Author: Lynn W. HuntonPublisher:
ISBN:
Category :
Languages : en
Pages : 36
Book Description
Effects of Twist and Camber on the Low-speed Characteristics of a Large-scale 45 Degree Swept-back Wing
Author: Lynn W. HuntonEffects of Twist and Camber on the Low-speed Characteristics of a Large-scale 45 Degrees Swept-back Wing
Author: Lynn W. HuntonEffects of Twist and Camber on the Low-speed Characteristics of a Large-scale 45° Swept-back Wing
Author: Lynn W. HuntonPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 32
Book Description
Effects of Twist and Camber on the Low-speed Longitudinal Stability Characteristics of a 45© Swept-back Wing of Aspect Ratio 8 at Reynolds Numbers from 1.5 X 106 to 4.8 X 10 as Determined by Pressure Distributions, Force Tests, and Calculations
Author: George L. PrattPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 110
Book Description
Effects of Double-slotted Flaps and Leading-edge Modifications on the Low-speed Characteristics of a Large-scale 45 Degree Swept-back Wing with and Without Camber and Twist
Author: Harry A. JamesThe Effects of Camber and Twist on the Aerodynamic Loading and Stalling Characteristics of a Large-scale 45 Degrees Swept-back Wing
Author: Lynn W. HuntonEffects of Twist and Camber on the Low-speed Longitudinal Stability Characteristics of a 45 Degree Sweptback Wing of Aspect Ratio 8 at Reynolds Numbers from 1.5 X (10)6 to 4.8 X (10)6 as Determined by Pressure Distributions, Force Tests, and Calculations
Author: George L. PrattEffects of Twist and Camber on the Low-speed Longitudinal Stability Characteristics of a 45 Degree Sweptback Wing of Aspect Ratio 8 at Reynolds Numbers from 1.5 X 10(exp 6) to 4.8 X 10(exp 6) as Determined by Pressure Distributions, Force Tests
Author: George L. PrattWing Theory
Author: Robert Thomas JonesPublisher: Princeton University Press
ISBN: 1400860776
Category : Technology & Engineering
Languages : en
Pages : 227
Book Description
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.
Author: George L. Pratt