Effect of Geometric Dihedral on Low-speed Static Stability Characteristics of A 40° Sweptback Wing PDF Download
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Author: Kazimierz J. Orlik-Rückemann
Publisher:
ISBN:
Category :
Languages : en
Pages : 18
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Book Description
Author: Kazimierz J. Orlik-Rückemann
Publisher:
ISBN:
Category :
Languages : en
Pages : 18
Get Book Here
Book Description
Author: Kazimierz Orlik-Ruckemann
Publisher:
ISBN:
Category :
Languages : en
Pages : 18
Get Book Here
Book Description
Author: Kazimierz Orlik-Rückemann
Publisher:
ISBN:
Category :
Languages : en
Pages : 18
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Author: K. Orlik-Rückemann
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ISBN:
Category :
Languages : en
Pages :
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Author: M. J. Queijo
Publisher:
ISBN:
Category :
Languages : en
Pages : 29
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Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 29
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Book Description
This report contains the results of wind-tunnel tests to determine the effect of dihedral on the static-stability and yawing derivatives of 45 degree sweptback-wing model of aspect ratio 2.61. The tests were made in the curved-flow test section of the Langley stability tunnel at a Reynolds number of approximately 1,100,000 and consisted of force measurements throughout the lift-coefficient range.
Author: Arthur Earl Bryson
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 340
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Author: John M. Riebe
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 32
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An investigation was made in the Langley 300 MPH 7- by 10-foot tunnel to determine the static stability characteristics of a cambered-delta-wing model. The cambered delta wing was derived from a segment of a cone selected so that the projected plan form with a wing dihedral angle of zero degrees was the same as a 60 degree delta wing. The projected plan form had an aspect ratio of 2.31.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 36
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Author: Kenneth P. Spreemann
Publisher:
ISBN:
Category :
Languages : en
Pages : 30
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