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Keywords: aerodynam
Your search found 33 books Now viewing Books 1 - 25 In stock items ship IMMEDIATELY. Other titles usually ship within 2-3 days. |
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| AeroDYNAMIC 3.0 | |||||||
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| A Microsoft Windowsô based software package on DVD, titled AeroDYNAMIC, provides a single integrated package with one universal user interface providing access to virtual laboratories, simulations, and design synthesis and analysis software based on the methods presented in the text. Pentium III or better and 128 Mb of RAM; Microsoft Office XP and a web browser like Netscape or Microsoft Internet Explorer. | |||||||
| AIAA | ISBN-10: 1563476894 ISBN-13: 9781563476891 | PGS: 0 | List: 94.95 YOUR PRICE: 90.20 | ||||
| Aerodynamics and Ventilation of Vehicle Tunnels (BHR Group Publication 43) | |||||||
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| WILEY | H | ISBN-10: 1860582559 ISBN-13: 9781860582554 | PGS: 1092 | List: 905.00 YOUR PRICE: 859.75 | |||
| Aerodynamics for Engineering Students | |||||||
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| Already established as the leading course text on aerodynamics, Aerodynamics for Engineering Students has been revised to include the latest developments in flow control and boundary layers, and their influence on modern wing design, as well as introducing recent advances in the understanding of fundamental fluid dynamics. Computational methods have been expanded and updated to reflect the modern approaches to aerodynamic design and research in the aeronautical industry and elsewhere, and the structure of the text has been developed to reflect current course requirements. The book is designed to be accessible and practical. Theory is developed logically within each chapter with notation, symbols and units well defined throughout, and the text is fully illustrated with worked examples and exercises. The classic text, expanded and updated. Includes latest developments in flow control, boundary layers and fluid dynamics. Fully illustrated throughout with illustrations, worked examples and exercises. | |||||||
| Butterworth-Heinemann - ELSEVIER | S | ISBN-10: 0750651113 ISBN-13: 9780750651110 | PGS: 608 | List: 72.95 YOUR PRICE: 69.30 | |||
| Aerodynamics for Engineers, 5th Ed. | |||||||
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(NOTE: Each section contains a Summary, Problems, and References) 1. Fluid Properties.
Concept of a Fluid. Fluid as a Continuum. Fluid Properties. Pr | |||||||
| Prentice Hall - PEARSON | H | ISBN-10: 0132272687 ISBN-13: 9780132272681 | PGS: N/A | List: 169.00 YOUR PRICE: 160.55 | |||
| AERODYNAMICS LARGE BRIDGES, 1st Ed. | |||||||
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| Taylor & Francis | H | ISBN-10: 9054100427 ISBN-13: 9789054100423 | PGS: N/A | List: 195.95 YOUR PRICE: 186.15 | |||
| Aerodynamics, Aeronautics, and Flight Mechanics, 2nd Edition | |||||||
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| Fluid Mechanics. Lift. Drag. Lift and Drag at High Mach Numbers. The Production of Thrust. Airplane Performance. Helicopters and V/STOL Aircraft. Static Stability and Control. Open-Loop Dynamic Stability and Control. Controlled Motion and Automatic Stability. Appendices. Index. | |||||||
| Wiley | H | ISBN-10: 0471575062 ISBN-13: 9780471575061 | PGS: N/A | List: 161.95 YOUR PRICE: 153.85 | |||
| APPLIED COMPUTATIONAL AERODYNAMICS | |||||||
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| Richly Illustrated Chapters Feature Types of Problems Ranging From the Classic Airfoil Problem to the Complexity of Complete Aircraft Such as the 737, 7J7, the F-16, & the Space Shuttle Launch Configuration. Applications for Components Are Also Detailed, Including Wings, High-Lift Systems, Propulsion System Components, & Rotors. | |||||||
| AIAA | H | ISBN-10: 093040369X ISBN-13: 9780930403690 | PGS: 925 | List: 110.95 YOUR PRICE: 105.40 | |||
| APPROXIMATE METHODS FOR WEAPON AERODYNAMICS | |||||||
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| The book reviews all approaches to calculate aerodynamics, allowing engineers to see the pros and cons of each approach, setting the stage sor a semiemprical approach. It contains many approximate aerodynamic methods, bringing together in a single text both linearized and nonlinear aerodynamics methods | |||||||
| AIAA | H | ISBN-10: 1563473992 ISBN-13: 9781563473999 | PGS: 464 | List: 105.95 YOUR PRICE: 100.65 | |||
| BASIC HELEICOPTER AERODYNAMICS, 2nd Ed. | |||||||
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| Contents: Inftroduction * Rotor in Vertical Flight: Momentum Theory and Wake Analysis * Rotor in Vertical Flight : Blade Element Theory * Rotor Mechanisms for Forward Flight * Rotor Aerodynamics in Forward Flight * Aerodyanamic Design * Performance * Trim, Stability, and Control * Index | |||||||
| AIAA | H | ISBN-10: 1563475103 ISBN-13: 9781563475108 | PGS: 156 | List: 68.95 YOUR PRICE: 68.95 | |||
| Computational Aerodynamics and Fluid Dynamics | |||||||
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| This textbook is written for senior undergraduate and graduate students as well as engineers who will develop or use code in the simulation of fluid flows or other physical phenomena. The objective of the book is to give the reader the basis for understan, Introduction.- Basics of the Finite-Difference Method.- Application to the Integration of Ordinary Differential Equations.- Partial Differential Equations.- Integration of a Linear Hyperbolic Equation.- Integration of a Linear Parabolic Equation.- Integra | |||||||
| SPRINGER VERLAG | H | ISBN-10: 3540434948 ISBN-13: 9783540434948 | PGS: N/A | List: 84.95 YOUR PRICE: 80.70 | |||
| EARLY DEELOPMENT OF MODERN AERODYNAMICS | |||||||
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| Contents: Introduction * A Survey of the Basic Principles of Modern Aerodynamics * From Antiquity to the Age of Newton * From Newton to the Emergence of the Field Theory of Fluid Flow * The Era of the Whirling Arm and the Invention of the Aeroplane * Nineteenth Century Developments in the Understanding of Fluid Flow * Practical DEvelopments in Aeronautics * Frederick William Lanchester * Lift Forces in Flowing Fluids* On the Motion of fluids with Very Little Friction * On Annexed Vortices * Boundary Layers in Fluids with Small Friction * On a Two Dimensional Flow Related to the Fundamentals of the Problems of Flight * On the Pressure Exerted by a Plane-Parallel Flow on Obstructing Bodies ( Aeroplane theory) * On the Contours of the Aerofoils of Hang Gliders* Subsequent Developments * Bibliography | |||||||
| AIAA | H | ISBN-10: 1563475162 ISBN-13: 9781563475160 | PGS: 230 | List: 94.95 YOUR PRICE: 90.20 | |||
| Experiments in Aerodynamics | |||||||
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| Langley first published Experiments in Aerodynamics in 1891. This facsimile edition is based on the second edition published in 1902 as part of the Smithsonian Contributions to Knowledge volumes. It reports on Langleyís early experiments in what he provisionally called aerodromics. From the Introductory: I have now been engaged since the beginning of the year 1887 in experiments on an extended scale for determining the possibility of, and the conditions for, transporting in the air a body whose specific gravity is greater than that of the air, and I desire to repeat my conviction that the obstacles in its way are not such as have been thought; that they lie more in such apparently secondary difficulties as though of guiding the body so that it may move in the direction desired, and ascend or descend with safety, than in what may appear to be the primary difficulties due to the nature of the air itself, and that in my opinion the evidence for this is now sufficiently complete to engage the serious attention of engineers to the practical solution of these secondary difficulties, and to the development of an art of mechanical flight which will bring with it a change in many of the conditions of individual and national existence whose importance can hardly be estimated. AIAA is pleased to bring this important book back into print." | |||||||
| AIAA | ISBN-10: 1563477882 ISBN-13: 9781563477881 | PGS: 140 | List: 29.95 YOUR PRICE: 28.45 | ||||
| FIXED AND FLAPPING WING AERODYNAMICS FOR MICRO AIR VEHICLE APPLICATIONS | |||||||
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| Contents: Preface: An Overview of Micro Air Vehicle Aerodynamics * Fixed Wings Aerodynamics * Higher-Order Boundary Layer Formulation and Application to Low Renolds Number Flows* Analysis and Design of Airfoils for Use at Ultra-Low Reynolds Numbers * Adaptive, Unstructured Meshes for Solving the Navier-Stokes Equations for Low-chord Reynolds Number Flows * Wind Tunnel Tests of Wings and Rings at Low Reynolds Numbers. Effects of Acoustic Disturbances on Low Re Aerofoil Flows * Aerodynamic Characteristics of Low Aspect Ratio Wings at Low Reynolds Numbers. Systematic Airfoil Design Studies at Low Reynolds Numbers * Numerical Optimization and Wind Tunnel Testing of Low Reynolds Number Airfoils. Unsteady Stalling Characteristics of Thin airfoils at Low Reynolds Number. Flapping and Rotary Wing Aerodynamics. Thrust and Drag in Flying Birds: Applications to Bird Like Micro Air Vehicles. Lift and Drag Characteristics of Rotary and Flapping Wings * A Rational Engineering Analysis of the Efficiency of flapping Flight * Leading-Edge Vortices of Flapping and Rotary Wings at Lower Reynolds Number * On the Flowfield and Forces Generated by a Flapping Rectangular Wing at Low Reynolds Number * Experimental and Computational Investigation of Flapping-Wing Propulsion for Micro-Air Vehicles. Aerodynamic Characteristics of Wings at Low Reynolds Number* A Non-Linear Model for the Study of Flapping Wing Flight * Euler Solutions for a Finite-Span Flapping Wing . From Soaring and Flapping Bird Flight to Innovative Wing and Propeller Contructions * passive Aeroelastic Tailoring for Optimal Flapping Wings * Shape Memory Alloy Acuators as Locomotor Muscles * Micro Air Vehicle Applications. MesoScale Flight and Miniature Rotorcraft Development * Development of the Black Widow Micro Air Vehicles * Computation of Aerodynamics Characteristics of a Micro Air Vehicle * Optic flow Sensors for MAV Navigation | |||||||
| AIAA | H | ISBN-10: 1563475170 ISBN-13: 9781563475177 | PGS: 605 | List: 100.95 YOUR PRICE: 100.95 | |||
| Flight Theory and Aerodynamics: A Practical Guide for Operational Safety, 2nd Edition | |||||||
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| Atmosphere and Airspeed Measurement. Airfoils and Aerodynamic Forces. Lift. Drag. Jet Aircraft Basic Performance. Jet Aircraft Applied Performance. Propeller Aircraft -- Basic Performance. Propeller Aircraft -- Applied Performance. Helicopter Flight Theory. Slow-Speed Flight. Takeoff Performance. Landing Performance. Maneuvering Performance. Longitudinal Stability and Control. Directional and Lateral Stability and Control. High-Speed Flight. Answers to Problems. References. Index. | |||||||
| Wiley-Interscience | H | ISBN-10: 0471370061 ISBN-13: 9780471370062 | PGS: N/A | List: 130.00 YOUR PRICE: 123.50 | |||
| FLIGHT VEHICLE PERFORMANCE AND AERODYNAMIC CONTROL | |||||||
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| Contents: Basic Nomenclature; Atmosphere; Characteristics of Power Plants; Flight Vehicle Lift-Drag Characteristics; Equations of Motion; Determination of Aerodynamic Characteristics; Flight Vehicle Performance; Aerodynamic Control Forces & Static Stability; Flight Vehicle Aerodynamic Control. CD-ROM INCLUDED. | |||||||
| AIAA | H | ISBN-10: 1563474638 ISBN-13: 9781563474637 | PGS: 350 | List: 127.95 YOUR PRICE: 121.55 | |||
| Foundations of Aerodynamics: Bases of Aerodynamic Design, 5th Edition | |||||||
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| The Fluid Medium. Kinematics of a Flow Field. Dynamics of Flow Fields. Irrotational Incompressible Flow About Two-Dimensional Bodies. Aerodynamic Characteristics of Airfoils. The Finite Wing. Introduction to Compressible Fluids. Energy Relations. Some Applications of One-Dimensional Compressible Flow. Waves. Linearized Compressible Flow. Airfoils in Compressible Flows. Wings and Wing-Body Combinations in Compressible Flow. The Dynamics of Viscous Fluids. Incompressible Laminar Flow in Tubes and Boundary Layers. Laminar Boundary Layers in Compressible Flow. Flow Instabilities and Transition from Laminar to Turbulent Flow. Turbulent Flows. Airfoil Design, Multiple Surfaces, Vortex Lift, Secondary Flows, Viscous Effects. Appendices. Tables. Oblique Shock Chart. References. Index. | |||||||
| Wiley | H | ISBN-10: 0471129194 ISBN-13: 9780471129196 | PGS: N/A | List: 161.95 YOUR PRICE: 153.85 | |||
| Fundamentals of Aerodynamics, 5th Ed. | |||||||
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| McGraw-Hill Science/Engineering/Math | H | ISBN-10: 0073398101 ISBN-13: 9780073398105 | PGS: N/A | List: 195.31 YOUR PRICE: 185.54 | |||
| Illustrated Guide to Aerodynamics, 2nd Ed. | |||||||
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| McGraw-Hill Professional | S | ISBN-10: 0830639012 ISBN-13: 9780830639014 | PGS: 337 | List: 39.95 YOUR PRICE: 37.95 | |||
| INTAKE AERODYNAMICS, SECOND EDITION | |||||||
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| Intake Aerodynamics, Second Edition presents new computational advancements and discoveries in intake aerodynamics. This important test considers the problem of airflow, both internal and external to air intake, as applied to civil and military aircraft. It covers the aerodynamics of subsonic and supersonic intakes in real flows, maintaining a progression through the transonic range. Also considered is the joint perspective of the airframe designer and the propulsion specialist in practical cases. Readers will gain insight into the fluid mechanics behind the deceleration of air from free stream to engine velocity, and an understanding of air compression and external drag in extensively revised chapters reflecting progress in the field. More than 300 drawings and diagrams help to illustrate the points defined througout the book | |||||||
| AIAA | H | ISBN-10: 1563473615 ISBN-13: 9781563473616 | PGS: 402 | List: 90.95 YOUR PRICE: 86.40 | |||
| Introduction to Aeronautics and AeroDynamic 3.0 Set | |||||||
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| This set contains Introduction to Aeronautics, Second Edition and AeroDYNAMIC 3.0 DVD. | |||||||
| AIAA | ISBN-10: 1563476924 ISBN-13: 9781563476921 | PGS: 0 | List: 109.95 YOUR PRICE: 104.45 | ||||
| INTRODUCTORY AERODYNAMICS AND HYDRODYNAMICS OF WINGS AND BODIES: Software-Based Approach | |||||||
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| Contents: Atmosphere & the Ocean; Elementary Flow Functions; Airfoils & the Joukowski Transform; Drag, Viscosity, & the Boundary Layer; Direct Computation of Airfoil Characteristics; Wing; Characteristics of Bodies at Small Angles of Attack; Characteristics of Wing Wakes; Computational Fluid Dynamics. SOFTWARE INCLUDED. | |||||||
| AIAA | H | ISBN-10: 1563472422 ISBN-13: 9781563472428 | PGS: 241 | List: 90.95 YOUR PRICE: 86.40 | |||
| Low-Speed Aerodynamics | |||||||
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| 1. Introduction and background; 2. Fundamentals of inviscid, incompressible flow; 3. General solution of the incompressible, potential flow equations; 4. Small disturbance flow over three-dimensional wings: formulation of the problem; 5. Small disturbance flow over two-dimensional airfoils; 6. Exact solutions with complex variables; 7. Perturbation methods; 8. Three-dimensional small disturbance solutions; 9. Numerical (panel) methods; 10. Singularity elements and influence coefficients; 11. Two-dimensional numerical solutions; 12. Three-dimensional numerical solutions; 13. Unsteady aerodynamics; 14. The laminar boundary layer; 15. Enhancement of the potential flow model; Appendices. | |||||||
| CAMBRIDGE UNIVERSITY PRESS | ISBN-10: 0521665523 ISBN-13: 9780521665520 | PGS: N/A | List: 70.00 YOUR PRICE: 70.00 | ||||
| MISSILE AERODYNAMICS | |||||||
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| The similarities between the airplane and the missile extend beyond their flying capabilities, and at higher operational speeds, rhe configuration distinctions become even less apparent. missile Aerodynamics, a classic now available from AIAA and Nielsen Engineering and Research, Inc. combines the best of missile and airplane aerodynamics, drawing extensively from numerous technical papers to present a rational and unified account of the principles behind missile projection. Evaluate the missile versus tha airplane ina multitude of areas, from longitudinal acceleration, wing loading, roll and dynamic stability guidance and navigation, and more. J.N. Nielsen covers every aspect of missile aerodynamics, from the classification of missiles and basic formulas to innovative aerodynamics controls. in one reliable reference, readers will find hu dreds of schematics, equations, and tables with practical applications in missile design and engineering. originally published by Neilsen Engineering and Research, inc. | |||||||
| AIAA | H | ISBN-10: 0962062901 ISBN-13: 9780962062902 | PGS: 450 | List: 84.95 YOUR PRICE: 80.70 | |||
| PRACTICAL INTAKE AERODYNAMIC DESIGN | |||||||
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| This book provides the distilled experience of authors who have been closely involved in design of air intakes for both airframe and engine manufacturers. Much valuable data from systematic experimental measurements on intakes for missiles, combat and V/ SOL aircraft from research sources in the United Kingdom, the United Stats, France & GErmany are included, together with the latest development in computational fluid dynamics aplied to air intakes. | |||||||
| AIAA | H | ISBN-10: 1563470640 ISBN-13: 9781563470646 | PGS: 448 | List: 84.95 YOUR PRICE: 80.70 | |||
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Your search found 33 books Now viewing Books 1 - 25 In stock items ship IMMEDIATELY. Other titles usually ship within 2-3 days. |
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