01951oam 2200577I 450 991071388650332120200824105309.0(CKB)5470000002504825(OCoLC)1104148277(EXLCZ)99547000000250482520190610d1954 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierAerodynamic forces, moments, and stability derivatives for slender bodies of general cross section /by Alvin H. SacksWashington, [D.C.] :National Advisory Committee for Aeronautics,1954.1 online resource (74 pages) illustrationsTechnical notes / National Advisory Committee for Aeronautics ;No. 3283"November 1954."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (pages 53-54).AerodynamicsAirplanesMathematical analysisStability of airplanesAerodynamicsfastAirplanesfastMathematical analysisfastStability of airplanesfastAerodynamics.Airplanes.Mathematical analysis.Stability of airplanes.Aerodynamics.Airplanes.Mathematical analysis.Stability of airplanes.Sacks Alvin H.1399803United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOTRAALOCLCFGPOBOOK9910713886503321Aerodynamic forces, moments, and stability derivatives for slender bodies of general cross section3465730UNINA