Introduction To Aircraft Performance Calculations
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Introduction To Aircraft Performance Calculations
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Author : P.H.. Sumner
language : en
Publisher:
Release Date : 1945
Introduction To Aircraft Performance Calculations written by P.H.. Sumner and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1945 with categories.
Introduction To Aircraft Performance Calculations
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Author : Percy James Hammond Sumner
language : en
Publisher:
Release Date : 1945
Introduction To Aircraft Performance Calculations written by Percy James Hammond Sumner and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1945 with Airplanes categories.
Lærebogsagtig beskrivelse af beregninger og teorien bag luftfartøjets ydeevne (Performance) såsom flyvehastighed, lasteevne, rækkevidde, brændstofforbrug m.m.
Aircraft Performance
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Author : Maido Saarlas
language : en
Publisher: John Wiley & Sons
Release Date : 2006-12-05
Aircraft Performance written by Maido Saarlas and has been published by John Wiley & Sons this book supported file pdf, txt, epub, kindle and other format this book has been release on 2006-12-05 with Technology & Engineering categories.
Aircraft PERFORMANCE STRAIGHTFORWARD METHODS TO DESIGN AND OPERATE AIRCRAFT TO MEET PERFORMANCE SPECIFICATIONS Aircraft Performance sets forth a group of tested and proven methods needed to determine the performance of an aircraft. The central theme of this book is the energy method, which enhances understanding of the standard methods and provides accessibility to advanced topics. As a result, readers gain a thorough understanding of the performance issues involved in operating an aircraft in an efficient and economic manner. While covering all the standard topics—level and climbing flight, range and endurance, take-off and landing, and maneuvering flight—the book focuses on the energy methods applied to path performance analysis. Throughout the text, numerous examples from both the commercial and military sectors show readers how the concepts and calculations are applied to real-life situations. Problems, ranging from basic to complex, test the readers’ understanding and provide an opportunity for essential practice. To help focus the readers’ attention on core issues, this text assumes that aerodynamics and propulsion are known inputs. Special appendices are provided to present some aerodynamic and propulsive equations and data. In general, topics are separated into horizontal and vertical plane approaches. Following an introduction and overview, basic energy concepts are employed to obtain a fundamental performance equation. This text, with its extensive use of examples and problem sets, is ideal for upper- level undergraduate and graduate students in engineering. It also serves as a reference for design engineers in both military and industrial sectors who want a set of clear and reliable methods to calculate aircraft performance.
An Introduction To Aircraft Performance
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Author : Mario Asselin
language : en
Publisher: AIAA
Release Date : 1997
An Introduction To Aircraft Performance written by Mario Asselin and has been published by AIAA this book supported file pdf, txt, epub, kindle and other format this book has been release on 1997 with Airplanes categories.
Introduction To Aircraft Flight Mechanics
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Author : Thomas R. Yechout
language : en
Publisher: AIAA
Release Date : 2003
Introduction To Aircraft Flight Mechanics written by Thomas R. Yechout and has been published by AIAA this book supported file pdf, txt, epub, kindle and other format this book has been release on 2003 with Aerodynamics categories.
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.
Aircraft Performance
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Author : W. Austyn Mair
language : en
Publisher: Cambridge University Press
Release Date : 1996-03-14
Aircraft Performance written by W. Austyn Mair and has been published by Cambridge University Press this book supported file pdf, txt, epub, kindle and other format this book has been release on 1996-03-14 with Science categories.
Describes the principles and equations required for evaluating the performance of an aircraft.
Theory And Practice Of Aircraft Performance
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Author : Ajoy Kumar Kundu
language : en
Publisher: John Wiley & Sons
Release Date : 2016-09-26
Theory And Practice Of Aircraft Performance written by Ajoy Kumar Kundu and has been published by John Wiley & Sons this book supported file pdf, txt, epub, kindle and other format this book has been release on 2016-09-26 with Technology & Engineering categories.
Textbook introducing the fundamentals of aircraft performance using industry standards and examples: bridging the gap between academia and industry Provides an extensive and detailed treatment of all segments of mission profile and overall aircraft performance Considers operating costs, safety, environmental and related systems issues Includes worked examples relating to current aircraft (Learjet 45, Tucano Turboprop Trainer, Advanced Jet Trainer and Airbus A320 types of aircraft) Suitable as a textbook for aircraft performance courses
Introduction To Aircraft Aeroelasticity And Loads
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Author : Jan Robert Wright
language : en
Publisher: John Wiley & Sons
Release Date : 2008-02-08
Introduction To Aircraft Aeroelasticity And Loads written by Jan Robert Wright and has been published by John Wiley & Sons this book supported file pdf, txt, epub, kindle and other format this book has been release on 2008-02-08 with Technology & Engineering categories.
Aircraft performance is influenced significantly both by aeroelastic phenomena, arising from the interaction of elastic, inertial and aerodynamic forces, and by load variations resulting from flight and ground manoeuvres and gust / turbulence encounters. There is a strong link between aeroelasticity and loads, and these topics have become increasingly integrated in recent years. Introduction to Aircraft Aeroelasticity and Loads introduces the reader to the main principles involved in a wide range of aeroelasticity and loads topics. Divided into three sections, the book begins by reviewing the underlying disciplines of vibrations, aerodynamics, loads and control. It goes on to describe simplified models to illustrate aeroelastic behaviour and aircraft response before introducing more advanced methodologies. Finally, it explains how industrial certification requirements for aeroelasticity and loads may be met and relates these to the earlier theoretical approaches used. Presents fundamentals of structural dynamics, aerodynamics, static and dynamic aeroelasticity, response and load calculations and testing techniques. Covers performance issues related to aeroelasticity such as flutter, control effectiveness, divergence and redistribution of lift. Includes up-to-date experimental methods and analysis. Accompanied by a website with MatLAB and SIMULINK programs that relate to the models used. Introduction to Aircraft Aeroelasticity and Loads enables the reader to understand the aeroelastic and loads principles and procedures employed in a modern aircraft design office. It will appeal to final year undergraduate and masters students as well as engineers who are new to the aerospace industry.
Aerodynamics And Aircraft Performance
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Author : James F. Marchman
language : en
Publisher: James F. Marchman
Release Date :
Aerodynamics And Aircraft Performance written by James F. Marchman and has been published by James F. Marchman this book supported file pdf, txt, epub, kindle and other format this book has been release on with Technology & Engineering categories.
Aerodynamics and Aircraft Performance, 3rd edition is a college undergraduate-level introduction to aircraft aerodynamics and performance. This text is designed for a course in Aircraft Performance that is taught before the students have had any course in fluid mechanics, fluid dynamics, or aerodynamics. The text is meant to provide the essential information from these types of courses that is needed for teaching basic subsonic aircraft performance, and it is assumed that the students will learn the full story of aerodynamics in other, later courses. The text assumes that the students will have had a university level Physics sequence in which they will have been introduced to the most fundamental concepts of statics, dynamics, fluid mechanics, and basic conservation laws that are needed to understand the coverage that follows. It is also assumed that students will have completed first year university level calculus sequence plus a course in multi-variable calculus. Separate courses in engineering statics and dynamics are helpful but not necessary. Any student who takes a course using this text after completing courses in aerodynamics or fluid dynamics should find the chapters of this book covering those subjects an interesting review of the material. The 236-page text was created specifically for use by undergraduate students in Aerospace Engineering and was based on Professor Marchman’s many years of experience teaching related subject matter as well as his numerous wind tunnel research projects related to aircraft aerodynamics and his personal experience as the owner and pilot of a general aviation airplane. It has been used at Virginia Tech and other universities.
Performance Of Light Aircraft
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Author : John T. Lowry
language : en
Publisher: AIAA
Release Date : 1999
Performance Of Light Aircraft written by John T. Lowry and has been published by AIAA this book supported file pdf, txt, epub, kindle and other format this book has been release on 1999 with Mathematics categories.
Pilots, aviation students, kitplane builders, aircraft fleet operators and aeronautical engineers can all determine how their propeller-driven airplanes will perform, under any conditions, by using the step-by-step bootstrap approach introduced in this book. A few routine flying manoeuvres (climbs, glides, a level speed run) will give the necessary nine numbers. High-school level calculations then give performance numbers with much greater detail and accuracy than many other methods - for the reader's individual aircraft.