Flight Performance of Fixed and Rotary Wing Aircraft

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Author :
Publisher : Elsevier
ISBN 13 : 0080461034
Total Pages : 600 pages
Book Rating : 4.0/5 (84 download)

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Book Synopsis Flight Performance of Fixed and Rotary Wing Aircraft by : Antonio Filippone

Download or read book Flight Performance of Fixed and Rotary Wing Aircraft written by Antonio Filippone and published by Elsevier. This book was released on 2006-05-10 with total page 600 pages. Available in PDF, EPUB and Kindle. Book excerpt: Calculation and optimisation of flight performance is required to design or select new aircraft, efficiently operate existing aircraft, and upgrade aircraft. It provides critical data for aircraft certification, accident investigation, fleet management, flight regulations and safety. This book presents an unrivalled range of advanced flight performance models for both transport and military aircraft, including the unconventional ends of the envelopes. Topics covered include the numerical solution of supersonic acceleration, transient roll, optimal climb of propeller aircraft, propeller performance, long-range flight with en-route stop, fuel planning, zero-gravity flight in the atmosphere, VSTOL operations, ski jump from aircraft carrier, optimal flight paths at subsonic and supersonic speed, range-payload analysis of fixed- and rotary wing aircraft, performance of tandem helicopters, lower-bound noise estimation, sonic boom, and more. This book will be a valuable text for undergraduate and post-graduate level students of aerospace engineering. It will also be an essential reference and resource for practicing aircraft engineers, aircraft operations managers and organizations handling air traffic control, flight and flying regulations, standards, safety, environment, and the complex financial aspects of flying aircraft. Unique coverage of fixed and rotary wing aircraft in a unified manner, including optimisation, emissions control and regulation. Ideal for students, aeronautical engineering capstone projects, and for widespread professional reference in the aerospace industry. Comprehensive coverage of computer-based solution of aerospace engineering problems; the critical analysis of performance data; and case studies from real world engineering experience. Supported by end of chapter exercises

Flight Testing of Fixed Wing Aircraft

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Author :
Publisher : AIAA
ISBN 13 : 9781600860560
Total Pages : 464 pages
Book Rating : 4.8/5 (65 download)

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Book Synopsis Flight Testing of Fixed Wing Aircraft by : Ralph D. Kimberlin

Download or read book Flight Testing of Fixed Wing Aircraft written by Ralph D. Kimberlin and published by AIAA. This book was released on 2003 with total page 464 pages. Available in PDF, EPUB and Kindle. Book excerpt: Annotation The measurement of performance during an airplane's flight, testing is one of the more important tasks to be accomplished during its development as it impacts on both the airplane's safety and its marketability. This book discusses performance for both propeller-driven and jet aircraft.

Fundamentals of fixed and rotary wing aerodynamics

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Author :
Publisher :
ISBN 13 :
Total Pages : 332 pages
Book Rating : 4.:/5 (2 download)

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Book Synopsis Fundamentals of fixed and rotary wing aerodynamics by :

Download or read book Fundamentals of fixed and rotary wing aerodynamics written by and published by . This book was released on 1984 with total page 332 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Advanced Aircraft Flight Performance

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Author :
Publisher : Cambridge University Press
ISBN 13 : 113978966X
Total Pages : pages
Book Rating : 4.1/5 (397 download)

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Book Synopsis Advanced Aircraft Flight Performance by : Antonio Filippone

Download or read book Advanced Aircraft Flight Performance written by Antonio Filippone and published by Cambridge University Press. This book was released on 2012-12-17 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: This book discusses aircraft flight performance, focusing on commercial aircraft but also considering examples of high-performance military aircraft. The framework is a multidisciplinary engineering analysis, fully supported by flight simulation, with software validation at several levels. The book covers topics such as geometrical configurations, configuration aerodynamics and determination of aerodynamic derivatives, weight engineering, propulsion systems (gas turbine engines and propellers), aircraft trim, flight envelopes, mission analysis, trajectory optimisation, aircraft noise, noise trajectories and analysis of environmental performance. A unique feature of this book is the discussion and analysis of the environmental performance of the aircraft, focusing on topics such as aircraft noise and carbon dioxide emissions.

Rotary-Wing Aerodynamics

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Author :
Publisher : Courier Corporation
ISBN 13 : 0486318516
Total Pages : 640 pages
Book Rating : 4.4/5 (863 download)

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Book Synopsis Rotary-Wing Aerodynamics by : W. Z. Stepniewski

Download or read book Rotary-Wing Aerodynamics written by W. Z. Stepniewski and published by Courier Corporation. This book was released on 2013-04-22 with total page 640 pages. Available in PDF, EPUB and Kindle. Book excerpt: DIVClear, concise text covers aerodynamic phenomena of the rotor and offers guidelines for helicopter performance evaluation. Originally prepared for NASA. Prefaces. New Indexes. 10 black-and-white photos. 537 figures. /div

The Future of Aerospace

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Author :
Publisher : National Academies Press
ISBN 13 : 0309048818
Total Pages : 88 pages
Book Rating : 4.3/5 (9 download)

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Book Synopsis The Future of Aerospace by : National Academy of Engineering

Download or read book The Future of Aerospace written by National Academy of Engineering and published by National Academies Press. This book was released on 1993-02-01 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt: Few technological advances have affected the lives and dreams of individuals and the operations of companies and governments as much as the continuing development of flight. From space exploration to package transport, from military transport to passenger helicopter use, from passenger jumbo jets to tilt-rotor commuter planes, the future of flying is still rapidly developing. The essays in this volume survey the state of progress along several fronts of this constantly evolving frontier. Five eminent authorities assess prospects for the future of rotary-wing aircraft, large passenger aircraft, commercial aviation, manned spaceflight, and defense aerospace in the post-Cold War era.

Steady Aircraft Flight and Performance

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Author :
Publisher : Princeton University Press
ISBN 13 : 9781400839063
Total Pages : 416 pages
Book Rating : 4.8/5 (39 download)

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Book Synopsis Steady Aircraft Flight and Performance by : N. Harris McClamroch

Download or read book Steady Aircraft Flight and Performance written by N. Harris McClamroch and published by Princeton University Press. This book was released on 2011-01-03 with total page 416 pages. Available in PDF, EPUB and Kindle. Book excerpt: This undergraduate textbook offers a unique introduction to steady flight and performance for fixed-wing aircraft from a twenty-first-century flight systems perspective. Emphasizing the interplay between mathematics and engineering, it fully explains the fundamentals of aircraft flight and develops the basic algebraic equations needed to obtain the conditions for gliding flight, level flight, climbing and descending flight, and turning flight. It covers every aspect of flight performance, including maximum and minimum air speed, maximum climb rate, minimum turn radius, flight ceiling, maximum range, and maximum endurance. Steady Aircraft Flight and Performance features in-depth case studies of an executive jet and a general aviation propeller-driven aircraft, and uses MATLAB to compute and illustrate numerous flight performance measures and flight envelopes for each. Requiring only sophomore-level calculus and physics, it also includes a section on translational flight dynamics that makes a clear connection between steady flight and flight dynamics, thereby providing a bridge to further study. Offers the best introduction to steady aircraft flight and performance Provides a comprehensive treatment of the full range of steady flight conditions Covers steady flight performance and flight envelopes, including maximum and minimum air speed, maximum climb rate, minimum turn radius, and flight ceiling Uses mathematics and engineering to explain aircraft flight Features case studies of actual aircraft, illustrated using MATLAB Seamlessly bridges steady flight and translational flight dynamics

Fixed and Flapping Wing Aerodynamics for Micro Air Vehicle Applications

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Author :
Publisher : AIAA
ISBN 13 : 9781600864469
Total Pages : 614 pages
Book Rating : 4.8/5 (644 download)

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Book Synopsis Fixed and Flapping Wing Aerodynamics for Micro Air Vehicle Applications by : Thomas J. Mueller

Download or read book Fixed and Flapping Wing Aerodynamics for Micro Air Vehicle Applications written by Thomas J. Mueller and published by AIAA. This book was released on 2001 with total page 614 pages. Available in PDF, EPUB and Kindle. Book excerpt: This title reports on the latest research in the area of aerodynamic efficency of various fixed-wing, flapping wing, and rotary wing concepts. It presents the progress made by over fifty active researchers in the field.

Rotorcraft Aeromechanics

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Publisher : Cambridge University Press
ISBN 13 : 1107355281
Total Pages : pages
Book Rating : 4.1/5 (73 download)

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Book Synopsis Rotorcraft Aeromechanics by : Wayne Johnson

Download or read book Rotorcraft Aeromechanics written by Wayne Johnson and published by Cambridge University Press. This book was released on 2013-04-29 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: A rotorcraft is a class of aircraft that uses large-diameter rotating wings to accomplish efficient vertical take-off and landing. The class encompasses helicopters of numerous configurations (single main rotor and tail rotor, tandem rotors, coaxial rotors), tilting proprotor aircraft, compound helicopters, and many other innovative configuration concepts. Aeromechanics covers much of what the rotorcraft engineer needs: performance, loads, vibration, stability, flight dynamics, and noise. These topics include many of the key performance attributes and the often-encountered problems in rotorcraft designs. This comprehensive book presents, in depth, what engineers need to know about modelling rotorcraft aeromechanics. The focus is on analysis, and calculated results are presented to illustrate analysis characteristics and rotor behaviour. The first third of the book is an introduction to rotorcraft aerodynamics, blade motion, and performance. The remainder of the book covers advanced topics in rotary wing aerodynamics and dynamics.

Rotary Wing Aircraft Handbooks and History: Special types of rotary wing aircraft

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Author :
Publisher :
ISBN 13 :
Total Pages : 142 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Rotary Wing Aircraft Handbooks and History: Special types of rotary wing aircraft by : Eugene K. Liberatore

Download or read book Rotary Wing Aircraft Handbooks and History: Special types of rotary wing aircraft written by Eugene K. Liberatore and published by . This book was released on 1954 with total page 142 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Flight Stability and Automatic Control

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Author :
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.

Advanced Aircraft Flight Performance

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Author :
Publisher : Cambridge University Press
ISBN 13 : 1107024005
Total Pages : 665 pages
Book Rating : 4.1/5 (7 download)

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Book Synopsis Advanced Aircraft Flight Performance by : Antonio Filippone

Download or read book Advanced Aircraft Flight Performance written by Antonio Filippone and published by Cambridge University Press. This book was released on 2012-12-17 with total page 665 pages. Available in PDF, EPUB and Kindle. Book excerpt: This unique book deals with the aeroplane at several levels and aims to simulate its flight performance using computer software.

Rotary Wing Aircraft Handbooks and History: Convertible aircraft

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Author :
Publisher :
ISBN 13 :
Total Pages : 86 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Rotary Wing Aircraft Handbooks and History: Convertible aircraft by : Eugene K. Liberatore

Download or read book Rotary Wing Aircraft Handbooks and History: Convertible aircraft written by Eugene K. Liberatore and published by . This book was released on 1954 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Foundations of Helicopter Flight

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Author :
Publisher : Elsevier
ISBN 13 : 0080928544
Total Pages : 317 pages
Book Rating : 4.0/5 (89 download)

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Book Synopsis Foundations of Helicopter Flight by : S. Newman

Download or read book Foundations of Helicopter Flight written by S. Newman and published by Elsevier. This book was released on 1994-04-07 with total page 317 pages. Available in PDF, EPUB and Kindle. Book excerpt: The unique design problems which helicopters produce are many and complex. Through practical examples and illustrated case studies, supported by all the relevant theory, this primer text provides an accessible introduction which guides the reader through the theory, design, construction and operation of helicopters. Fundamental performance and control equations are developed, from which the book explores the rotor aerodynamic and dynamic characteristics of helicopters. Example calculations and performance predictions, reflecting current practice, show how to assess the feasibility of a design. * Tackles the theory, design, construction and operation of helicopters* Illustrated with many practical examples and case studies* Provides the fundamental equations describing performance and dynamic behaviour

An Introduction to Aircraft Performance

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Author :
Publisher : AIAA
ISBN 13 : 9781600860249
Total Pages : 366 pages
Book Rating : 4.8/5 (62 download)

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Book Synopsis An Introduction to Aircraft Performance by : Mario Asselin

Download or read book An Introduction to Aircraft Performance written by Mario Asselin and published by AIAA. This book was released on 1997 with total page 366 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Introduction of the M-85 High-speed Rotorcraft Concept

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Author :
Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Introduction of the M-85 High-speed Rotorcraft Concept by :

Download or read book Introduction of the M-85 High-speed Rotorcraft Concept written by and published by . This book was released on 1991 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Stability and Control of Airplanes and Helicopters

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Author :
Publisher : Academic Press
ISBN 13 : 148322015X
Total Pages : 522 pages
Book Rating : 4.4/5 (832 download)

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Book Synopsis Stability and Control of Airplanes and Helicopters by : Edward Seckel

Download or read book Stability and Control of Airplanes and Helicopters written by Edward Seckel and published by Academic Press. This book was released on 2014-05-10 with total page 522 pages. Available in PDF, EPUB and Kindle. Book excerpt: Stability 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.