The Bending-moment Distribution of Chambered-span Wing Systems Having Minimum Induced Drag PDF Download
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Author: Clarence D. Cone
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 40
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Book Description
Author: Clarence D. Cone
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 40
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Book Description
Author: Clarence D. Cone
Publisher:
ISBN:
Category :
Languages : en
Pages : 29
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Book Description
Author: Clarence D. Cone
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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Book Description
Author: Clarence D. Cone
Publisher:
ISBN:
Category :
Languages : en
Pages : 29
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Book Description
Author: Robert T. Jones
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 708
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Book Description
The problem of the minimum induced drag of wings having a given lift and a given span is extended to include cases in which the bending moment to be supported by the wing is also given. Expressions for the spanwise load distribution and the minimum drag in terms of the lateral position of the load centroid are given. The results show a 15-percent reduction of the induced drag with a 15-percent increase in span over that for an elliptic loading having the same total lift and bending moment.
Author: Clarence D. Cone
Publisher:
ISBN:
Category :
Languages : en
Pages : 26
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Author: United States. Department of Commerce. Office of Technical Services
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 618
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Author: Karl L. E. Nickel
Publisher:
ISBN:
Category :
Languages : en
Pages : 43
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Let L, R, Y be arbitrary real constants. A wing with fixed span which produces lift L, roll moment R, yaw moment Y and which has minimal induced drag D is wanted. This problem arises in airplane engineering. It is solved by means of Prandtl's lifting line theory combined with computation. (Author).
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 92
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Author: Keisuke Asai
Publisher:
ISBN:
Category :
Languages : ja
Pages : 22
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