01851oam 2200541 450 991071667450332120210702144419.0(CKB)5470000002523418(OCoLC)23677387(OCoLC)761485743(OCoLC)890699916(EXLCZ)99547000000252341819910502j197302 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierEffect of a reduction in blade thickness on performance of a single-stage 20.32-centimeter mean-diameter turbine /by William J. Nusbaum and Milton G. KofskeyWashington, D.C. :National Aeronautics and Space Administration,February 1973.1 online resource (24 pages) illustrationsNASA/TN ;D-7128"February 1973."Includes bibliographical references (page 11).Gas-turbinesBladesGas-turbinesAerodynamicsGas-turbinesAerodynamicsfastGas-turbinesBladesfastGas-turbinesBlades.Gas-turbinesAerodynamics.Gas-turbinesAerodynamics.Gas-turbinesBlades.Nusbaum William J.1413835Kofskey Milton G.United States.National Aeronautics and Space Administration,Lewis Research Center.ABCABCAD#OCLCEOCLCQOCLCOOCLCFOCLCQCOPGPOBOOK9910716674503321Effect of a reduction in blade thickness on performance of a single-stage 20.32-centimeter mean-diameter turbine3538409UNINA