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Numerical methods for engine-airframe integration /
| Clasificación: | Libro Electrónico |
|---|---|
| Autores Corporativos: | , |
| Otros Autores: | , |
| Formato: | Electrónico Congresos, conferencias eBook |
| Idioma: | Inglés |
| Publicado: |
New York, N.Y. :
American Institute of Aeronautics and Astronautics, Inc.,
©1986.
|
| Colección: | Progress in astronautics and aeronautics ;
v. 102. |
| Temas: | |
| Acceso en línea: | Texto completo |
Tabla de Contenidos:
- 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 DesignChapter 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 MethodsSubsonic/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