01785oam 2200493I 450 991071519700332120201211093107.0(CKB)5470000002508039(OCoLC)761188102(EXLCZ)99547000000250803920111115j196808 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierCold-air investigation of effects of partial admission on performance of 3.75-inch mean-diameter single-stage axial-flow turbine /by Hugh A. KlassenWashington, D.C. :National Aeronautics and Space Administration,August 1968.1 online resource (19 pages) illustrationsNASA technical note ;TN D-4700"August 1968."Includes bibliographical references (page 19).TurbinesBladesTestingTurbinesDesign and constructionTurbinesBladesTestingfastTurbinesDesign and constructionfastTurbinesBladesTesting.TurbinesDesign and construction.TurbinesBladesTesting.TurbinesDesign and construction.Klassen Hugh A.1404884United States.National Aeronautics and Space Administration,Lewis Research Center.OCLCEOCLCEOCLCQOCLCFOCLCOOCLCQGPOBOOK9910715197003321Cold-air investigation of effects of partial admission on performance of 3.75-inch mean-diameter single-stage axial-flow turbine3480375UNINA