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|a TL671.6
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082 |
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4 |
|a 629.134/31
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049 |
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|a UAMI
|
245 |
0 |
0 |
|a Numerical methods for engine-airframe integration /
|c edited by S.N.B. Murthy, Gerald C. Paynter.
|
260 |
|
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|a New York, N.Y. :
|b American Institute of Aeronautics and Astronautics, Inc.,
|c ©1986.
|
300 |
|
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|a 1 online resource (xvi, 538 pages) :
|b illustrations
|
336 |
|
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|a text
|b txt
|2 rdacontent
|
337 |
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|a computer
|b c
|2 rdamedia
|
338 |
|
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|a online resource
|b cr
|2 rdacarrier
|
490 |
1 |
|
|a Progress in astronautics and aeronautics ;
|v v. 102
|
500 |
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|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 |
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|a Includes bibliographical references and index.
|
505 |
0 |
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|a 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
|
505 |
8 |
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|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 |
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|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 -- CFD�A User's Technology Assessment -- Author Index
|
590 |
|
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|a ProQuest Ebook Central
|b Ebook Central Academic Complete
|
650 |
|
0 |
|a Airframes
|x Design and construction
|v Congresses.
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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 |
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|a Murthy, S. N. B.
|
700 |
1 |
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|a Paynter, Gerald C.
|
710 |
2 |
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|a American Institute of Aeronautics and Astronautics.
|
711 |
2 |
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|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.
|
856 |
4 |
0 |
|u https://ebookcentral.uam.elogim.com/lib/uam-ebooks/detail.action?docID=3111600
|z Texto completo
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