02120oam 2200625I 450 991071388860332120200821144741.0(CKB)5470000002504804(OCoLC)1104148123(EXLCZ)99547000000250480420190610d1954 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierAerodynamics of slender wings and wing-body combinations having swept trailing edges /by Harold MirelsWashington, [D.C.] :National Advisory Committee for Aeronautics,1954.1 online resource (ii, 96 pages) illustrationsTechnical notes / National Advisory Committee for Aeronautics ;No. 3105"March 1954."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (pages 73-75).AerodynamicsAir flowAirplanesWings, Swept-backIntegral equationsTrailing edges (Aerodynamics)AerodynamicsfastAir flowfastAirplanesWings, Swept-backfastIntegral equationsfastTrailing edges (Aerodynamics)fastAerodynamics.Air flow.AirplanesWings, Swept-back.Integral equations.Trailing edges (Aerodynamics)Aerodynamics.Air flow.AirplanesWings, Swept-back.Integral equations.Trailing edges (Aerodynamics)Mirels Harold1416564United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOTRAALOCLCFGPOBOOK9910713888603321Aerodynamics of slender wings and wing-body combinations having swept trailing edges3527533UNINA