Numerical Methods for Engine-Airframe Integration.

Cover -- Title -- Copyright -- Table of Contents -- Preface -- Chapter I. Fundamental Considerations -- Scientific Computing Environment for the 1980s -- 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.

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Electronic reproduction. Ann Arbor, Michigan : ProQuest Ebook Central, 2024. Available via World Wide Web. Access may be limited to ProQuest Ebook Central affiliated libraries.