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Author: Caroline Snowden Guild
Publisher:
ISBN:
Category : Children's stories
Languages : en
Pages : 0
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Book Description
Author: Caroline Snowden Guild
Publisher:
ISBN:
Category : Children's stories
Languages : en
Pages : 0
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Book Description
Author: Caroline Snowden Guild
Publisher:
ISBN:
Category : Children
Languages : en
Pages : 210
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Book Description
Author:
Publisher:
ISBN:
Category : Engineering
Languages : en
Pages : 988
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Book Description
Author: United States National Museum
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 828
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Book Description
Author: BPP Learning Media
Publisher: BPP Learning Media
ISBN: 0751782769
Category : Computers
Languages : en
Pages : 87
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Book Description
Support and improve the online web presence by optimising a website to increase traffic, create more impact and generate higher sales and recognition.
Author: Tui T. Sutherland
Publisher: Scholastic UK
ISBN: 1407147773
Category : Juvenile Fiction
Languages : en
Pages : 274
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Book Description
Seven dragon tribes have been at war for generations. A secret movement called the Talons of Peace is determined to bring an end to the fighting, with the help of a prophecy. Five dragonets are enlisted, against their will, to end the terrible war. But when they escape their prison, the result may be more than intended . . .
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Book Description
Author: United States. Army. Corps of Engineers
Publisher:
ISBN:
Category :
Languages : en
Pages : 1074
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 448
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Book Description
Author: George W. Zender
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 692
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Book Description
An approximate method of calculating the deformation of wings of uniform thickness having swept, M or W, Lambda, and swept-tip plan forms is presented. The method employs an adjustment to the elementary beam theory to account for the effect of the triangular root portion portion of a swept wing on the deformation of the outboard section of the wing. To demonstrate the general applicability of the method, the modified elementary theory is applied to the more comples M or W, Lambda, and swept-tip plan forms as well as to swept plan forms. For the purpose of calculating angles of attack, it is shown that the unmodified elementary beam theory applied to that part of the wing outboard of the root triangle produces satisfactory results. However, for calculating deflections it is necessary to include the effects of the root-triangle deformation.
