01840oam 2200517 450 991071590150332120210427123524.0(CKB)5470000002517085(OCoLC)785286626(OCoLC)56097993(OCoLC)761200027(EXLCZ)99547000000251708520120408j196812 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierTheory for computing span loads and stability derivatives due to sideslip, yawing, and rolling for wings in subsonic compressible flow /by M.J. QueijoWashington, D.C. :National Aeronautics and Space Administration,December 1968.1 online resource (76 pages) illustrationsNASA/TN ;D-4929"December 1968."Includes bibliographical references (pages 40-41).Compressible flownasatStability derivativesnasatAirplanesWingsAerodynamicsfastRolling (Aerodynamics)fastYawing (Aerodynamics)fastCompressible flow.Stability derivatives.AirplanesWingsAerodynamics.Rolling (Aerodynamics)Yawing (Aerodynamics)Queijo M. J.1401855United States.National Aeronautics and Space Administration,OCLCEOCLCEEGMAD#OCLCQOCLCFOCLCQGPOBOOK9910715901503321Theory for computing span loads and stability derivatives due to sideslip, yawing, and rolling for wings in subsonic compressible flow3471141UNINA