01893nam 2200493I 450 991070403160332120151030161002.0(CKB)5470000002437340(OCoLC)927176907(EXLCZ)99547000000243734020151030j198507 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierUse of hyperbolic grid generation scheme in simulating supersonic viscous flow about three-dimensional winged configurations / Yehia M. Rizk, Joseph L. Steger, Denny S. ChausseMoffett Field, CA :National Aeronautics and Space Administration, Ames Research Center,July 1985.1 online resource (13 pages) illustrationsNASA technical memorandum ;86776Title from title screen (viewed Oct. 30, 2015)."July 1985."Includes bibliographical references (page 7).Computational gridsnasatGrid generation (mathematics)nasatSpace Shuttle orbitersnasatSupersonic flownasatAerodynamic configurationsnasatComputational grids.Grid generation (mathematics)Space Shuttle orbiters.Supersonic flow.Aerodynamic configurations.Rizk Yehia M.1395177Steger Joseph L.Chausse Denny S.Ames Research Center,United States.National Aeronautics and Space Administration,GPOGPOBOOK9910704031603321Use of hyperbolic grid generation scheme in simulating supersonic viscous flow about three-dimensional winged configurations3453244UNINA