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Some Data On The Static Longitudinal Stability And Control Of Airplanes
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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.
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.
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.
Book Synopsis An Analysis of the Effects of Aeroelasticity on Static Longitudinal Stability and Control of a Swept-back-wing Airplane by : Richard B. Skoog
Download or read book An Analysis of the Effects of Aeroelasticity on Static Longitudinal Stability and Control of a Swept-back-wing Airplane written by Richard B. Skoog and published by . This book was released on 1951 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Longitudinal, Directional, and Lateral Stability and Control Data at a Mach Number of 6.83 of the Final Configuration of the X-15 Research Airplane by : Jim A. Penland
Download or read book Static Longitudinal, Directional, and Lateral Stability and Control Data at a Mach Number of 6.83 of the Final Configuration of the X-15 Research Airplane written by Jim A. Penland and published by . This book was released on 1960 with total page 150 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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.
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:
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
Book Synopsis Flight Investigation of Pilot's Ability to Control an Airplane Having Positive and Negative Static Longitudinal Stability Coupled with Various Effective Lift-curve Slopes by : Roy F. Brissenden
Download or read book Flight Investigation of Pilot's Ability to Control an Airplane Having Positive and Negative Static Longitudinal Stability Coupled with Various Effective Lift-curve Slopes written by Roy F. Brissenden and published by . This book was released on 1960 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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.
Book Synopsis Static Longitudinal and Lateral Stability and Control Data from an Exploratory Investigation at a Mach Number of 6.86 of an Airplane Configuration Having a Wing of Trapezoidal Plan Form by : David E. Jr Fetterman
Download or read book Static Longitudinal and Lateral Stability and Control Data from an Exploratory Investigation at a Mach Number of 6.86 of an Airplane Configuration Having a Wing of Trapezoidal Plan Form written by David E. Jr Fetterman and published by . This book was released on 1955 with total page 103 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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.
Book Synopsis Flight-test Data on the Static Fore-and-aft Stability of Various German Airplanes by : Walter Hübner
Download or read book Flight-test Data on the Static Fore-and-aft Stability of Various German Airplanes written by Walter Hübner and published by . This book was released on 1933 with total page 668 pages. Available in PDF, EPUB and Kindle. Book excerpt: The static longitudinal stability of an airplane with locked elevator is usually determined by analysis and model tests. The present report proposes to supply the results of such measurements. The method consisted of recording the dynamic pressure versus elevator displacement at different center-of-gravity positions in unaccelerated flight.
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)
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.
Book Synopsis Longitudinal Stability and Control Derivatives Obtained from Flight Data of a PA-30 Aircraft by : Dale R. Turley
Download or read book Longitudinal Stability and Control Derivatives Obtained from Flight Data of a PA-30 Aircraft written by Dale R. Turley and published by . This book was released on 1981 with total page 104 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Longitudinal Stability and Control Derivatives of a Jet Fighter Airplane Extracted from Flight Test Data by Utilizing Maximum Likelihood Estimation by : George G. Steinmetz
Download or read book Longitudinal Stability and Control Derivatives of a Jet Fighter Airplane Extracted from Flight Test Data by Utilizing Maximum Likelihood Estimation written by George G. Steinmetz and published by . This book was released on 1971 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: "A method of parameter extraction for stability and control derivatives of aircraft from flight test data, implementing maximum likelihood estimation, has been developed and successfully applied to actual longitudinal flight test data from a modern sophisticated jet fighter. The results of this application establish the merits of the estimation technique and its computer implementation (allowing full analyst interaction with the program) as well as provide data for the validation of a portion of the Langley differential maneuvering simulator (DMS). The results are presented for all flight test runs in tabular form and as time history comparisons between the estimated states and the actual flight test data."--Page i
