01401nam a2200313Ia 4500011433273MiAaHDL20141009010000.0m d cr bn ---auaua071120s1975 dcua b 000 0 eng dsdr-uiuc6390550(OCoLC)181643627EGMEGMUIUUHaas, Jeffrey E.Cold-air performance of a 12.766-centimeter-tip-diameter axial-flow cooled turbine.I,Design and performance of a solid blade configuration /Jeffrey E. Haas, Milton G. Kofskey.NASA TN D-7881Washington, D.C. :National Aeronautics and Space Administration ;Springfield, VA :For sale by the Clearinghouse for Federal Scientific and Technical Information,1975.21 p. :ill. ;27 cm.NASA technical note ;D-7881Prepared by Lewis Research Center and U.S. Army Air Mobility R&D Laboratory, Cleveland, Ohio, 44135.Includes bibliographical references (p. 11-12).Mode of access: Internet.TurbinesCooling.Gas-turbines.Axial flow.TurbinesTestingPerformance.Kofskey, Milton G.U.S. Army Air Mobility Research and Development Laboratory.Lewis Research Center.United States.National Aeronautics and Space Administration.01143327320101101161430.020141009010000.020141112164151.02026-01-21T19:18:46Z2026-01-21T18:30:03Z2019-10-29T20:00:02ZSDR-UIUCUNKNOWNloader.pl-003-020BKsdr-uiuc6390550uiugSDRUIUCuiug.30112106633321UIU6390550UIUUIUC20260121googleuiug.301121066333211975pdusgfv