Effects of Three Spanwise Twist Variations on the Longitudinal Aerodynamic Characteristics of a Thin 45° Sweptback Highly Tapered Wing at Transonic Speeds PDF Download
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Author: John P. Mugler
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 50
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Book Description
Author: John P. Mugler
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 50
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Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 44
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 986
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1386
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 642
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1212
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Author: Royal Aeronautical Society
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 972
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Author: Robert C. Nelson
Publisher:
ISBN:
Category : History
Languages : en
Pages : 464
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Book Description
This edition of this this flight stability and controls guide features an unintimidating math level, full coverage of terminology, and expanded discussions of classical to modern control theory and autopilot designs. Extensive examples, problems, and historical notes, make this concise book a vital addition to the engineer's library.
Author: Dietrich Küchemann
Publisher: AIAA Education
ISBN: 9781600869228
Category : Technology & Engineering
Languages : en
Pages : 0
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Book Description
Dietrich Kuchemann's The Aerodynamic Design of Aircraft is as relevant and as forward looking today as it was when it was first published in 1978. It comprises the philosophy and life's work of a unique and visionary intellect. Based upon material taught in a course at Imperial College London, the insight and intuition conveyed by this text are timeless. With its republication, Kuchemann's influence will extend to the next generation of aerospace industry students and practitioners and the vehicles they will produce. Kuchemann establishes three classes of aircraft based on the character of flow involved. Each class is suitable for a distinct cruise speed regime: classical and swept aircraft for subsonic and transonic cruise, slender-wing aircraft for supersonic cruise, and wave-rider aircraft for hypersonic cruise. Unlike most engineering texts, which focus on a set of tools, Kuchemann's approach is to focus on the problem and its solution - what kind of flow is best for a given class of aircraft and how to achieve it.With this approach, Kuchemann fully embraces the true inverse nature of design; rather than answer what flow given the shape, he strives to answer what flow given the purpose and then what shape given the flow.
Author: Harvey H. Hubbard
Publisher:
ISBN:
Category : Aerodynamic noise
Languages : en
Pages : 620
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Book Description
