Space Vehicle Design

Space Vehicle Design
Author: Michael Douglas Griffin
Publisher: AIAA
Total Pages: 700
Release: 2004
Genre: Space vehicles
ISBN: 9781600861123

Aircraft Engine Design

Aircraft Engine Design
Author: Jack D. Mattingly
Publisher: AIAA
Total Pages: 732
Release: 2002
Genre: Aircraft gas-turbines
ISBN: 9781600860164

Annotation A design textbook attempting to bridge the gap between traditional academic textbooks, which emphasize individual concepts and principles; and design handbooks, which provide collections of known solutions. The airbreathing gas turbine engine is the example used to teach principles and methods. The first edition appeared in 1987. The disk contains supplemental material. Annotation c. Book News, Inc., Portland, OR (booknews.com).

Aircraft and Rotorcraft System Identification

Aircraft and Rotorcraft System Identification
Author: Mark Brian Tischler
Publisher: AIAA Education
Total Pages: 0
Release: 2012
Genre: Technology & Engineering
ISBN: 9781600868207

Although many books have been written on the theory of system identification, few are available that provide a complete engineering treatment of system identification and how to successfully apply it to flight vehicles. This book presents proven methods, practical guidelines, and real-world flight-test results for a wide range of state-of-the-art flight vehicles, from small uncrewed aerial vehicles (UAVs) to large manned aircraft/rotorcraft.

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)
Total Pages: 156
Release: 2011
Genre: Science
ISBN: 9781600868276

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).

Elements of Spacecraft Design

Elements of Spacecraft Design
Author: Charles D. Brown
Publisher: AIAA
Total Pages: 632
Release: 2002
Genre: Space vehicles
ISBN: 9781600860515

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
Total Pages: 586
Release: 2000
Genre: Computers
ISBN: 9781563474569

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

Introduction to Aircraft Flight Mechanics

Introduction to Aircraft Flight Mechanics
Author: Thomas R. Yechout
Publisher: AIAA
Total Pages: 666
Release: 2003
Genre: Aerodynamics
ISBN: 9781600860782

Based on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.