Introductory Aerodynamics And Hydrodynamics Of Wings And Bodies

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Introductory Aerodynamics and Hydrodynamics of Wings and Bodies

Author : Frederick O. Smetana
Publisher : AIAA
Page : 270 pages
File Size : 40,9 Mb
Release : 1997
Category : Aerodynamics
ISBN : 1600860834

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Introductory Aerodynamics and Hydrodynamics of Wings and Bodies by Frederick O. Smetana Pdf

Annotation This textbook and its six supporting computer programs provide theoretical modeling of the aerodynamic characteristics of wings and bodies at low Mach numbers. The approach presented directly helps engineering students improve problem-solving skills by teaching them to discern the necessary steps associated with solving analytical problems. The book also presents a justification and rationale for validating end results that leave the student with an understanding of the answer. The text differs from others by providing interactive computer programs that allow the student to conduct trade studies. It provides case-specific software that permits the student to do considerably more characteristic analysis of user-selected wings and bodies than is possible with other introductory textbooks. In addition, the algorithms are capable of working problems at a level well beyond those typically solved by hand in other textbooks. This approach allows students to determine easily the effects of modifying parameters and geometry. Another benefit of using this textbook is the understanding students gain of the capabilities of large industrial codes.

Aerodynamics of Wings and Bodies

Author : Holt Ashley,Mårten Landahl,Marten T. Landahl
Publisher : Courier Corporation
Page : 306 pages
File Size : 47,6 Mb
Release : 1965-01-01
Category : Technology & Engineering
ISBN : 9780486648996

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Aerodynamics of Wings and Bodies by Holt Ashley,Mårten Landahl,Marten T. Landahl Pdf

This excellent, innovative reference offers a wealth of useful information and a solid background in the fundamentals of aerodynamics. Fluid mechanics, constant density inviscid flow, singular perturbation problems, viscosity, thin-wing and slender body theories, drag minimalization, and other essentials are addressed in a lively, literate manner and accompanied by diagrams.

Introduction to Theoretical Aerodynamics and Hydrodynamics

Author : William Rees Sears
Publisher : Amer Inst of Aeronautics &
Page : 203 pages
File Size : 46,9 Mb
Release : 2011
Category : Science
ISBN : 1600867731

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Introduction to Theoretical Aerodynamics and Hydrodynamics by William Rees Sears Pdf

Formally published for the first time, Professor William R. Sears classic work, "Introduction to Theoretical Aerodynamics and Hydrodynamics, "reflects many years of continual evolution as a course study guide at the Graduate School of Aeronautical Engineering at Cornell University, with updates prepared by his former students to enhance ease of use by todays students. Instructors will find this a superb textbook for a first course in ideal aerodynamics and/or hydrodynamics. Because Sears was a master of connecting mathematical concepts with physical fluid dynamic quantities, readers will find fundamental concepts directly connected to practical applications in the numerous step-by-step examples found throughout the book. SPECIAL FEATURES

EBOOK: Fluid Mechanics (SI units)

Author : White
Publisher : McGraw Hill
Page : 794 pages
File Size : 44,7 Mb
Release : 2016-02-01
Category : Technology & Engineering
ISBN : 9780077190354

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EBOOK: Fluid Mechanics (SI units) by White Pdf

Overview White's Fluid Mechanics offers students a clear and comprehensive presentation of the material that demonstrates the progression from physical concepts to engineering applications and helps students quickly see the practical importance of fluid mechanics fundamentals. The wide variety of topics gives instructors many options for their course and is a useful resource to students long after graduation. The book’s unique problem-solving approach is presented at the start of the book and carefully integrated in all examples. Students can progress from general ones to those involving design, multiple steps and computer usage. McGraw-Hill Education's Connect, is also available as an optional, add on item. Connect is the only integrated learning system that empowers students by continuously adapting to deliver precisely what they need, when they need it, how they need it, so that class time is more effective. Connect allows the professor to assign homework, quizzes, and tests easily and automatically grades and records the scores of the student's work. Problems are randomized to prevent sharing of answers an may also have a "multi-step solution" which helps move the students' learning along if they experience difficulty. The eighth edition of Fluid Mechanics offers students a clear and comprehensive presentation of the material that demonstrates the progression from physical concepts to engineering applications. The book helps students to see the practical importance of fluid mechanics fundamentals. The wide variety of topics gives instructors many options for their course and is a useful resource to students long after graduation. The problem-solving approach is presented at the start of the book and carefully integrated in all examples. Students can progress from general examples to those involving design, multiple steps, and computer usage.

Theoretical and Applied Aerodynamics

Author : J. J. Chattot,M. M. Hafez
Publisher : Springer
Page : 620 pages
File Size : 51,5 Mb
Release : 2015-03-31
Category : Science
ISBN : 9789401798259

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Theoretical and Applied Aerodynamics by J. J. Chattot,M. M. Hafez Pdf

This book covers classical and modern aerodynamics, theories and related numerical methods, for senior and first-year graduate engineering students, including: -The classical potential (incompressible) flow theories for low speed aerodynamics of thin airfoils and high and low aspect ratio wings. - The linearized theories for compressible subsonic and supersonic aerodynamics. - The nonlinear transonic small disturbance potential flow theory, including supercritical wing sections, the extended transonic area rule with lift effect, transonic lifting line and swept or oblique wings to minimize wave drag. Unsteady flow is also briefly discussed. Numerical simulations based on relaxation mixed-finite difference methods are presented and explained. - Boundary layer theory for all Mach number regimes and viscous/inviscid interaction procedures used in practical aerodynamics calculations. There are also four chapters covering special topics, including wind turbines and propellers, airplane design, flow analogies and hypersonic (rotational) flows. A unique feature of the book is its ten self-tests and their solutions as well as an appendix on special techniques of functions of complex variables, method of characteristics and conservation laws and shock waves. The book is the culmination of two courses taught every year by the two authors for the last two decades to seniors and first-year graduate students of aerospace engineering at UC Davis.

Fixed and Flapping Wing Aerodynamics for Micro Air Vehicle Applications

Author : Thomas J. Mueller
Publisher : AIAA
Page : 614 pages
File Size : 50,5 Mb
Release : 2001
Category : Aerodynamics
ISBN : 1600864465

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Fixed and Flapping Wing Aerodynamics for Micro Air Vehicle Applications by Thomas J. Mueller Pdf

This title reports on the latest research in the area of aerodynamic efficency of various fixed-wing, flapping wing, and rotary wing concepts. It presents the progress made by over fifty active researchers in the field.

Flight Testing of Fixed Wing Aircraft

Author : Ralph D. Kimberlin
Publisher : AIAA
Page : 464 pages
File Size : 48,6 Mb
Release : 2003
Category : Airplanes
ISBN : 1600860567

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Flight Testing of Fixed Wing Aircraft by Ralph D. Kimberlin Pdf

Annotation The measurement of performance during an airplane's flight, testing is one of the more important tasks to be accomplished during its development as it impacts on both the airplane's safety and its marketability. This book discusses performance for both propeller-driven and jet aircraft.

Computational Flight Dynamics

Author : Malcolm J. Abzug
Publisher : AIAA
Page : 504 pages
File Size : 51,5 Mb
Release : 1998
Category : Aerodynamics
ISBN : 1600860419

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Computational Flight Dynamics by Malcolm J. Abzug Pdf

Flight Vehicle Performance and Aerodynamic Control

Author : Frederick O. Smetana
Publisher : AIAA
Page : 392 pages
File Size : 51,6 Mb
Release : 2001
Category : Aerodynamics
ISBN : 1600860575

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Flight Vehicle Performance and Aerodynamic Control by Frederick O. Smetana Pdf

Annotation "Flight Vehicle Performance and Aerodynamic Control is designed to serve as a text for either an 11-week or a 16-week course at the sophomore level. It explains typical methods used to estimate aircraft performance, the theoretical basis of these methods, and how various parameters derived from the aircraft geometry can be used to estimate the requirements of control surfaces and the aerodynamic forces required to actuate these surfaces. This book includes time-tested computer programs that perform the analyses in a manner that reduces student error and improves result accuracy. Because the source code is given, users with a FORTRAN compiler can modify the program to suit particular needs. The major advantage of the software is that more realistic problems may be treated and the effects of parametric programs are more accurate than calculators. The programs are available as executables for Windows machines as well as in ASCII source code versions that can be readily compiled and then executed on Unix, Linux, and Macintosh machines and on mainframes.

Advanced Dynamics

Author : Shuh-Jing Ying
Publisher : AIAA
Page : 398 pages
File Size : 45,5 Mb
Release : 1997
Category : Dynamics
ISBN : 1600860028

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Advanced Dynamics by Shuh-Jing Ying Pdf

Finite Element Multidisciplinary Analysis

Author : Kajal K. Gupta
Publisher : AIAA
Page : 458 pages
File Size : 55,9 Mb
Release : 2003
Category : Finite element method
ISBN : 1600860532

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Finite Element Multidisciplinary Analysis by Kajal K. Gupta Pdf

Annotation This book fills a gap within the finite element literature by addressing the challenges and developments in multidiscipli-nary analysis. Current developments include disciplines of structural mechanics, heat transfer, fluid mechanics, controls engineering and propulsion technology, and their interaction as encountered in many practical problems in aeronautical, aerospace, and mechanical engineering, among others. These topics are reflected in the 15 chapter titles of the book. Numerical problems are provided to illustrate the applicability of the techniques. Exercises may be solved either manually or by using suitable computer software. A version of the multidisciplinary analysis program STARS is available from the author. As a textbook, the book is useful at the senior undergraduate or graduate level. The practicing engineer will find it invaluable for solving full-scale practical problems.

Design Methodologies for Space Transportation Systems

Author : Walter Edward Hammond
Publisher : AIAA
Page : 906 pages
File Size : 40,9 Mb
Release : 2001
Category : Astronautics
ISBN : 1600860451

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Design Methodologies for Space Transportation Systems by Walter Edward Hammond Pdf

Annotation "Design Methodologies for Space Transportation Systems is a sequel to the author's earlier text, "Space Transportation: A Systems Approach to Analysis and Design. Both texts represent the most comprehensive exposition of the existing knowledge and practice in the design and project management of space transportation systems, and they reflect a wealth of experience by the author with the design and management of space systems. The text discusses new conceptual changes in the design philosophy away from multistage expendable vehicles to winged, reusable launch vehicles and presents an overview of the systems engineering and vehicle design process as well as systems trades and analysis. Individual chapters are devoted to specific disciplines such as aerodynamics, aerothermal analysis, structures, materials, propulsion, flight mechanics and trajectories, avionics and computers, and control systems. The final chapters deal with human factors, payload, launch and mission operations, safety, and mission assurance. The two texts by the author provide a valuable source of information for the space transportation community of designers, operators, and managers. A companion CD-ROM succinctly packages some oversized figures and tables, resources for systems engineering and launch ranges, and a compendium of software programs. The computer programs include the USAF AIRPLANE AND MISSILE DATCOM CODES (with extensive documentation); COSTMODL for software costing; OPGUID launch vehicle trajectory generator; SUPERFLO-a series of 11 programs intended for solving compressible flow problems in ducts and pipes found in industrial facilities; and a wealth of Microsoft Excel spreadsheet programs covering thedisciplines of statistics, vehicle trajectories, propulsion performance, math utilities,

Spacecraft Mission Design

Author : Charles D. Brown
Publisher : AIAA
Page : 204 pages
File Size : 46,7 Mb
Release : 1998
Category : Astrodynamics
ISBN : 1600861156

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Spacecraft Mission Design by Charles D. Brown Pdf

Analytical Mechanics of Space Systems

Author : Hanspeter Schaub,John L. Junkins
Publisher : AIAA
Page : 744 pages
File Size : 55,5 Mb
Release : 2003
Category : Celestial mechanics
ISBN : 1600860273

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Analytical Mechanics of Space Systems by Hanspeter Schaub,John L. Junkins Pdf

Modeling and Simulation of Aerospace Vehicle Dynamics

Author : Peter H. Zipfel
Publisher : AIAA
Page : 586 pages
File Size : 49,6 Mb
Release : 2000
Category : Computers
ISBN : 1563474565

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Modeling and Simulation of Aerospace Vehicle Dynamics by Peter H. Zipfel Pdf

A textbook for an advanced undergraduate course in which Zipfel (aerospace engineering, U. of Florida) introduces the fundamentals of an approach to, or step in, design that has become a field in and of itself. The first part assumes an introductory course in dynamics, and the second some specialized knowledge in subsystem technologies. Practicing engineers in the aerospace industry, he suggests, should be able to cover the material without a tutor. Rather than include a disk, he has made supplementary material available on the Internet. Annotation copyrighted by Book News, Inc., Portland, OR