandum ;E56J16"January 9, 1957."Includes bibliographical references (p. 13-14).Mode of access: Internet.Aerodynamics, Supersonic.http://id.loc.gov/authorities/subjects/sh85001297Axial flow.http://id.loc.gov/authorities/subjects/sh2002010496TurbinesDesign and construction.Scibbe, Herbert W.Wintucky, William T.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)3901508646399210016786620241218002437.020250726000000.020260228140658.02026-03-01T06:51:34Z2024-04-21T17:30:02ZSDR-MIUmiuALMAprepare.pl-004-009BKsdr-miu.990128618230106381MiUSDRGWLA012861823mdp.39015086463992MIU990128618230106381MIUGWLA20260301googlemdp.390150864639921957pdbibUS fed doc