01880oam 2200529 450 991071672710332120210827125529.0(CKB)5470000002524907(OCoLC)1159597625(EXLCZ)99547000000252490720200623d1937 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierFuselage-drag tests in the variable-density wind tunnel streamline bodies of revolution, fineness ratio of 5 /by Ira H. AbbottWashington, [D.C.] :National Advisory Committee for Aeronautics,1937.1 online resource (11 pages, 5 unnumbered pages) illustrationsTechnical note / National Advisory Committee for Aeronautics ;No. 614"September 1937."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 8).Fuselage-drag tests in the variable-density wind tunnel AirplanesFuselageDrag (Aerodynamics)Wind tunnel testingAirplanesFuselagefastDrag (Aerodynamics)fastWind tunnel testingfastAirplanesFuselage.Drag (Aerodynamics)Wind tunnel testing.AirplanesFuselage.Drag (Aerodynamics)Wind tunnel testing.Abbott Ira H. A.1418987United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFGPOBOOK9910716727103321Fuselage-drag tests in the variable-density wind tunnel3534463UNINA