LEADER 03746nam 2200625 a 450 001 9910781405503321 005 20230213212250.0 010 $a1-60086-576-3 010 $a1-60086-357-4 035 $a(CKB)2550000000072645 035 $a(EBL)3111600 035 $a(SSID)ssj0000565833 035 $a(PQKBManifestationID)12224471 035 $a(PQKBTitleCode)TC0000565833 035 $a(PQKBWorkID)10533747 035 $a(PQKB)10166489 035 $a(Au-PeEL)EBL3111600 035 $a(CaPaEBR)ebr10516705 035 $a(OCoLC)922979001 035 $a(MiAaPQ)EBC3111600 035 $a(EXLCZ)992550000000072645 100 $a19860428d1986 uy 0 101 0 $aeng 135 $aurcn||||||||| 181 $ctxt 182 $cc 183 $acr 200 00$aNumerical methods for engine-airframe integration$b[electronic resource] /$fedited by S.N.B. Murthy, Gerald C. Paynter 210 $aNew York, N.Y. $cAmerican Institute of Aeronautics and Astronautics, Inc.$dc1986 215 $a1 online resource (555 p.) 225 1 $aProgress in astronautics and aeronautics ;$vv. 102 300 $a"Technical papers selected from the AIAA 22nd Aerospace Sciences Meeting, January 1984, subsequently revised for this volume, and papers especially invited by the editors for this volume." 311 $a0-930403-09-6 320 $aIncludes bibliographical references and index. 327 $a""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Preface""; ""Chapter I. Fundamental Considerations""; ""Scientific Computing Environment for the 1980's""; ""Prediction of Complex Turbulent Flows: An Overview 1985""; ""A Survey of Composite Grid Generation for General Three-Dimensional Regions""; ""Numerical Solutions of the Compressible Navier-Stokes Equations""; ""Chapter II. Scope and Opportunities""; ""Elements of Computational Engine/Airframe Integration""; ""Computational Requirements for Efficient Engine Installation"" 327 $a""Application of CAE and CFD Techniques to Complete Tactical Missile Design"" ""Chapter III. Inviscid and Inviscid Plus Boundary-Layer Methods""; ""CFD Applications to Engine/Airframe Integration""; ""Three-Dimensional Flow Analysis of Turboprop Inlet and Nacelle Configurations""; ""Application of Computational Methods to the Design of Large Turbofan Engine Nacelles""; ""Comparison of Full Potential and Euler Solution Algorithms for Aeropropulsive Flowfield Computations""; ""Subsonic/Transonic/Supersonic Nozzle Flows and Nozzle Integration"" 327 $a""Chapter IV. Viscous/Inviscid Interaction and Navier-Stokes Methods"" ""Subsonic/Transonic Prediction Capabilities for Nozzle/Afterbody Configurations""; ""Three-Dimensional Viscous Design Methodology of Supersonic Inlet Systems for Advanced Technology Aircraft""; ""Review of Inlet/Airframe Integration Using Navier-Stokes Computational Fluid Dynamics""; ""Chapter V. Summary and Conclusions""; ""CFD A User's Technology Assessment""; ""Author Index"" 410 0$aProgress in astronautics and aeronautics ;$vv. 102. 606 $aAirframes$xDesign and construction$vCongresses 606 $aAirplanes$xMotors$vCongresses 615 0$aAirframes$xDesign and construction 615 0$aAirplanes$xMotors 676 $a629.134/31 676 $a629.1 s 701 $aMurthy$b S. N. B$013320 701 $aPaynter$b Gerald C$01513841 712 02$aAmerican Institute of Aeronautics and Astronautics. 712 12$aAIAA Aerospace Sciences Meeting$d(22nd :$f1984 :$eReno, Nev.) 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910781405503321 996 $aNumerical methods for engine-airframe integration$93748499 997 $aUNINA