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| Titolo: |
Numerical methods for engine-airframe integration [[electronic resource] /] / edited by S.N.B. Murthy, Gerald C. Paynter
|
| Pubblicazione: | New York, N.Y., : American Institute of Aeronautics and Astronautics, Inc., c1986 |
| Descrizione fisica: | 1 online resource (555 p.) |
| Disciplina: | 629.134/31 |
| 629.1 s | |
| Soggetto topico: | Airframes - Design and construction |
| Airplanes - Motors | |
| Soggetto genere / forma: | Electronic books. |
| Altri autori: |
MurthyS. N. B
PaynterGerald C
|
| Note generali: | "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." |
| Nota di bibliografia: | Includes bibliographical references and index. |
| Nota di contenuto: | ""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"" | |
| Titolo autorizzato: | Numerical methods for engine-airframe integration ![]() |
| ISBN: | 1-60086-576-3 |
| 1-60086-357-4 | |
| Formato: | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione: | Inglese |
| Record Nr.: | 9910457214703321 |
| Lo trovi qui: | Univ. Federico II |
| Opac: | Controlla la disponibilità qui |