03779nam 2200637 a 450 991045721470332120200520144314.01-60086-576-31-60086-357-4(CKB)2550000000072645(EBL)3111600(SSID)ssj0000565833(PQKBManifestationID)12224471(PQKBTitleCode)TC0000565833(PQKBWorkID)10533747(PQKB)10166489(MiAaPQ)EBC3111600(Au-PeEL)EBL3111600(CaPaEBR)ebr10516705(OCoLC)922979001(EXLCZ)99255000000007264519860428d1986 uy 0engurcn|||||||||txtccrNumerical methods for engine-airframe integration[electronic resource] /edited by S.N.B. Murthy, Gerald C. PaynterNew York, N.Y. American Institute of Aeronautics and Astronautics, Inc.c19861 online resource (555 p.)Progress in astronautics and aeronautics ;v. 102"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."0-930403-09-6 Includes bibliographical references and index.""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""""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""""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""Progress in astronautics and aeronautics ;v. 102.AirframesDesign and constructionCongressesAirplanesMotorsCongressesElectronic books.AirframesDesign and constructionAirplanesMotors629.134/31629.1 sMurthy S. N. B13320Paynter Gerald C928444American Institute of Aeronautics and Astronautics.AIAA Aerospace Sciences Meeting(22nd :1984 :Reno, Nev.)MiAaPQMiAaPQMiAaPQBOOK9910457214703321Numerical methods for engine-airframe integration2086788UNINA