Mach 0 6 To 3 0 Flows Over Rectangular Cavities

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Mach 0.6 to 3.0 Flows Over Rectangular Cavities

Author : Louis G. Kaufman,Algirdas Maciulaitis,Rodney L. Clark
Publisher : Unknown
Page : 288 pages
File Size : 54,9 Mb
Release : 1983
Category : Aeroacoustics
ISBN : UOM:39015095307644

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Mach 0.6 to 3.0 Flows Over Rectangular Cavities by Louis G. Kaufman,Algirdas Maciulaitis,Rodney L. Clark Pdf

Internal weapons carriage in high performance aircraft is often adversely affected by the severe aeroacoustic environment produced with the weapons bay doors open. To obtain a better understanding of this fluid dynamic problem, basic static and oscillatory pressure data were obtained for Mach 0.6 to 3.0 flows over shallow rectangular cavities in a generic flat plate model. Cavity length to depth ratios were varied from approximately 5 to 10. Static pressure data characteristic of both open and closed cavity flows were obtained. An improved Rossiter method is presented that satisfactorily predicts the possible frequency modes within the cavity. Highest fluctuating pressure occurs on the aft bulkhead, peaking near Mach 1.5 for the conditions tested. Aeroacoustic levels are substantially reduced by installing suppression fences (spoilers) at subsonic and low supersonic conditions. Acoustic levels generally drop rapidly above Mach 1.5. (Author).

Progress in Hybrid RANS-LES Modelling

Author : Shia-Hui Peng,Piotr Doerffer,Werner Haase
Publisher : Springer Science & Business Media
Page : 361 pages
File Size : 55,7 Mb
Release : 2010-09-17
Category : Technology & Engineering
ISBN : 9783642141683

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Progress in Hybrid RANS-LES Modelling by Shia-Hui Peng,Piotr Doerffer,Werner Haase Pdf

Hybrid modelling of turbulent flows, combining RANS and LES techniques, has received increasing attention over the past decade to fill the gap between (U)RANS and LES computations in aerodynamic applications at industrially relevant Reynolds numbers. With the advantage of hybrid RANS-LES modelling approaches, being considerably more computationally efficient than full LES and more accurate than (U)RANS, particularly for unsteady aerodynamic flows, has motivated numerous research and development activities. These activities have been increasingly stimulated by the provision of modern computing facilities. The present book contains the contributions presented at the Third Symposium on Hybrid RANS-LES Methods, held in Gdansk, Poland, 10-12 June 2009. To a certain extent, this conference was a continuation of the first symposium taking place in Stockholm (Sweden, 2005) and the second in Corfu (Greece, 2007). Motivated by the extensive interest in the research community, the papers presented at the Corfu symposium were published by Springer in the book entitled “Advances in Hybrid RANS-LES Modelling” (in Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Vol. 97). At the Gdansk symposium, along with four invited keynotes, given respectively by S. Fu, U. Michel, M. Sillen and P. Spalart, another 28 papers were presented on the following topics: Unsteady RANS, LES, Improved DES Methods, Hybrid RANS-LES Methods, DES versus URANS and other Hybrid Methods, Modelli- related Numerical Issues and Industrial Applications. After the symposium all full papers have been further reviewed and revised for publication in the present book.

Separated Flows and Jets

Author : Victor V. Kozlov,Alexander Dovgal
Publisher : Springer Science & Business Media
Page : 907 pages
File Size : 50,8 Mb
Release : 2012-12-06
Category : Science
ISBN : 9783642844478

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Separated Flows and Jets by Victor V. Kozlov,Alexander Dovgal Pdf

Separated flows and jets are closely linked in a variety of applications. They are of great importance in various fields of fluid mechanics including vehicle efficiency, technical branches concerned with gas/liquid flows, atmospheric effects on various constructions, etc. Knowledge of the physics of separated flows and jets and the development of reliable control techniques are prerequisite for future progress in the field. These aspects were in focus during the IUTAM-Symposium which was held in Novosibirsk, 9-13 July, 1990. This volume contains a selection of papers presenting recent results of theoretical and numerical studies as well as experimental work on separated flows and jets. The topics include sub- and supersonic, laminar and turbulent separation as well as organized structures in separated flows and jets. The reader will find here the state of the art and major trends for research in this field of aero-hydrodynamics.

NASA Technical Paper

Author : Anonim
Publisher : Unknown
Page : 60 pages
File Size : 47,7 Mb
Release : 1991
Category : Science
ISBN : STANFORD:36105024800687

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NASA Technical Paper by Anonim Pdf

NASA Technical Paper

Author : United States. National Aeronautics and Space Administration
Publisher : Unknown
Page : 604 pages
File Size : 54,7 Mb
Release : 1990
Category : Aeronautics
ISBN : UOM:39015022359072

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NASA Technical Paper by United States. National Aeronautics and Space Administration Pdf

Recent Advances in Mechanical Engineering

Author : Anoop Kumar Shukla,Bhupendra Prakash Sharma,Ahmad Arabkoohsar,Pradeep Kumar
Publisher : Springer Nature
Page : 840 pages
File Size : 45,9 Mb
Release : 2023-06-18
Category : Science
ISBN : 9789819918942

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Recent Advances in Mechanical Engineering by Anoop Kumar Shukla,Bhupendra Prakash Sharma,Ahmad Arabkoohsar,Pradeep Kumar Pdf

This volume comprises the select proceedings of the 3rd Biennial International Conference on Future Learning Aspects of Mechanical Engineering (FLAME) 2022. It aims to provide a comprehensive and broad-spectrum picture of the state-of-the-art research and development in thermal, fluids, energy and process engineering, mechatronics, control and robotics, material science and engineering, solid mechanics and structural engineering, dynamics and control, engineering design, manufacturing and industrial engineering, automobile engineering. This volume will prove a valuable resource for researchers and professionals in mechanical engineering and allied fields.

NASA Technical Memorandum

Author : Anonim
Publisher : Unknown
Page : 246 pages
File Size : 54,7 Mb
Release : 1992
Category : Aeronautics
ISBN : UOM:39015031266573

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NASA Technical Memorandum by Anonim Pdf

Computational Fluid Dynamics 2010

Author : Alexander Kuzmin
Publisher : Springer Science & Business Media
Page : 902 pages
File Size : 47,5 Mb
Release : 2011-05-03
Category : Technology & Engineering
ISBN : 9783642178849

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Computational Fluid Dynamics 2010 by Alexander Kuzmin Pdf

The International Conference on Computational Fluid Dynamics is held every two years and brings together physicists, mathematicians and engineers to review and share recent advances in mathematical and computational techniques for modeling fluid flow. The proceedings of the 2010 conference (ICCFD6) held in St Petersburg, Russia, contain a selection of refereed contributions and are meant to serve as a source of reference for all those interested in the state of the art in computational fluid dynamics.

Index of N A S A Technical Publications

Author : United States. National Aeronautics and Space Administration
Publisher : Unknown
Page : 448 pages
File Size : 52,9 Mb
Release : 1960
Category : Electronic
ISBN : OSU:32435029092020

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Index of N A S A Technical Publications by United States. National Aeronautics and Space Administration Pdf

Applied Mechanics Reviews

Author : Anonim
Publisher : Unknown
Page : 686 pages
File Size : 47,5 Mb
Release : 1967
Category : Mechanics, Applied
ISBN : UCAL:C2682425

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Applied Mechanics Reviews by Anonim Pdf

Parallel Computational Fluid Dynamics 2003

Author : Boris Chetverushkin,Jacques Periaux,N. Satofuka,A. Ecer
Publisher : Elsevier
Page : 558 pages
File Size : 49,5 Mb
Release : 2004-05-06
Category : Mathematics
ISBN : 9780080473673

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Parallel Computational Fluid Dynamics 2003 by Boris Chetverushkin,Jacques Periaux,N. Satofuka,A. Ecer Pdf

The book is devoted to using of parallel multiprocessor computer systems for numerical simulation of the problems which can be described by the equations of continuum mechanics. Parallel algorithms and software, the problems of meta-computing are discussed in details, some results of high performance simulation of modern gas dynamic problems, combustion phenomena, plasma physics etc are presented. · Parallel Algorithms for Multidisciplinary Studies