Longitudinal and Lateral Aerodynamic Characteristics at Mach Numbers from 0.60 to 2.20 of a Variable Sweep Fighter Model with Wing Sweep Angles from 25 Deg to 75 Deg
Author:
Publisher:
Published: 1962
Total Pages: 28
ISBN-13:
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Introduction to Aircraft Flight Mechanics
Author: Thomas R. Yechout
Publisher: AIAA
Published: 2003
Total Pages: 666
ISBN-13: 9781600860782
DOWNLOAD EBOOKBased 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.
Simulator Study of Stall/post-stall Characteristics of a Fighter Airplane with Relaxed Longitudinal Static Stability
Author:
Publisher:
Published: 1979
Total Pages: 236
ISBN-13:
DOWNLOAD EBOOKFlight Stability and Automatic Control
Author: Robert C. Nelson
Publisher:
Published: 1998
Total Pages: 464
ISBN-13:
DOWNLOAD EBOOKThis edition of this this flight stability and controls guide features an unintimidating math level, full coverage of terminology, and expanded discussions of classical to modern control theory and autopilot designs. Extensive examples, problems, and historical notes, make this concise book a vital addition to the engineer's library.
Aircraft Design
Author: Daniel P. Raymer
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
Published: 2006
Total Pages: 0
ISBN-13: 9781563478291
DOWNLOAD EBOOKWinner of the Summerfield Book Award Winner of the Aviation-Space Writers Association Award of Excellence. --Over 30,000 copies sold, consistently the top-selling AIAA textbook title This highly regarded textbook presents the entire process of aircraft conceptual designfrom requirements definition to initial sizing, configuration layout, analysis, sizing, and trade studiesin the same manner seen in industry aircraft design groups. Interesting and easy to read, the book has more than 800 pages of design methods, illustrations, tips, explanations, and equations, and extensive appendices with key data essential to design. It is the required design text at numerous universities around the world, and is a favorite of practicing design engineers.
Fundamentals of Airplane Flight Mechanics
Author: David G. Hull
Publisher: Springer Science & Business Media
Published: 2007-01-20
Total Pages: 311
ISBN-13: 3540465731
DOWNLOAD EBOOKFlight mechanics is the application of Newton's laws to the study of vehicle trajectories (performance), stability, and aerodynamic control. This volume details the derivation of analytical solutions of airplane flight mechanics problems associated with flight in a vertical plane. It covers trajectory analysis, stability, and control. In addition, the volume presents algorithms for calculating lift, drag, pitching moment, and stability derivatives. Throughout, a subsonic business jet is used as an example for the calculations presented in the book.
Flight Dynamics Principles
Author: Michael V. Cook
Publisher: Butterworth-Heinemann
Published: 2012-10-03
Total Pages: 608
ISBN-13: 008098276X
DOWNLOAD EBOOKThe study of flight dynamics requires a thorough understanding of the theory of the stability and control of aircraft, an appreciation of flight control systems and a grounding in the theory of automatic control. Flight Dynamics Principles is a student focused text and provides easy access to all three topics in an integrated modern systems context. Written for those coming to the subject for the first time, the book provides a secure foundation from which to move on to more advanced topics such as, non-linear flight dynamics, flight simulation, handling qualities and advanced flight control. - Additional examples to illustrate the application of computational procedures using tools such as MATLAB®, MathCad® and Program CC® - Improved compatibility with, and more expansive coverage of the North American notational style - Expanded coverage of lateral-directional static stability, manoeuvrability, command augmentation and flight in turbulence - An additional coursework study on flight control design for an unmanned air vehicle (UAV)
Investigation of Axisymmetric and Nonaxisymmetric Nozzles Installed on a 0.10 Scale F-18 Prototype Airplane Model
Author: Francis J. Capone
Publisher:
Published: 1980
Total Pages: 308
ISBN-13:
DOWNLOAD EBOOKAirfoil Design and Data
Author: Richard Eppler
Publisher: Springer Science & Business Media
Published: 2012-12-06
Total Pages: 569
ISBN-13: 3662026465
DOWNLOAD EBOOKThis detailed book describes a procedure for the design and analysis of subsonic airfoils. Contains 116 new airfoils for a wide range of Reynolds numbers and application requirements, including the input data for the computer code.
Theory of Wing Sections
Author: Ira H. Abbott
Publisher: Courier Corporation
Published: 2012-04-26
Total Pages: 708
ISBN-13: 0486134997
DOWNLOAD EBOOKConcise compilation of subsonic aerodynamic characteristics of NACA wing sections, plus description of theory. 350 pages of tables.
