02304oam 2200601I 450 991071388770332120200824084829.0(CKB)5470000002504813(OCoLC)1104148279(EXLCZ)99547000000250481320190610d1954 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierAerodynamic investigation of a four-blade propeller operating through an angle-of-attack range from 0° to 180° /by H. Clyde McLemore and Michael D. CannonWashington, [D.C.] :National Advisory Committee for Aeronautics,1954.1 online resource (62 pages) illustrationsTechnical notes / National Advisory Committee for Aeronautics ;No. 3228"June 1954."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 15).Aerodynamic investigation of a four-blade propeller operating through an angle-of-attack range from 0 degrees to 180 degreesAngle of attack (Aerodynamics)Mathematical analysisPropellers, AerialTestingWind tunnel testingAngle of attack (Aerodynamics)fastMathematical analysisfastPropellers, AerialTestingfastWind tunnel testingfastAngle of attack (Aerodynamics)Mathematical analysis.Propellers, AerialTesting.Wind tunnel testing.Angle of attack (Aerodynamics)Mathematical analysis.Propellers, AerialTesting.Wind tunnel testing.McLemore H. Clyde1404416Cannon Michael D.United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOTRAALOCLCFGPOBOOK9910713887703321Aerodynamic investigation of a four-blade propeller operating through an angle-of-attack range from 0° to 1803478944UNINA