Flight Dynamics
ISBN: 9780691114071 / Angielski / Twarda / 864 str. Termin realizacji zamówienia: ok. 5-8 dni roboczych.
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cena:
576,61 zł |
Direct Methods for Solving the Boltzmann Equation and Study of Nonequilibrium Flows
ISBN: 9780792368311 / Angielski / Twarda / 302 str. Termin realizacji zamówienia: ok. 5-8 dni roboczych. This book is concerned with the methods of solving the nonlinear Boltz mann equation and of investigating its possibilities for describing some aerodynamic and physical problems. This monograph is a sequel to the book 'Numerical direct solutions of the kinetic Boltzmann equation' (in Russian) which was written with F. G. Tcheremissine and published by the Computing Center of the Russian Academy of Sciences some years ago. The main purposes of these two books are almost similar, namely, the study of nonequilibrium gas flows on the basis of direct integration of the kinetic equations....
This book is concerned with the methods of solving the nonlinear Boltz mann equation and of investigating its possibilities for describing some aerody...
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cena:
390,87 zł |
Direct Methods for Solving the Boltzmann Equation and Study of Nonequilibrium Flows
ISBN: 9781402003882 / Angielski / Miękka / 302 str. Termin realizacji zamówienia: ok. 5-8 dni roboczych. This book is concerned with the methods of solving the nonlinear Boltz mann equation and of investigating its possibilities for describing some aerodynamic and physical problems. This monograph is a sequel to the book 'Numerical direct solutions of the kinetic Boltzmann equation' (in Russian) which was written with F. G. Tcheremissine and published by the Computing Center of the Russian Academy of Sciences some years ago. The main purposes of these two books are almost similar, namely, the study of nonequilibrium gas flows on the basis of direct integration of the kinetic equations....
This book is concerned with the methods of solving the nonlinear Boltz mann equation and of investigating its possibilities for describing some aerody...
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cena:
429,96 zł |
Kinetic Theory of Gases in Shear Flows: Nonlinear Transport
ISBN: 9781402014369 / Angielski / Twarda / 319 str. Termin realizacji zamówienia: ok. 5-8 dni roboczych. The kinetic theory of gases as we know it dates to the paper of Boltzmann in 1872. The justification and context of this equation has been clarified over the past half century to the extent that it comprises one of the most complete examples of many-body analyses exhibiting the contraction from a microscopic to a mesoscopic description. The primary result is that the Boltzmann equation applies to dilute gases with short ranged interatomic forces, on space and time scales large compared to the corresponding atomic scales. Otherwise, there is no a priori limitation on the state of the system....
The kinetic theory of gases as we know it dates to the paper of Boltzmann in 1872. The justification and context of this equation has been clarified o...
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cena:
586,33 zł |
Mathematical Methods in Aerodynamics
ISBN: 9781402016639 / Angielski / Twarda / 573 str. Termin realizacji zamówienia: ok. 5-8 dni roboczych. The researchers in Aerodynamics know that there is not a unitary method of investigation in this field. The first mathematical model of the air- plane wing, the model meaning the integral equation governing the phe- nomenon, was proposed by L. Prandtl in 1918. The integral equation deduced by Prandtl, on the basis of some assumptions which will be specified in the sequeL furnishes the circulation C(y) (see Chapter 6). U sing the circulation, one calculates the lift and moment coefficients, which are very important in Aerodynamics. The first hypothesis made by Prandtl consists in replacing the...
The researchers in Aerodynamics know that there is not a unitary method of investigation in this field. The first mathematical model of the air- plane...
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cena:
781,79 zł |
Boundary Element Methods in Nonlinear Fluid Dynamics: Developments in Boundary Element Methods - 6
ISBN: 9781851664290 / Angielski / Twarda / 368 str. Termin realizacji zamówienia: ok. 5-8 dni roboczych. This volume demonstrates that boundary element methods are both elegant and efficient in their application to time dependent time harmonic problems in engineering and therefore worthy of considerable development.
This volume demonstrates that boundary element methods are both elegant and efficient in their application to time dependent time harmonic problems in...
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cena:
2086,77 zł |
Aircraft Performance Explanation for Takeoff from a High Altitude Airport
ISBN: 9783836483438 / Angielski / Miękka / 112 str. Termin realizacji zamówienia: ok. 5-8 dni roboczych. Pilots must be provided explanations, predictions, factors of safety and control for high density altitude environments. Anytime a higher than standard temperature exists at a departure airport, improper planning and/or a lack of knowledge may lead to a fatal outcome. Attempting takeoff without a thorough knowledge and understanding of high density altitude takeoff parameters are known to be contributing factors in general aviation takeoff accidents. A critical ethnographic study was conducted to reveal cultural differences among the general aviation community, air carrier, and commuter and...
Pilots must be provided explanations, predictions, factors of safety and control for high density altitude environments. Anytime a higher than standar...
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cena:
225,35 zł |
Organizational Accidents in an Air Force - Brazilian Squadron Commanders' Perceptions
ISBN: 9783836483490 / Angielski / Miękka / 168 str. Termin realizacji zamówienia: ok. 5-8 dni roboczych. Despite the ongoing preventive actions, supervision failure remains the most serious contributor to aircraft accidents in the Brazilian Air Force (FAB). The Organizational Accidents Theory, introduced by James Reason (1997), focuses on the preexisting conditions that result from fallible decisions made by top management. Squadron Commanders are the managers who deal directly with frontline operations in the FAB, becoming the last managerial barriers to counteract flaw top-down decision-makings. The purpose of this study aims to assess squadron commanders perceptions regarding the theory of...
Despite the ongoing preventive actions, supervision failure remains the most serious contributor to aircraft accidents in the Brazilian Air Force (FAB...
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cena:
312,73 zł |
Vortex Dynamics, Statistical Mechanics, and Planetary Atmospheres
ISBN: 9789812839138 / Angielski / Miękka / 224 str. Termin realizacji zamówienia: ok. 5-8 dni roboczych. Vortex Dynamics, Statistical Mechanics, and Planetary Atmospheres introduces the reader with a background in either fluid mechanics or statistical mechanics to the modeling of planetary atmospheres by barotropic and shallow-water models. These potent models are introduced in both analytical and numerical treatments highlighting the ways both approaches inform and enlighten the other. This book builds on Vorticity, Statistical Mechanics, and Monte Carlo Simulations by Lim and Nebus in providing a rare introduction to this intersection of research fields. While the book reaches the cutting edge...
Vortex Dynamics, Statistical Mechanics, and Planetary Atmospheres introduces the reader with a background in either fluid mechanics or statistical mec...
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cena:
318,23 zł |
Vortex Dynamics, Statistical Mechanics, and Planetary Atmospheres
ISBN: 9789812839121 / Angielski / Twarda / 224 str. Termin realizacji zamówienia: ok. 5-8 dni roboczych. Introduces the reader with a background in either fluid mechanics or statistical mechanics to the modeling of planetary atmospheres by barotropic and shallow-water models. This book builds on Vorticity, Statistical Mechanics, and Monte Carlo Simulations by Lim and Nebus in providing a rare introduction to this intersection of research fields.
Introduces the reader with a background in either fluid mechanics or statistical mechanics to the modeling of planetary atmospheres by barotropic and ...
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cena:
547,77 zł |
Vortex Wakes of Aircrafts
ISBN: 9783642017599 / Angielski / Twarda / 172 str. Termin realizacji zamówienia: ok. 5-8 dni roboczych. Investigation of vortex wakes behind various aircraft, especially behind wide bodied and heavy cargo ones, is of both scientific and practical in terest. The vortex wakes shed from the wing s trailing edge are long lived and attenuate only atdistances of10 12kmbehindthe wake generating aircraft. The encounter of other aircraft with the vortex wake of a heavy aircraft is open to catastrophic hazards. For example, air refueling is adangerous operationpartly due to thepossibility of the receiver aircraft s encountering the trailing wake of the tanker aircraft. It is very important to know the...
Investigation of vortex wakes behind various aircraft, especially behind wide bodied and heavy cargo ones, is of both scientific and practical in tere...
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cena:
390,87 zł |
Kinetic Theory of Gases in Shear Flows: Nonlinear Transport
ISBN: 9789048163472 / Angielski / Miękka / 319 str. Termin realizacji zamówienia: ok. 5-8 dni roboczych. This monograph provides a comprehensive study about how a dilute gas described by the Boltzmann equation responds under extreme nonequilibrium conditions. This response is basically characterized by nonlinear transport equations relating fluxes and hydrodynamic gradients through generalized transport coefficients that depend on the strength of the gradients. In addition, many interesting phenomena (e.g. chemical reactions or other processes with a high activation energy) are strongly influenced by the population of particles with an energy much larger than the thermal velocity, what... This monograph provides a comprehensive study about how a dilute gas described by the Boltzmann equation responds under extreme nonequilibrium cond... |
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cena:
586,33 zł |
Mathematical Methods in Aerodynamics
ISBN: 9789048164455 / Angielski / Miękka / 573 str. Termin realizacji zamówienia: ok. 5-8 dni roboczych. The researchers in Aerodynamics know that there is not a unitary method of investigation in this field. The first mathematical model of the air plane wing, the model meaning the integral equation governing the phe nomenon, was proposed by L. Prandtl in 1918. The integral equation deduced by Prandtl, on the basis of some assumptions which will be specified in the sequeL furnishes the circulation C(y) (see Chapter 6). U sing the circulation, one calculates the lift and moment coefficients, which are very important in Aerodynamics. The first hypothesis made by Prandtl consists in replacing the...
The researchers in Aerodynamics know that there is not a unitary method of investigation in this field. The first mathematical model of the air plane ...
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cena:
781,79 zł |
SolidWorks Ultimate Training
ISBN: 9781456728144 / Angielski / Miękka / 808 str. Termin realizacji zamówienia: ok. 5-8 dni roboczych. The many uses of SolidWorks Software is enormous and covering all its capabilities in any single book, is quite impossible however most topics to get the Student/Design Engineer to understand the easy and simple approach to design, has been well explained. The Tutorials started by introducing the Student/Design Engineer to New tools and their location and uses. Examples of processes were explained step by step with loads of practical references and different approach to design covered. Topics that included, but not limited to, Sheet metal design, Weldments, Equations and Configuration,...
The many uses of SolidWorks Software is enormous and covering all its capabilities in any single book, is quite impossible however most topics to get ...
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cena:
439,70 zł |
Vortex Wakes of Aircrafts
ISBN: 9783642242465 / Angielski / Miękka / 154 str. Termin realizacji zamówienia: ok. 5-8 dni roboczych. Investigation of vortex wakes behind various aircraft, especially behind wide bodied and heavy cargo ones, is of both scientific and practical in terest. The vortex wakes shed from the wing s trailing edge are long lived and attenuate only atdistances of10 12kmbehindthe wake generating aircraft. The encounter of other aircraft with the vortex wake of a heavy aircraft is open to catastrophic hazards. For example, air refueling is adangerous operationpartly due to thepossibility of the receiver aircraft s encountering the trailing wake of the tanker aircraft. It is very important to know the...
Investigation of vortex wakes behind various aircraft, especially behind wide bodied and heavy cargo ones, is of both scientific and practical in tere...
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cena:
390,87 zł |
Understanding Aerodynamics: Arguing from the Real Physics
ISBN: 9781119967514 / Angielski / Twarda / 576 str. Termin realizacji zamówienia: ok. 5-8 dni roboczych. Much-needed, fresh approach that brings a greater insight into the physical understanding of aerodynamics
Based on the author's decades of industrial experience with Boeing, this book helps students and practicing engineers to gain a greater physical understanding of aerodynamics. Relying on clear physical arguments and examples, Mclean provides a much-needed, fresh approach to this sometimes contentious subject without shying away from addressing -real- aerodynamic situations as opposed to the oversimplified ones frequently used for mathematical convenience. Motivated by the belief... Much-needed, fresh approach that brings a greater insight into the physical understanding of aerodynamics
Based on the author's decades of i... |
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cena:
444,54 zł |
NASA's Contributions to Aeronuatics Volume I: Aerodynamics, Structures, Propulsion, Controls
ISBN: 9781782663010 / Angielski / Miękka / 970 str. Termin realizacji zamówienia: ok. 5-8 dni roboczych. NASA publication NASA SP 2010-570 Volume one of a two-volume collection of case studies on aspects of NACA-NASA research by noted engineers, airmen, historians, museum curators, journalists, and independent scholars. Explores various aspects of how NACA-NASA research took aeronautics from the subsonic to the hypersonic era. Illustrated.
NASA publication NASA SP 2010-570 Volume one of a two-volume collection of case studies on aspects of NACA-NASA research by noted engineers, airmen, h...
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cena:
173,16 zł |
The Simple Science of Flight: From Insects to Jumbo Jets
ISBN: 9780262513135 / Angielski / Miękka / 216 str. Termin realizacji zamówienia: ok. 5-8 dni roboczych. From the smallest gnat to the largest aircraft, all things that fly obey the same aerodynamic principles. In The Simple Science of Flight, Henk Tennekes investigates just how machines and creatures fly: what size wings they need, how much energy is required for their journeys, how they cross deserts and oceans, how they take off, climb, and soar. Fascinated by the similarities between nature and technology, Tennekes offers an introduction to flight that teaches by association. Swans and Boeings differ in numerous ways, but they follow the same aerodynamic principles. Biological evolution... From the smallest gnat to the largest aircraft, all things that fly obey the same aerodynamic principles. In The Simple Science of Flight, Henk Ten... |
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cena:
129,35 zł |
Flight Vehicle Aerodynamics
ISBN: 9780262526449 / Angielski / Miękka / 279 str. Termin realizacji zamówienia: ok. 5-8 dni roboczych. This book offers a general overview of the physics, concepts, theories, and models underlying the discipline of aerodynamics. A particular focus is the technique of velocity field representation and modeling via source and vorticity fields and via their sheet, filament, or point-singularity idealizations. These models provide an intuitive feel for aerodynamic flow-field behavior and are the basis of aerodynamic force analysis, drag decomposition, flow interference estimation, and other important applications. The models are applied to both low speed and high speed flows. Viscous flows are... This book offers a general overview of the physics, concepts, theories, and models underlying the discipline of aerodynamics. A particular focus is... |
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cena:
346,65 zł |
Aeroelastic Vibrations and Stability of Plates and Shells
ISBN: 9783110338362 / Angielski / Twarda / 231 str. Termin realizacji zamówienia: ok. 5-8 dni roboczych. Back-action of aerodynamics onto structures such as wings cause vibrations and may resonantly couple to them, thus causing instabilities (flutter) and endangering the whole structure. By careful choices of geometry, materials and damping mechanisms, hazardous effects on wind engines, planes, turbines and cars can be avoided. Besides an introduction into the problem of flutter, new formulations of flutter problems are given as well as a treatise of supersonic flutter and of a whole range of mechanical effects. Numerical and analytical methods to study them are developed and applied... Back-action of aerodynamics onto structures such as wings cause vibrations and may resonantly couple to them, thus causing instabilities (flutter) ... |
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cena:
1048,57 zł |