introduction to aircraft performance selection and design

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Introduction To Aircraft Performance Selection And Design

Author : Francis J. Hale
ISBN : UOM:39015040352984
Genre : Technology & Engineering
File Size : 50. 12 MB
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A self-contained in-depth treatment of aircraft performance, designed for a first course in aeronautical or aerospace engineering for undergraduate engineers. Provides an understanding of why conventional aircraft look and fly the way they do. This well written text covers turbofan and turboprop propulsion, subjects often avoided in other texts. New to the text is the treatment of wind effects on aircraft. Includes illustrative examples and references to practical piloting procedures and the significance of parameters.

Solutions Manual To Accompany Introduction To Aircraft Performance Selection And Design

Author : Francis J. Hale
ISBN : 0471882852
Genre : Aeronautics
File Size : 52. 72 MB
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Aircraft Performance

Author : Mohammad H. Sadraey
ISBN : 9781498776561
Genre : Science
File Size : 71. 29 MB
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Aircraft Performance: An Engineering Approach introduces flight performance analysis techniques that enable readers to determine performance and flight capabilities of aircraft. Flight performance analysis for prop-driven and jet aircraft is explored, supported by examples and illustrations, many in full color. MATLAB programming for performance analysis is included, and coverage of modern aircraft types is emphasized. The text builds a strong foundation for advanced coursework in aircraft design and performance analysis.

Aircraft Performance

Author : Maido Saarlas
ISBN : 9780470044162
Genre : Technology & Engineering
File Size : 81. 81 MB
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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.

Advanced Aircraft Design

Author : Egbert Torenbeek
ISBN : 9781118568095
Genre : Technology & Engineering
File Size : 47. 92 MB
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Although the overall appearance of modern airliners has notchanged a lot since the introduction of jetliners in the 1950s,their safety, efficiency and environmental friendliness haveimproved considerably. Main contributors to this have been gasturbine engine technology, advanced materials, computationalaerodynamics, advanced structural analysis and on-board systems.Since aircraft design became a highly multidisciplinary activity,the development of multidisciplinary optimization (MDO) has becomea popular new discipline. Despite this, the application of MDOduring the conceptual design phase is not yet widespread. Advanced Aircraft Design: Conceptual Design, Analysis andOptimization of Subsonic Civil Airplanes presents aquasi-analytical optimization approach based on a concise set ofsizing equations. Objectives are aerodynamic efficiency, missionfuel, empty weight and maximum takeoff weight. Independent designvariables studied include design cruise altitude, wing area andspan and thrust or power loading. Principal features ofintegrated concepts such as the blended wing and body and highlynon-planar wings are also covered. The quasi-analytical approach enables designers to compare theresults of high-fidelity MDO optimization with lower-fidelitymethods which need far less computational effort. Another advantageto this approach is that it can provide answers to “whatif” questions rapidly and with little computational cost. Key features: Presents a new fundamental vision on conceptual airplane designoptimization Provides an overview of advanced technologies for propulsionand reducing aerodynamic drag Offers insight into the derivation of design sensitivityinformation Emphasizes design based on first principles Considers pros and cons of innovative configurations Reconsiders optimum cruise performance at transonic Machnumbers Advanced Aircraft Design: Conceptual Design, Analysis andOptimization of Subsonic Civil Airplanes advances understandingof the initial optimization of civil airplanes and is a must-havereference for aerospace engineering students, applied researchers,aircraft design engineers and analysts.

Theory And Practice Of Aircraft Performance

Author : Ajoy Kumar Kundu
ISBN : 9781119074175
Genre : Technology & Engineering
File Size : 83. 33 MB
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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

Performance And Stability Of Aircraft

Author : J. Russell
ISBN : 9780080538648
Genre : Business & Economics
File Size : 25. 73 MB
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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

Volume 1 Performance Phase Chapter 1 Introduction To Aircraft Performance Testing

Author :
ISBN : OCLC:227837874
Genre :
File Size : 42. 59 MB
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Aircraft performance can be defined as the ability of an aircraft to climb, accelerate, or maneuver in order to successfully accomplish its mission. Obviously, expected performance specifications must be an integral part of the design process of an aircraft. Given certain performance expectations by the customer, the designer must make decisions regarding wing loading, power plant selection, airfoil selection, planform configuration, and many other considerations. All of these help to tailor the design to give the aircraft the desired performance characteristics. It is also certain that actual performance characteristics will not always be the same as those predicted by the designer. Herein lies the need for performance flight testing. Performance flight testing is defined as the process of determining aircraft performance characteristics, or in a more modern sense, evaluation of the energy gaining and losing capability of the aircraft. Determination of aircraft performance is dependent upon our knowledge of fundamentals in several different scientific disciplines. In order to predict or measure an aircraft's performance, we must be able to estimate the aerodynamic forces involved. This requires knowledge of the properties and behavior of the fluid medium in which we operate, i.e., the earth's atmosphere. Therefore, we must study atmospheric science, fluid dynamics, thermodynamics, and aerodynamics. Performance prediction or measurement requires knowledge of the aircraft propulsion system. Hence, we must be familiar with the theory and operation of basic turbine and turbine variant engines, reciprocating internal-combustion engines, and propeller theory. We must also understand the basic measurements, instrumentation techniques, and equipment used to gather the data needed to determine an aircraft's performance.

Aircraft Performance

Author : W. Austyn Mair
ISBN : 0521568366
Genre : Science
File Size : 34. 72 MB
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Describes the principles and equations required for evaluating the performance of an aircraft.

Introduction To Aircraft Structural Analysis

Author : T.H.G. Megson
ISBN : 1856179338
Genre : Technology & Engineering
File Size : 30. 70 MB
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Introduction to Aircraft Structural Analysis is an essential resource for learning aircraft structural analysis. Based on the author's best-selling book Aircraft Structures for Engineering Students, this brief text introduces the reader to the basics of structural analysis as applied to aircraft structures. Coverage of elasticity, energy methods and virtual work sets the stage for discussions of airworthiness/airframe loads and stress analysis of aircraft components. Numerous worked examples, illustrations, and sample problems show how to apply the concepts to realistic situations. The book covers the core concepts in about 200 fewer pages by removing some optional topics like structural vibrations and aero elasticity. It consists of 23 chapters covering a variety of topics from basic elasticity to torsion of solid sections; energy methods; matrix methods; bending of thin plates; structural components of aircraft; airworthiness; airframe loads; bending of open, closed, and thin walled beams; combined open and closed section beams; wing spars and box beams; and fuselage frames and wing ribs. This book will appeal to undergraduate and postgraduate students of aerospace and aeronautical engineering, as well as professional development and training courses. Based on the author's best-selling text Aircraft Structures for Engineering Students, this Intro version covers the core concepts in about 200 fewer pages by removing some optional topics like structural vibrations and aeroelasticity Systematic step by step procedures in the worked examples Self-contained, with complete derivations for key equations

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