Aerodynamics For Engineers. 3rd Edition - Couverture souple

Bertin, John-J; Smith, Michael-L

Couverture souple

ISBN 10 : 013761487X ISBN 13 : 9780137614875

Editeur : Prentice Hall, 1997

Synopsis

This comprehensive guide to aerodynamics focuses on practical problems and discusses the fundamental principles and techniques used to solve these problems. It presents a background discussion of each topic followed by a presentation of the theory, and then derives fundamental equations, applies them to simple computational techniques, and compares them to experimental data.* NEW - Places more emphasis on design applications of phenomena/equations. * NEW - Relocates CFD-specific coverage to the beginning of the text (Ch. 3). * NEW - Adds/expands/revises discussions on: * Derivation of the drag polar (Ch. 5). * Sample problems on the calculation of wing geometry parameters for a delta wing and for the Space Shuttle Orbiter (Ch. 5). * Parasite drag (Ch. 5). * Included drag (Ch. 5). * L/D ration (Ch. 5). * The stall velocity for the F-16 (Ch. 5). * High lift military airfoils, including Flow field phenomena and data from recent AIAA papers. (Ch. 6). * Factors affecting drag due to lift at subsonic speeds (Ch. 7). * High angle of attack aerodynamics (Ch. 7). * The relation between the distribution of the cross-section area and the transonic drag rise, including an interesting case study for the transonic drag rise problems for the B-58, using flight data from NASA Langley, photographs, and quotes from Harry Hillaker (Ch. 9). * Numerical method for calculating the pressure distribution given the configuration (Ch. 11). * Numerical method for the determination of the camber Distribution (Ch. 11). * The design of the SST and of the HSCT (Ch. 11). * High L/P hypersonic configurations - waveriders (Ch. 12). * The evolution of the F-16 (Ch. 13). * Considerations for wing/canard, wing/tail, and tail-less configurations (Ch. 13). * Tables summarizing the main design features for a variety of operational requirements (Ch. 13). * Codes for aircraft design and calibration and validation of codes (Ch. 14). * NEW - Includes more sample problems and homework problems. * Makes use of spread-sheet software available as part of most office packages. * NEW - Cites recent references from the literature. * Presents a background discussion of each topic, followed by a presentation of the theory. * Carefully notes the assumptions (and, therefore, the restrictions) incorporated into the development of the theory. * Illustrates applications of theory with example problems. * Example problems are worked for relatively simple flow fields which can be adequately defined by a few control points and which can be worked using electronic calculators. * Solutions are obtained using numerical techniques in order to apply the theory for those flows where closed-form solutions are impractical or impossible. * Compares the theoretical solutions and/or the computed results with experimental data from the open literature to illustrate both the validity of the theoretical analysis and its limitations (or, equivalently, the range of conditions for which the theory is applicable). * Uses both SI units and English units throughout. * Includes conversion factors between SI units and English units.

A propos du livre

Quatrième de couverture

The fourth edition of Aerodynamics for Engineers has been written to reflect the rapid advances in software and in hardware that have resulted in the ever increasing use of Computational Fluid Dynamics (CFD) in the design of aerospace vehicles. The increased reliance on computational methods has led to two changes unique to the fourth edition.

1. Some very sophisticated numerical solutions for high-alpha flow fields (Chapter 7), transonic flows around an NACA airfoil (Chapter 9), and flow over the SR-71 at three high-speed Mach numbers (Chapter 11) appear for the first time in Aerodynamics for Engineers. Although these results have appeared in the open literature, the high-quality figures were provided by Cobalt Solutions, LLC, using the post-processing packages Fieldview and EnSight.
2. Chapter 14 has been completely rewritten to provide a discussion of the complementary use of experiment and of computation as tools for defining the aerodynamic environment. This was the greatest single change to the text. Chapter 14 was a major effort, intended to put in perspective the strengths and limitations of the various tools that were discussed individually throughout the text.

Présentation de l'éditeur

For junior/senior and graduate-level courses in Aerodynamics, Mechanical Engineering, and Aerospace Engineering.

Aerodynamics for Engineers merges fundamental fluid mechanics, experimental techniques, and computational fluid dynamics techniques to build a solid foundation for students in aerodynamic applications from low-speed flight through hypersonic flight. It presents a background discussion of each topic followed by a presentation of the theory, and then derives fundamental equations, applies them to simple computational techniques, and compares them to experimental data.

Détails de l'édition

• Éditeur: Prentice Hall
• Date d'édition: 1997
• Langue: anglais
• ISBN 10: 013761487X
• ISBN 13: 9780137614875
• Reliure: Broché
• Numéro d'édition: 3
• Nombre de pages: 688
• Coordonnées du fabricant: non disponible
• Personne responsable: non disponible