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An Introduction to Aircraft Performance

Author: Mario Asselin
Publisher: AIAA
ISBN: 9781600860249
Category : Airplanes
Languages : en
Pages : 354

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Book Description

An Introduction to Aircraft Performance

Author: Mario Asselin
Publisher: AIAA
ISBN: 9781600860249
Category : Airplanes
Languages : en
Pages : 354

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Book Description

Introduction to Aircraft Performance, Selection, and Design

Author: Francis J. Hale
Publisher: John Wiley & Sons Incorporated
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 344

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Book Description
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.

Introduction to aircraft performance calculations

Author: P.H.. Sumner
Publisher:
ISBN:
Category :
Languages : en
Pages : 83

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Book Description

Theory and Practice of Aircraft Performance

Author: Ajoy Kumar Kundu
Publisher: John Wiley & Sons
ISBN: 1119074177
Category : Technology & Engineering
Languages : en
Pages : 704

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Book Description
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

Steady Aircraft Flight and Performance

Author: N. Harris McClamroch
Publisher: Princeton University Press
ISBN: 9781400839063
Category : Technology & Engineering
Languages : en
Pages : 416

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Book Description
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

Aircraft Performance and Design

Author: Mitra
Publisher: Ambar K. Mitra
ISBN: 9780999746615
Category :
Languages : en
Pages : 208

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Book Description
This book addresses the fundamentals of aircraft performance and design and the required background of readers is sophomore level physics and calculus. The purpose is to excite the sophomores, in an aerospace program, about airplanes without overwhelming them with differential equations and complex calculus. People with a fascination of airplanes will find many of their 'how, why, and what' questions answered in this book. Even seniors will find the concepts and practices useful for their capstone design projects.

Solutions Manual to Accompany Introduction to Aircraft Performance, Selection, and Design

Author: Francis J. Hale
Publisher: Wiley
ISBN: 9780471882855
Category : Aeronautics
Languages : en
Pages : 124

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Book Description

Introduction to Aviation Management

Author: Andreas Wald
Publisher: LIT Verlag Münster
ISBN: 3643106262
Category : Business & Economics
Languages : en
Pages : 385

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Book Description
This volume provides an introduction to aviation management covering all major actors and processes, the fundamental structures, and the economic and regulatory background of the industry. It comprises contributions from experienced practitioners of the aviation industry and from scholars in that field.

Aircraft Performance

Author: Maido Saarlas
Publisher: John Wiley & Sons
ISBN: 0470044160
Category : Technology & Engineering
Languages : en
Pages : 298

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Book Description
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.

Aerodynamics and Aircraft Performance

Author: James F. Marchman
Publisher: James F. Marchman
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 318

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Book Description
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.