Flight Vehicle Performance And Aerodynamic Control PDF Download
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| Author | : Frederick O. Smetana |
| Publisher | : AIAA |
| Total Pages | : 392 |
| Release | : 2001 |
| Genre | : Aerodynamics |
| ISBN | : 9781600860577 |
Download Flight Vehicle Performance and Aerodynamic Control Book in PDF, ePub and Kindle
Annotation "Flight Vehicle Performance and Aerodynamic Control is designed to serve as a text for either an 11-week or a 16-week course at the sophomore level. It explains typical methods used to estimate aircraft performance, the theoretical basis of these methods, and how various parameters derived from the aircraft geometry can be used to estimate the requirements of control surfaces and the aerodynamic forces required to actuate these surfaces. This book includes time-tested computer programs that perform the analyses in a manner that reduces student error and improves result accuracy. Because the source code is given, users with a FORTRAN compiler can modify the program to suit particular needs. The major advantage of the software is that more realistic problems may be treated and the effects of parametric programs are more accurate than calculators. The programs are available as executables for Windows machines as well as in ASCII source code versions that can be readily compiled and then executed on Unix, Linux, and Macintosh machines and on mainframes.
| Author | : Bandu N. Pamadi |
| Publisher | : AIAA |
| Total Pages | : 810 |
| Release | : 2004 |
| Genre | : Aerodynamics |
| ISBN | : 9781600860997 |
Download Performance, Stability, Dynamics, and Control of Airplanes Book in PDF, ePub and Kindle
| Author | : Thomas R. Yechout |
| Publisher | : AIAA |
| Total Pages | : 666 |
| Release | : 2003 |
| Genre | : Aerodynamics |
| ISBN | : 9781600860782 |
Download Introduction to Aircraft Flight Mechanics Book in PDF, ePub and Kindle
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.
| Author | : Frederick O. Smetana |
| Publisher | : McGraw-Hill Companies |
| Total Pages | : 664 |
| Release | : 1984 |
| Genre | : Aerodynamics |
| ISBN | : |
Download Computer Assisted Analysis of Aircraft Performance, Stability, and Control Book in PDF, ePub and Kindle
| Author | : David G. Hull |
| Publisher | : Springer Science & Business Media |
| Total Pages | : 311 |
| Release | : 2007-01-20 |
| Genre | : Technology & Engineering |
| ISBN | : 3540465731 |
Download Fundamentals of Airplane Flight Mechanics Book in PDF, ePub and Kindle
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.
| Author | : Mark Drela |
| Publisher | : MIT Press |
| Total Pages | : 304 |
| Release | : 2014-02-07 |
| Genre | : Science |
| ISBN | : 0262526441 |
Download Flight Vehicle Aerodynamics Book in PDF, ePub and Kindle
An overview of the physics, concepts, theories, and models underlying the discipline of aerodynamics. This book offers a general overview of the physics, concepts, theories, and models underlying the discipline of aerodynamics. A particular focus is the technique of velocity field representation and modeling via source and vorticity fields and via their sheet, filament, or point-singularity idealizations. These models provide an intuitive feel for aerodynamic flow-field behavior and are the basis of aerodynamic force analysis, drag decomposition, flow interference estimation, and other important applications. The models are applied to both low speed and high speed flows. Viscous flows are also covered, with a focus on understanding boundary layer behavior and its influence on aerodynamic flows. The book covers some topics in depth while offering introductions and summaries of others. Computational methods are indispensable for the practicing aerodynamicist, and the book covers several computational methods in detail, with a focus on vortex lattice and panel methods. The goal is to improve understanding of the physical models that underlie such methods. The book also covers the aerodynamic models that describe the forces and moments on maneuvering aircraft, and provides a good introduction to the concepts and methods used in flight dynamics. It also offers an introduction to unsteady flows and to the subject of wind tunnel measurements. The book is based on the MIT graduate-level course “Flight Vehicle Aerodynamics” and has been developed for use not only in conventional classrooms but also in a massive open online course (or MOOC) offered on the pioneering MOOC platform edX. It will also serve as a valuable reference for professionals in the field. The text assumes that the reader is well versed in basic physics and vector calculus, has had some exposure to basic fluid dynamics and aerodynamics, and is somewhat familiar with aerodynamics and aeronautics terminology.
| Author | : Eric T. Falangas |
| Publisher | : John Wiley & Sons |
| Total Pages | : 432 |
| Release | : 2015-12-21 |
| Genre | : Technology & Engineering |
| ISBN | : 1119009766 |
Download Performance Evaluation and Design of Flight Vehicle Control Systems Book in PDF, ePub and Kindle
The purpose of this book is to assist analysts, engineers, and students toward developing dynamic models, and analyzing the control of flight vehicles with various blended features comprising aircraft, launch vehicles, reentry vehicles, missiles and aircraft. Graphical methods for analysing vehicle performance Methods for trimming deflections of a vehicle that has multiple types of effectors Presents a parameters used for speedily evaluating the performance, stability, and controllability of a new flight vehicle concept along a trajectory or with fixed flight conditions
| Author | : Courtland D. Perkins |
| Publisher | : John Wiley & Sons |
| Total Pages | : 514 |
| Release | : 1949-01-15 |
| Genre | : Technology & Engineering |
| ISBN | : |
Download Airplane Performance, Stability and Control Book in PDF, ePub and Kindle
First written in 1949, this is a classic text in aeronautical engineering. It covers airplane performance in reciprocating engine craft, propeller performance, as well as aircraft stability and control. This is an excellent book for the professional and the serious amateur aircraft maker. It is written in a straightforward and easy to understand manner. To get the most out of this book, readers should have an understanding of differential calculus.
| Author | : Nandan K. Sinha |
| Publisher | : CRC Press |
| Total Pages | : 348 |
| Release | : 2017-06-27 |
| Genre | : Science |
| ISBN | : 1498746063 |
Download Advanced Flight Dynamics with Elements of Flight Control Book in PDF, ePub and Kindle
Advanced Flight Dynamics aim to integrate the subjects of aircraft performance, trim and stability/control in a seamless manner. Advanced Flight Dynamics highlights three key and unique viewpoints. Firstly, it follows the revised and corrected aerodynamic modeling presented previously in recent textbook on Elementary Flight Dynamics. Secondly, it uses bifurcation and continuation theory, especially the Extended Bifurcation Analysis (EBA) procedure devised by the authors, to blend the subjects of aircraft performance, trim and stability, and flight control into a unified whole. Thirdly, rather than select one control design tool or another, it uses the generalized Nonlinear Dynamic Inversion (NDI) methodology to illustrate the fundamental principles of flight control. Advanced Flight Dynamics covers all the standard airplane maneuvers, various types of instabilities normally encountered in flight dynamics and illustrates them with real-life airplane data and examples, thus bridging the gap between the teaching of flight dynamics/ control theory in the university and its practice in airplane design bureaus. The expected reader group for this book would ideally be senior undergraduate and graduate students, practicing aerospace/flight simulation engineers/scientists from industry as well as researchers in various organizations. Key Features: Focus on unified nonlinear approach, with nonlinear analysis tools. Provides an up-to-date, corrected, and unified presentation of aircraft trim, stability and control analysis including nonlinear phenomena and closed-loop stability analysis. Contains a computational tool and real-life example carried through the chapters. Includes complementary nonlinear dynamic inversion control approach, with relevant aircraft examples. Fills the gap in the market for a text including non-linear flight dynamics and continuation methods.
| Author | : Rama K. Yedavalli |
| Publisher | : John Wiley & Sons |
| Total Pages | : 554 |
| Release | : 2020-02-25 |
| Genre | : Technology & Engineering |
| ISBN | : 1118934458 |
Download Flight Dynamics and Control of Aero and Space Vehicles Book in PDF, ePub and Kindle
Flight Vehicle Dynamics and Control Rama K. Yedavalli, The Ohio State University, USA A comprehensive textbook which presents flight vehicle dynamics and control in a unified framework Flight Vehicle Dynamics and Control presents the dynamics and control of various flight vehicles, including aircraft, spacecraft, helicopter, missiles, etc, in a unified framework. It covers the fundamental topics in the dynamics and control of these flight vehicles, highlighting shared points as well as differences in dynamics and control issues, making use of the ‘systems level’ viewpoint. The book begins with the derivation of the equations of motion for a general rigid body and then delineates the differences between the dynamics of various flight vehicles in a fundamental way. It then focuses on the dynamic equations with application to these various flight vehicles, concentrating more on aircraft and spacecraft cases. Then the control systems analysis and design is carried out both from transfer function, classical control, as well as modern, state space control points of view. Illustrative examples of application to atmospheric and space vehicles are presented, emphasizing the ‘systems level’ viewpoint of control design. Key features: Provides a comprehensive treatment of dynamics and control of various flight vehicles in a single volume. Contains worked out examples (including MATLAB examples) and end of chapter homework problems. Suitable as a single textbook for a sequence of undergraduate courses on flight vehicle dynamics and control. Accompanied by a website that includes additional problems and a solutions manual. The book is essential reading for undergraduate students in mechanical and aerospace engineering, engineers working on flight vehicle control, and researchers from other engineering backgrounds working on related topics.
