AIAA Aerospace Design Engineers Guide
AIAA Aerospace Design Engineers Guide

Author: AIAA (American Institute of Aeronautics and Astronautics)

Publisher: John Wiley & Sons

Published: 2005-07-18

Total Pages: 456

ISBN-13: 9781860584244

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An indispensable reference for aerospace designers, analysts and students. This fifth revised and enlarged edition of this classic, indispensable, and practical guide provides a condensed collection of commonly used engineering reference data specifically related to aerospace design. New material on air breathing propulsion, systems engineering, and radar cross section has been added to reflect recent data in aircraft design. Features: New material on air breathing propulsion, systems engineering, and radar cross section Most commonly used formulas and data for aerospace design Convenient size and binding Large, easy-to-read tables, charts, and figures Handy reference for everyday use Developed by aerospace professionals AIAA Aerospace Design Engineers Guide is an essential tool for every design engineer and every aspiring aerospace engineering student.

Elements of Spacecraft Design
Elements of Spacecraft Design

Author: Charles D. Brown

Publisher: AIAA

Published: 2002

Total Pages: 632

ISBN-13: 9781600860515

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Annotation This text discusses the conceptual stages of mission design, systems engineering, and orbital mechanics, providing a basis for understanding the design process for different components and functions of a spacecraft. Coverage includes propulsion and power systems, structures, attitude control, thermal control, command and data systems, and telecommunications. Worked examples and exercises are included, in addition to appendices on acronyms and abbreviations and spacecraft design data. The book can be used for self-study or for a course in spacecraft design. Brown directed the team that produced the Magellan spacecraft, and has taught spacecraft design at the University of Colorado. Annotation c. Book News, Inc., Portland, OR (booknews.com).

Modeling and Simulation of Aerospace Vehicle Dynamics
Modeling and Simulation of Aerospace Vehicle Dynamics

Author: Peter H. Zipfel

Publisher: AIAA

Published: 2000

Total Pages: 586

ISBN-13: 9781563474569

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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

Aerospace Materials and Applications
Aerospace Materials and Applications

Author: Biliyar N. Bhat

Publisher:

Published: 2018

Total Pages: 0

ISBN-13: 9781624104886

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"The present volume is focused on documenting the novel processing, fabrication, characterization, and testing approaches that are unique to aerospace materials/structures/systems"--Preface.

Introduction to Flight Testing and Applied Aerodynamics
Introduction to Flight Testing and Applied Aerodynamics

Author: Barnes Warnock McCormick

Publisher: AIAA (American Institute of Aeronautics & Astronautics)

Published: 2011

Total Pages: 156

ISBN-13: 9781600868276

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An introduction into the art and science of measuring and predicting airplane performance, ""Introduction to Flight Testing and Applied Aerodynamics"" will benefit students, homebuilders, pilots, and engineers in learning how to collect and analyze data relevant to the takeoff, climb, cruise, handling qualities, descent, and landing of an aircraft. This textbook presents a basic and concise analysis of airplane performance, stability, and control. Basic algebra, trigonometry, and some calculus are used. Topics discussed include: Engine and propeller performance; Estimation of drag; Airplane dynamics; Wing spanwise lift distributions; Flight experimentation; Airspeed calibration; Takeoff performance; Climb performance; and, Dynamic and static stability. Special features: examples containing student-obtained data about specific airplanes and engines; simple experiments that determine an airplane's performance and handling qualities; and, end-of-chapter problems (with answers supplied in an appendix).

Introduction to Aircraft Aeroelasticity and Loads
Introduction to Aircraft Aeroelasticity and Loads

Author: Jan Robert Wright

Publisher: John Wiley & Sons

Published: 2008-02-28

Total Pages: 559

ISBN-13: 047085846X

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Aeroelastic phenomena arising from the interaction of aerodynamic, elastic and inertia forces, and the loads resulting from flight / ground manoeuvres and gust / turbulence encounters, have a significant influence upon aircraft design. The prediction of aircraft aeroelastic stability, response and loads requires application of a range of interrelated engineering disciplines. This new textbook introduces the foundations of aeroelasticity and loads for the flexible aircraft, providing an understanding of the main concepts involved and relating them to aircraft behaviour and industrial practice. This book includes the use of simplified mathematical models to demonstrate key aeroelastic and loads phenomena including flutter, divergence, control effectiveness and the response and loads resulting from flight / ground manoeuvres and gust / turbulence encounters. It provides an introduction to some up-to-date methodologies for aeroelastics and loads modelling. It lays emphasis on the strong link between aeroelasticity and loads. It also includes provision of MATLAB and SIMULINK programs for the simplified analyses. It offers an overview of typical industrial practice in meeting certification requirements.