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E-Book

E-Book, Englisch, 228 Seiten

Reihe: Princeton Legacy Library

Jones Wing Theory


Course Book
ISBN: 978-1-4008-6077-7
Verlag: De Gruyter
Format: PDF
 Kopierschutz: 1 - PDF Watermark

E-Book, Englisch, 228 Seiten

Reihe: Princeton Legacy Library

ISBN: 978-1-4008-6077-7
Verlag: De Gruyter
Format: PDF
 Kopierschutz: 1 - PDF Watermark

Originator of many of the theories used in modern wing design, Robert T. Jones surveys the aerodynamics of wings from the early theories of lift to modern theoretical developments. This work covers the behavior of wings at both low and high speeds, including the range from very low Reynolds numbers to the determination of minimum drag at supersonic speed. Emphasizing analytical techniques, Wing Theory provides invaluable physical principles and insights for advanced students, professors, and aeronautical engineers, as well as for scientists involved in computational approaches to the subject. This book is based on over forty years of theoretical and practical work performed by the author and other leading researchers in the field of aerodynamics.

Originally published in 1990.

The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.

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Autoren/Hrsg.

Jones, Robert Thomas

Fachgebiete

Weitere Infos & Material

FrontMatter, pg. i
CONTENTS, pg. v
Preface, pg. ix
CHAPTER ONE Fundamental Considerations, pg. 3
CHAPTER TWO. Potential Flow over Ellipsoids, pg. 12
CHAPTER THREE. Two-Dimensional Flow: Wing Section Theory, pg. 20
CHAPTER FOUR. Thin Airfoil Theory, pg. 53
CHAPTER FIVE. Influence of Compressibility, pg. 74
CHAPTER SIX. Effects of Sweep, pg. 90
CHAPTER SEVEN. Wings of High Aspect Ratio, pg. 105
CHAPTER EIGHT. Lifting Surface Theory, pg. 129
CHAPTER NINE. The Minimum Drag of Thin Wings, pg. 159
CHAPTER TEN. Drag of Wings and Bodies in Combination, pg. 200
Bibliography, pg. 209
Index, pg. 211

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