Notes on the Static Longitudinal Stability and Control of Aircraft

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Publisher :
ISBN 13 :
Total Pages : 78 pages
Book Rating : 4.X/5 ( download)

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Book Synopsis Notes on the Static Longitudinal Stability and Control of Aircraft by : Waldemar Otto Brehaus

Download or read book Notes on the Static Longitudinal Stability and Control of Aircraft written by Waldemar Otto Brehaus and published by . This book was released on 1953 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Introduction to Aircraft Flight Mechanics

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Publisher : AIAA
ISBN 13 : 9781600860782
Total Pages : 666 pages
Book Rating : 4.8/5 (67 download)

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Book Synopsis Introduction to Aircraft Flight Mechanics by : Thomas R. Yechout

Download or read book Introduction to Aircraft Flight Mechanics written by Thomas R. Yechout and published by AIAA. This book was released on 2003 with total page 666 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.

Flight Stability and Automatic Control

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Publisher : WCB/McGraw-Hill
ISBN 13 : 9780071158381
Total Pages : 441 pages
Book Rating : 4.1/5 (583 download)

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Book Synopsis Flight Stability and Automatic Control by : Robert C. Nelson

Download or read book Flight Stability and Automatic Control written by Robert C. Nelson and published by WCB/McGraw-Hill. This book was released on 1998 with total page 441 pages. Available in PDF, EPUB and Kindle. Book excerpt: The 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.

DYNAMICS OF FLIGHT

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Publisher :
ISBN 13 : 9788126528912
Total Pages : pages
Book Rating : 4.5/5 (289 download)

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Book Synopsis DYNAMICS OF FLIGHT by : BERNARD. ETKIN

Download or read book DYNAMICS OF FLIGHT written by BERNARD. ETKIN and published by . This book was released on 1995 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Performance and Stability of Aircraft

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Publisher : Butterworth-Heinemann
ISBN 13 : 0080538649
Total Pages : 317 pages
Book Rating : 4.0/5 (85 download)

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Book Synopsis Performance and Stability of Aircraft by : J. Russell

Download or read book Performance and Stability of Aircraft written by J. Russell and published by Butterworth-Heinemann. This book was released on 1996-08-02 with total page 317 pages. Available in PDF, EPUB and Kindle. Book excerpt: The performance, stability, control and response of aircraft are key areas of aeronautical engineering. This book provides a comprehensive overview to the underlying theory and application of what are often perceived to be difficult topics. Initially it introduces the reader to the fundamental concepts underlying performance and stability, including lift characteristics and estimation of drag, before moving on to a more detailed analysis of performance in both level and climbing flight. Pitching motion is then described followed by a detailed discussion of all aspects of both lateral and longitudinal stability and response. It finishes with an examination of inertial cross-coupling and automatic control and stabilization. The student is helped to think in three dimensions throughout the book by the use of illustrative examples. The progression from one degree of freedom to six degrees of freedom is gradually introduced. The result is an approach dealing specifically with all aspects of performance, stability and control that fills a gap in the current literature. It will be essential reading for all those embarking on degree level courses in aeronautical engineering and will be of interest to all with an interest in stability and dynamics, including those in commercial flying schools who require an insight into the performance of their aircraft. Ideal for undergraduate aeronautical engineers Three-dimensional thinking introduced through worked examples and simple situations

Definition and Application of Longitudinal Stability Derivatives for Elastic Airplanes

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Publisher :
ISBN 13 :
Total Pages : 132 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Definition and Application of Longitudinal Stability Derivatives for Elastic Airplanes by : William B. Kemp

Download or read book Definition and Application of Longitudinal Stability Derivatives for Elastic Airplanes written by William B. Kemp and published by . This book was released on 1972 with total page 132 pages. Available in PDF, EPUB and Kindle. Book excerpt: A set of longitudinal stability derivatives for elastic airplanes is defined from fundamental principles allowing perturbations in forward speed. Application of these derivatives to longitudinal stability analysis by use of approximate expressions for static stability and control parameters as well as the dynamic equations of motion is illustrated. One commonly used alternative formulation for elastic airplanes is shown to yield significant inaccuracies because of inappropriate interpretation of inertial effects.

Some Data on the Static Longitudinal Stability and Control of Airplanes

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Publisher :
ISBN 13 :
Total Pages : 672 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Some Data on the Static Longitudinal Stability and Control of Airplanes by : A. Martinov

Download or read book Some Data on the Static Longitudinal Stability and Control of Airplanes written by A. Martinov and published by . This book was released on 1940 with total page 672 pages. Available in PDF, EPUB and Kindle. Book excerpt: In the solution of a number of problems on the stability and controllability of airplanes, there arises the necessity for knowing the characteristics of the tail surfaces of the types in common use today. Of those characteristics, the most important are the effectiveness and hinge moments of the tail surfaces. As has been shown in the present paper, there exists the possibility of determining these characteristics by the formulas obtained with a degree of accuracy sufficient for the purposes of preliminary computation. These formulas take into account a number of fundamental tail characteristics such as tail cut-outs on the control surface and the form of the control surface leading edge.

Flight Investigations of Automatic Stabilization of an Airplane Having Static Longitudinal Instability

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Publisher :
ISBN 13 :
Total Pages : 42 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Flight Investigations of Automatic Stabilization of an Airplane Having Static Longitudinal Instability by : Walter R. Russell

Download or read book Flight Investigations of Automatic Stabilization of an Airplane Having Static Longitudinal Instability written by Walter R. Russell and published by . This book was released on 1959 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Effect of Various External Stores on the Static Longitudinal Stability, Longitudinal Control, and Drag Characteristics of the Model F-4C Airplane

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Publisher :
ISBN 13 :
Total Pages : 143 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Effect of Various External Stores on the Static Longitudinal Stability, Longitudinal Control, and Drag Characteristics of the Model F-4C Airplane by : J. M. Whoric

Download or read book Effect of Various External Stores on the Static Longitudinal Stability, Longitudinal Control, and Drag Characteristics of the Model F-4C Airplane written by J. M. Whoric and published by . This book was released on 1973 with total page 143 pages. Available in PDF, EPUB and Kindle. Book excerpt: The results from analysis of data obtained from wind tunnel tests, which were conducted to determine the effect of various external stores on the aerodynamic characteristics of the model F-4C airplane, are presented and discussed. The analysis includes evaluation of the static longitudinal stability, drag, and longitudinal control characteristics of the F-4C when loaded with the Pavestorm missile series, Modular Weapons series, Mark 84 EOGB, M-118 LGB, SUU-51B/B, SUU-30H/B, and Rockeye stores. Moreover, analysis of the probable cause as well as the wind tunnel verification of a pilot-reported 'tuck-under' problem with the F-4C when carrying the Pavestorm series of stores is presented and discussed. Incremental drag rise and neutral point shift associated with store loading are compared with results obtained from existing prediction methods and techniques. Data are presented for aircraft weights representative of each store loading at altitudes of sea level, 10-, 20-, and 30-thousand feet for aircraft center-of-gravity locations of 25, 33, and 36 percent of the mean aerodynamic chord over the Mach number range from 0.4 to 1.3. (Author).

A Wind-tunnel Evaluation of Analytical Techniques for Predicting Static Stability and Control Characteristics of Flexible Aircraft

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Publisher :
ISBN 13 :
Total Pages : 76 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis A Wind-tunnel Evaluation of Analytical Techniques for Predicting Static Stability and Control Characteristics of Flexible Aircraft by : Irving Abel

Download or read book A Wind-tunnel Evaluation of Analytical Techniques for Predicting Static Stability and Control Characteristics of Flexible Aircraft written by Irving Abel and published by . This book was released on 1972 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental evaluation of analytical techniques for predicting certain stability and control characteristics of a large flexible aircraft is presented. Analytical methods based on both the model approach and flexibility influence coefficients are developed to predict the aerodynamic characteristics of a flexible airplane. These methods are then applied to a flexibly scaled model of a supersonic transport configuration. Comparisons of wind-tunnel data, calculations based on the model approach, and flexibility influence coefficients are presented over the Mach number range from 0.6 to 2.7. An examination of the results obtained from this study indicates that both analytical techniques predict reasonably well the effect of flexibility on the basic longitudinal characteristics and that both techniques give generally comparable results.

Flight Dynamics Principles

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Publisher : Butterworth-Heinemann
ISBN 13 : 008098276X
Total Pages : 608 pages
Book Rating : 4.0/5 (89 download)

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Book Synopsis Flight Dynamics Principles by : Michael V. Cook

Download or read book Flight Dynamics Principles written by Michael V. Cook and published by Butterworth-Heinemann. This book was released on 2012-10-03 with total page 608 pages. Available in PDF, EPUB and Kindle. Book excerpt: The 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)

An Introduction to the Longitudinal Static Stability of Low-Speed Aircraft

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Publisher : Elsevier
ISBN 13 : 1483225224
Total Pages : 160 pages
Book Rating : 4.4/5 (832 download)

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Book Synopsis An Introduction to the Longitudinal Static Stability of Low-Speed Aircraft by : F. G. Irving

Download or read book An Introduction to the Longitudinal Static Stability of Low-Speed Aircraft written by F. G. Irving and published by Elsevier. This book was released on 2014-07-10 with total page 160 pages. Available in PDF, EPUB and Kindle. Book excerpt: International Series of Monographs in Aeronautics and Astronautics, Volume 5: An Introduction to the Longitudinal Static Stability of Low-Speed Aircraft covers the concepts and practical applications of longitudinal static stability and control to the design and flight testing of low-speed aircraft. This book is composed of 11 chapters, and begins with a brief overview of the concepts of static stability. The next chapters deal with the forces and moments acting on an aeroplane, particularly on the wings and tail, as well as their properties, which are expressed in mathematical terms. These topics are followed by discussions on conditions of static stability; general stability considerations; the influence of static stability on the pilot's action, and measure of static stability for flight tests. The final chapters review the maneuverability in pitch and the motion of tailplanes. This book will prove useful to undergraduate aeronautics students.

Airplane Stability and Control

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Publisher : Cambridge University Press
ISBN 13 : 1107320194
Total Pages : 417 pages
Book Rating : 4.1/5 (73 download)

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Book Synopsis Airplane Stability and Control by : Malcolm J. Abzug

Download or read book Airplane Stability and Control written by Malcolm J. Abzug and published by Cambridge University Press. This book was released on 2002-09-23 with total page 417 pages. Available in PDF, EPUB and Kindle. Book excerpt: From 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.

Static Longitudinal Stability and Control Characteristics of a Typical High-Speed Aircraft Design at Supersonic Speeds

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Publisher :
ISBN 13 :
Total Pages : 39 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Static Longitudinal Stability and Control Characteristics of a Typical High-Speed Aircraft Design at Supersonic Speeds by : Edward Seckel

Download or read book Static Longitudinal Stability and Control Characteristics of a Typical High-Speed Aircraft Design at Supersonic Speeds written by Edward Seckel and published by . This book was released on 1948 with total page 39 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Compressibility Effects on the Longitudinal Stability and Control of a Pursuit-type Airplane as Measured in Flight

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Publisher :
ISBN 13 :
Total Pages : 72 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Compressibility Effects on the Longitudinal Stability and Control of a Pursuit-type Airplane as Measured in Flight by : William N. Turner

Download or read book Compressibility Effects on the Longitudinal Stability and Control of a Pursuit-type Airplane as Measured in Flight written by William N. Turner and published by . This book was released on 1945 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt: Measurements of the longitudinal stability and control of a pursuit-type airplane (the P-39N-1 airplane) were made in flight up to a Mach number of 0.78. The data are presented in the form of curves showing the variation, with center-of-gravity position, dynamic pressure, and Mach number, of the stick-fixed and stick-free stability, control, and balance of the airplane.

Simulator Study of Stall/post-stall Characteristics of a Fighter Airplane with Relaxed Longitudinal Static Stability

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Publisher :
ISBN 13 :
Total Pages : 236 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Simulator Study of Stall/post-stall Characteristics of a Fighter Airplane with Relaxed Longitudinal Static Stability by :

Download or read book Simulator Study of Stall/post-stall Characteristics of a Fighter Airplane with Relaxed Longitudinal Static Stability written by and published by . This book was released on 1979 with total page 236 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Fundamentals of Airplane Flight Mechanics

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Publisher : Springer Science & Business Media
ISBN 13 : 3540465731
Total Pages : 311 pages
Book Rating : 4.5/5 (44 download)

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Book Synopsis Fundamentals of Airplane Flight Mechanics by : David G. Hull

Download or read book Fundamentals of Airplane Flight Mechanics written by David G. Hull and published by Springer Science & Business Media. This book was released on 2007-01-20 with total page 311 pages. Available in PDF, EPUB and Kindle. Book excerpt: Flight 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.