Natural Stability and the Parachute Principle in Aeroplanes
Author: W. LeMaitre
Publisher:
Published: 1911
Total Pages: 94
ISBN-13:
DOWNLOAD EBOOKRead and Download eBook Full
Author: W. LeMaitre
Publisher:
Published: 1911
Total Pages: 94
ISBN-13:
DOWNLOAD EBOOKAuthor: Robert C. Nelson
Publisher: WCB/McGraw-Hill
Published: 1998
Total Pages: 441
ISBN-13: 9780071158381
DOWNLOAD EBOOKThe second edition of Flight Stability and Automatic Control presents an organized introduction to the useful and relevant topics necessary for a flight stability and controls course. Not only is this text presented at the appropriate mathematical level, it also features standard terminology and nomenclature, along with expanded coverage of classical control theory, autopilot designs, and modern control theory. Through the use of extensive examples, problems, and historical notes, author Robert Nelson develops a concise and vital text for aircraft flight stability and control or flight dynamics courses.
Author: W. LeMaitre
Publisher:
Published: 1911
Total Pages: 72
ISBN-13:
DOWNLOAD EBOOKAuthor: Malcolm J. Abzug
Publisher: Cambridge University Press
Published: 2002-09-23
Total Pages: 417
ISBN-13: 1107320194
DOWNLOAD EBOOKFrom the early machines to today's sophisticated aircraft, stability and control have always been crucial considerations. In this second edition, Abzug and Larrabee again forge through the history of aviation technologies to present an informal history of the personalities and the events, the art and the science of airplane stability and control. The book includes never-before-available impressions of those active in the field, from pre-Wright brothers airplane and glider builders through to contemporary aircraft designers. Arranged thematically, the book deals with early developments, research centers, the effects of power on stability and control, the discovery of inertial coupling, the challenge of stealth aerodynamics, a look toward the future, and much more. It is profusely illustrated with photographs and figures, and includes brief biographies of noted stability and control figures along with a core bibliography. Professionals, students, and aviation enthusiasts alike will appreciate this readable history of airplane stability and control.
Author: W. LeMaitre
Publisher:
Published: 1911
Total Pages: 86
ISBN-13:
DOWNLOAD EBOOKAuthor: 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.
Author: Robert C. Nelson
Publisher: McGraw-Hill Companies
Published: 1989
Total Pages: 304
ISBN-13:
DOWNLOAD EBOOKAuthor: W. J. Duncan
Publisher: Cambridge University Press
Published: 2016-02-04
Total Pages: 409
ISBN-13: 1316509745
DOWNLOAD EBOOKFirst published in 1959, this book provides a detailed discussion regarding control and stability in aircraft, encompassing the broader subject of aircraft dynamics. Information on newer discoveries related to the effects of compressibility of air and the deformation of aircraft structures is included.
Author: George Hartley Bryan
Publisher:
Published: 1911
Total Pages: 216
ISBN-13:
DOWNLOAD EBOOKAuthor: Edward Seckel
Publisher: Academic Press
Published: 2014-05-10
Total Pages: 523
ISBN-13: 148322015X
DOWNLOAD EBOOKStability and Control of Airplanes and Helicopters deals with aircraft flying qualities that determine the stability and control of airplanes and helicopters. It includes problems based on real aircraft, selected to represent the gamut from simple to complicated, and from conventional utility designs to futuristic research types. Many of these problems involve comparison of theory and experiment to demonstrate their mutual relationship. Comprised of 25 chapters, this book begins with a discussion on the aerodynamics of the component parts related to the lift and moment characteristics of an airplane, including wings and associated accessories; bodies such as fuselages, nacelles, and tip tanks; and control surfaces. The reader is then introduced to some mathematical techniques for linear differential equations; steady flight at different speeds; and stick force and control-free stability. Subsequent chapters focus on flaps and high-lift devices; power and compressibility effects; and the manner in which the aircraft responds to the application of control. Aeroelasticity and longitudinal equations of motion are also examined. This monograph is intended for undergraduate and graduate students taking modern engineering courses.