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Numerical methods for engine-airframe integration /

Detalles Bibliográficos
Clasificación:Libro Electrónico
Autores Corporativos: American Institute of Aeronautics and Astronautics, AIAA Aerospace Sciences Meeting
Otros Autores: Murthy, S. N. B., Paynter, Gerald C.
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

MARC

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245 0 0 |a Numerical methods for engine-airframe integration /  |c edited by S.N.B. Murthy, Gerald C. Paynter. 
260 |a New York, N.Y. :  |b American Institute of Aeronautics and Astronautics, Inc.,  |c ©1986. 
300 |a 1 online resource (xvi, 538 pages) :  |b illustrations 
336 |a text  |b txt  |2 rdacontent 
337 |a computer  |b c  |2 rdamedia 
338 |a online resource  |b cr  |2 rdacarrier 
490 1 |a Progress in astronautics and aeronautics ;  |v v. 102 
500 |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." 
504 |a Includes bibliographical references and index. 
505 0 |a Cover -- Title -- Copyright -- Table of Contents -- Preface -- Chapter I. Fundamental Considerations -- Scientific Computing Environment for the 1980s -- Prediction of Complex Turbulent Flows: An Overviewâ€?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 
505 8 |a 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 
505 8 |a 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 -- CFDâ€?A User's Technology Assessment -- Author Index 
590 |a ProQuest Ebook Central  |b Ebook Central Academic Complete 
650 0 |a Airframes  |x Design and construction  |v Congresses. 
650 0 |a Airplanes  |x Motors  |v Congresses. 
650 6 |a Avions  |x Moteurs  |v Congrès. 
650 7 |a Airframes  |x Design and construction  |2 fast 
650 7 |a Airplanes  |x Motors  |2 fast 
655 7 |a Conference papers and proceedings  |2 fast 
700 1 |a Murthy, S. N. B. 
700 1 |a Paynter, Gerald C. 
710 2 |a American Institute of Aeronautics and Astronautics. 
711 2 |a AIAA Aerospace Sciences Meeting  |n (22nd :  |d 1984 :  |c Reno, Nev.) 
776 0 8 |i Print version:  |t Numerical methods for engine-airframe integration.  |d New York, N.Y. : American Institute of Aeronautics and Astronautics, Inc., ©1986  |w (DLC) 86010920 
830 0 |a Progress in astronautics and aeronautics ;  |v v. 102. 
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