01586oam 2200445 450 991071652930332120210701112138.0(CKB)5470000002522865(OCoLC)890693636(EXLCZ)99547000000252286520140916j197212 ua 0engur|||||||||||txtrdacontentcrdamediacrrdacarrierNumerical method for design of minimum-drag supersonic wing camber with constraints on pitching moment and surface deformation /by Russell B. Sorrells and David S. MillerWashington, D.C. :National Aeronautics and Space Administration,December 1972.1 online resource (47 pages) illustrationsNASA/TN ;D-7097"December 1972."Includes bibliographical references (page 21).AerodynamicsnasatCambernasatWingsnasatAerodynamics.Camber.Wings.Sorrells Russell B.1414584Miller David S(Of Langley Research Center),United States.National Aeronautics and Space Administration,Langley Research Center.OCLCEOCLCEOCLCQGPOBOOK9910716529303321Numerical method for design of minimum-drag supersonic wing camber with constraints on pitching moment and surface deformation3514307UNINA