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Aerodynamics and Aircraft Performance
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Aerodynamics and Aircraft Performance, 3rd edition is a college undergraduate-level introductory textbook on 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.

Table of Contents
1. Introduction to Aerodynamics
2. Propulsion
3. Additional Aerodynamics Tools
4. Performance in Striaght and Level Flight
5. Altitude Change: Climb and Glide
6. Range and Endurance
7. Accelerated Performance: Takeoff and Landing
8. Accelerated Performance: Turns
9. The Role of Performance in Aircraft Design: Constraint Analysis
Appendix A: Airfoil Data

Instructors reviewing, adopting, or adapting parts or the whole of the text are requested to register their interest at: https://bit.ly/aerodynamics_interest.

978-1-949373-63-9 (PDF) http://hdl.handle.net/10919/96525
978-1-949373-64-6 (ePub) http://hdl.handle.net/10919/96525
978-1-949373-62-2 (HTML/Pressbooks) https://pressbooks.lib.vt.edu/aerodynamics

Subject:
Applied Science
Engineering
Material Type:
Textbook
Provider:
Virginia Tech
Provider Set:
VTech Works
Author:
James F. Marchman III
Date Added:
08/09/2021
Aerodynamics and Aircraft Performance, 3rd edition
Unrestricted Use
CC BY
Rating
0.0 stars

Short Description:
Aerodynamics and Aircraft Performance, 3rd edition Intended for undergraduates, this text provides “stand alone” coverage of basic, subsonic, aircraft performance preceded by an introduction to the basics of aerodynamics that will provide a background sufficient to the understanding of the subjects to be studied in aircraft performance. NewParaDownloadable versions of this book and further information are freely available at: http://hdl.handle.net/10919/96525NewParaDr. James F. Marchman III is Professor Emeritus of Aerospace and Ocean Engineering and a former Associate Dean of Engineering at Virginia Tech where he taught and conducted research in aerodynamics, aircraft performance, aircraft design and other areas over a 40 year career. NewParaInstructors reviewing, adopting, or adapting parts or the whole of the text are requested to register their interest at: https://bit.ly/aerodynamics_interest.

Long Description:
Aerodynamics and Aircraft Performance, 3rd edition is a college undergraduate-level introduction to aircraft aerodynamics and performance. The objective of this text is to provide a “stand alone” coverage of basic, subsonic, aircraft performance preceded by an introduction to the basics of aerodynamics that will provide a background sufficient to the understanding of the subjects to be studied in aircraft 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

This is a nearly verbatim presentation of Dr. Marchman’s 3rd edition (2004) of the text with minor corrections to text and formulas, addition of machine-readable math, alt text, and redrawn figures. It is available in Pressbooks, PDF, and ePub.

Instructors reviewing, adopting, or adapting parts or the whole of the text are requested to register their interest at: https://bit.ly/aerodynamics_interest.

Downloadable versions of this book and further information are freely available at: http://hdl.handle.net/10919/96525

Word Count: 86443

ISBN: 978-1-949373-62-2

(Note: This resource's metadata has been created automatically by reformatting and/or combining the information that the author initially provided as part of a bulk import process.)

Subject:
Applied Science
Engineering
Material Type:
Textbook
Provider:
Virginia Tech
Author:
James F. Marchman III
Date Added:
08/06/2021