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Shock Wave Boundary Layer Interactions

Shock Wave Boundary Layer Interactions Author Holger Babinsky
ISBN-10 9781139498647
Release 2011-09-12
Pages
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Shock wave-boundary-layer interaction (SBLI) is a fundamental phenomenon in gas dynamics that is observed in many practical situations, ranging from transonic aircraft wings to hypersonic vehicles and engines. SBLIs have the potential to pose serious problems in a flowfield; hence they often prove to be a critical - or even design limiting - issue for many aerospace applications. This is the first book devoted solely to a comprehensive, state-of-the-art explanation of this phenomenon. It includes a description of the basic fluid mechanics of SBLIs plus contributions from leading international experts who share their insight into their physics and the impact they have in practical flow situations. This book is for practitioners and graduate students in aerodynamics who wish to familiarize themselves with all aspects of SBLI flows. It is a valuable resource for specialists because it compiles experimental, computational and theoretical knowledge in one place.



Fundamentals of Aerospace Navigation and Guidance

Fundamentals of Aerospace Navigation and Guidance Author Pierre T. Kabamba
ISBN-10 9781107070943
Release 2014-08-29
Pages 334
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This text covers fundamentals in navigation of modern aerospace vehicles. It is an excellent resource for both graduate students and practicing engineers.



Computational Aeroacoustics

Computational Aeroacoustics Author Christopher K. W. Tam
ISBN-10 9780521806787
Release 2012-09-28
Pages 481
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Both a textbook for graduate students with exercises and a reference with code for researchers in computational aeroacoustics (CAA).



Nonequilibrium Gas Dynamics and Molecular Simulation

Nonequilibrium Gas Dynamics and Molecular Simulation Author Iain D. Boyd
ISBN-10 9781107073449
Release 2017-03-23
Pages 400
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"The book is divided into two parts based on the overall goals, with the first part focusing on fundamental considerations, and the second part dedicated to describing computer simulation methods. The first section covers three different areas: (1) kinetic theory, (2) quantum mechanics, and (3) statistical mechanics. Important results from these three areas are then brought together to allow analysis of nonequilibrium processes in a gas based on molecular level considerations. Chapter 1 covers kinetic theory, in which the basic idea is to develop techniques to relate the properties and behavior of particles, representing atoms and molecules, to the fluid mechanical aspects of a gas at the macroscopic level. This requires us to provide a basic definition by what is meant by a particle, and how these particles interact with one another through the mechanism of inter-molecular collisions. This leads us into a discussion of modeling of macroscopic molecular transport processes, such as viscosity and thermal conductivity, that represents one of the first key successes of kinetic theory. We will find that kinetic theory relies on the use of statistical analysis techniques, such as probability density functions, due to the very large volumes of information involved in tracking the behavior of every single particle in a real gas flow"--



Boundary Layer Theory

Boundary Layer Theory Author Herrmann Schlichting
ISBN-10 3540662707
Release 2003-05-20
Pages 800
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A new edition of the almost legendary textbook by Schlichting completely revised by Klaus Gersten is now available. This book presents a comprehensive overview of boundary-layer theory and its application to all areas of fluid mechanics, with emphasis on the flow past bodies (e.g. aircraft aerodynamics). It contains the latest knowledge of the subject based on a thorough review of the literature over the past 15 years. Yet again, it will be an indispensable source of inexhaustible information for students of fluid mechanics and engineers alike.



Compressibility Turbulence and High Speed Flow

Compressibility  Turbulence and High Speed Flow Author Thomas B. Gatski
ISBN-10 9780123973184
Release 2013-03-05
Pages 342
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Compressibility, Turbulence and High Speed Flow introduces the reader to the field of compressible turbulence and compressible turbulent flows across a broad speed range, through a unique complimentary treatment of both the theoretical foundations and the measurement and analysis tools currently used. The book provides the reader with the necessary background and current trends in the theoretical and experimental aspects of compressible turbulent flows and compressible turbulence. Detailed derivations of the pertinent equations describing the motion of such turbulent flows is provided and an extensive discussion of the various approaches used in predicting both free shear and wall bounded flows is presented. Experimental measurement techniques common to the compressible flow regime are introduced with particular emphasis on the unique challenges presented by high speed flows. Both experimental and numerical simulation work is supplied throughout to provide the reader with an overall perspective of current trends. An introduction to current techniques in compressible turbulent flow analysis An approach that enables engineers to identify and solve complex compressible flow challenges Prediction methodologies, including the Reynolds-averaged Navier Stokes (RANS) method, scale filtered methods and direct numerical simulation (DNS) Current strategies focusing on compressible flow control



International Aerospace Abstracts

International Aerospace Abstracts Author
ISBN-10 STANFORD:36105021108068
Release 1998
Pages
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International Aerospace Abstracts has been writing in one form or another for most of life. You can find so many inspiration from International Aerospace Abstracts also informative, and entertaining. Click DOWNLOAD or Read Online button to get full International Aerospace Abstracts book for free.



Elements of Numerical Methods for Compressible Flows

Elements of Numerical Methods for Compressible Flows Author Doyle Knight
ISBN-10 0521554748
Release 2006-08-14
Pages 245
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The purpose of this book is to present the basic elements of numerical methods for compressible flows. It is appropriate for advanced undergraduate and graduate students and specialists working in high speed flows. The focus is on the unsteady one-dimensional Euler equations which form the basis for numerical algorithms in compressible fluid mechanics. The author believes it is therefore essential to understand the development and implementation of these algorithms in their original one-dimensional context. The text is supplemented by numerous end-of-chapter exercises.



AIAA 27th Aerospace Sciences Meeting

AIAA 27th Aerospace Sciences Meeting Author
ISBN-10 PSU:000016363557
Release 1989
Pages
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AIAA 27th Aerospace Sciences Meeting has been writing in one form or another for most of life. You can find so many inspiration from AIAA 27th Aerospace Sciences Meeting also informative, and entertaining. Click DOWNLOAD or Read Online button to get full AIAA 27th Aerospace Sciences Meeting book for free.



Turbulent Flows

Turbulent Flows Author S. B. Pope
ISBN-10 0521598869
Release 2000-08-10
Pages 771
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Graduate text on turbulent flow, an important topic in fluid mechanics.



Drag Reduction by Shock and Boundary Layer Control

Drag Reduction by Shock and Boundary Layer Control Author Egon Stanewsky
ISBN-10 9783540458562
Release 2013-11-11
Pages 452
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The survival of the Aeronautical Industries of Europe in the highly competitive World Aviation Market is strongly dependent on such factors as time-to-market of a new or derivative aircraft and on its manufacturing costs but also on the achievement of a competitive technological advantage by which an increased market share can be gained. Recognizing this, cooperative research is continuously encouraged and co-financed by the European Union in order to strengthen the scientific and technological base of the Aeronautical Industries thus providing - among others - the technological edge needed for survival. Corresponding targets of research within Area 3, Technologies for Transport Means, and here in particular Area 3A, Aeronautics Technologies, of the Industrial and Materials Technologies Program ( Brite -EuRam III, 1994 -1998) have been identified to be aircraft efficiency, cost effectiveness and environmental impact. Concerning aircraft efficiency - relevant to the present research - a reduction in aircraft drag of 10%, a reduction in aircraft fuel consumption of 30%, and a reduction in airframe, engine and system weight of 20% are envisaged. Meeting these objectives has, of course, also a strong positive impact on the environment.



A Collection of Technical Papers 04 2614 04 2702

A Collection of Technical Papers  04 2614   04 2702 Author
ISBN-10 PSU:000054737976
Release 2004
Pages
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A Collection of Technical Papers 04 2614 04 2702 has been writing in one form or another for most of life. You can find so many inspiration from A Collection of Technical Papers 04 2614 04 2702 also informative, and entertaining. Click DOWNLOAD or Read Online button to get full A Collection of Technical Papers 04 2614 04 2702 book for free.



General Continuum Mechanics

General Continuum Mechanics Author T. J. Chung
ISBN-10 9780521874069
Release 1988
Pages 424
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General Continuum Mechanics provides an integrated and unified study of continuum mechanics.



Aerospace Engineering Index

Aerospace Engineering Index Author
ISBN-10 UOM:39015024394309
Release 1950
Pages
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Aerospace Engineering Index has been writing in one form or another for most of life. You can find so many inspiration from Aerospace Engineering Index also informative, and entertaining. Click DOWNLOAD or Read Online button to get full Aerospace Engineering Index book for free.



Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports Author
ISBN-10 STANFORD:36105007168896
Release 1988
Pages
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Scientific and Technical Aerospace Reports has been writing in one form or another for most of life. You can find so many inspiration from Scientific and Technical Aerospace Reports also informative, and entertaining. Click DOWNLOAD or Read Online button to get full Scientific and Technical Aerospace Reports book for free.



The Aeronautical Journal

The Aeronautical Journal Author
ISBN-10 UOM:39015058914535
Release 2005
Pages
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The Aeronautical Journal has been writing in one form or another for most of life. You can find so many inspiration from The Aeronautical Journal also informative, and entertaining. Click DOWNLOAD or Read Online button to get full The Aeronautical Journal book for free.



Rotorcraft Aeromechanics

Rotorcraft Aeromechanics Author Wayne Johnson
ISBN-10 9781107355286
Release 2013-04-29
Pages
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A rotorcraft is a class of aircraft that uses large-diameter rotating wings to accomplish efficient vertical take-off and landing. The class encompasses helicopters of numerous configurations (single main rotor and tail rotor, tandem rotors, coaxial rotors), tilting proprotor aircraft, compound helicopters, and many other innovative configuration concepts. Aeromechanics covers much of what the rotorcraft engineer needs: performance, loads, vibration, stability, flight dynamics, and noise. These topics include many of the key performance attributes and the often-encountered problems in rotorcraft designs. This comprehensive book presents, in depth, what engineers need to know about modelling rotorcraft aeromechanics. The focus is on analysis, and calculated results are presented to illustrate analysis characteristics and rotor behaviour. The first third of the book is an introduction to rotorcraft aerodynamics, blade motion, and performance. The remainder of the book covers advanced topics in rotary wing aerodynamics and dynamics.