An Investigation of Wing and Aileron Loads Due to Deflected Inboard and Outboard Ailerons on a 4-percent-thick 30 Degree Swepptback Wing at Transonic Speeds PDF Download

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An Investigation of Wing and Aileron Loads Due to Deflected Inboard and Outboard Ailerons on a 4-percent-thick 30 Degree Swepptback Wing at Transonic Speeds

An Investigation of Wing and Aileron Loads Due to Deflected Inboard and Outboard Ailerons on a 4-percent-thick 30 Degree Swepptback Wing at Transonic Speeds PDF Author: Charles F. Whitcomb
Publisher:
ISBN:
Category :
Languages : en
Pages : 286

Book Description

An Investigation of Wing and Aileron Loads Due to Deflected Inboard and Outboard Ailerons on a 4-percent-thick 30 Degree Swepptback Wing at Transonic Speeds

An Investigation of Wing and Aileron Loads Due to Deflected Inboard and Outboard Ailerons on a 4-percent-thick 30 Degree Swepptback Wing at Transonic Speeds PDF Author: Charles F. Whitcomb
Publisher:
ISBN:
Category :
Languages : en
Pages : 286

Book Description

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Publisher:
ISBN:
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Publisher:
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Publisher:
ISBN:
Category : History
Languages : en
Pages : 464

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Publisher: Springer
ISBN: 3319319183
Category : Technology & Engineering
Languages : en
Pages : 272

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This book is based on lectures held at the faculty of mechanical engineering at the Technical University of Kaiserslautern. The focus is on the central theme of societies overall aircraft requirements to specific material requirements and highlights the most important advantages and challenges of carbon fiber reinforced plastics (CFRP) compared to conventional materials. As it is fundamental to decide on the right material at the right place early on the main activities and milestones of the development and certification process and the systematic of defining clear requirements are discussed. The process of material qualification - verifying material requirements is explained in detail. All state-of-the-art composite manufacturing technologies are described, including changes and complemented by examples, and their improvement potential for future applications is discussed. Tangible case studies of high lift and wing structures emphasize the specific advantages and challenges of composite technology. Finally, latest R&D results are discussed, providing possible future solutions for key challenges such as low cost high performance materials, electrical function integration and morphing structures.

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Publisher: AIAA
ISBN: 9781600860782
Category : Aerodynamics
Languages : en
Pages : 666

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Publisher: Springer Science & Business Media
ISBN: 3662026465
Category : Technology & Engineering
Languages : en
Pages : 569

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Publisher: Courier Corporation
ISBN: 0486134997
Category : Technology & Engineering
Languages : en
Pages : 708

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Publisher: John Wiley & Sons
ISBN: 0471575062
Category : Technology & Engineering
Languages : en
Pages : 677

Book Description
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Publisher:
ISBN: 9781626830219
Category : Research aircraft
Languages : en
Pages : 334

Book Description
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