Effect of Geometric Dihedral on Low-speed Static Stability Characteristics of a 40 Degree Swept-back Wing PDF Download
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Author: Kazimierz Orlik-Ruckemann
Publisher:
ISBN:
Category :
Languages : en
Pages : 18
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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
Get Book Here
Book Description
Author: Kazimierz J. Orlik-Rückemann
Publisher:
ISBN:
Category :
Languages : en
Pages : 18
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Book Description
Author: K. Orlik-Rückemann
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Author: John M. Riebe
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 32
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Book Description
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:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 29
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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: Donald E. Hewes
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 36
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Book Description
The trends in lateral stability and control produced variations of the mass distribution were determined for a model with a 45 degree sweptback wing. Calculations were made to correlate the trends determined by theory with those determined from tests of a free-flying dynamic model in the Langley free-flight tunnel.
Author: Clarence L. Gillis
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 48
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A test and analysis method is presented for determining airplane lateral stability characteristics, including aerodynamic derivatives, from flight tests of scale models. The method of analysis utilizes the rotating time-vector concept and also a quasi-static approach. Data are presented at transonic speeds for three swept-wing rocket-propelled models differing only in vertical position and dihedral of the wing. The method proved to be adequate for delineating the major effects of the geometric variations on the aerodynamic lateral stability derivatives. The effects of Reynolds number on the linearity of the static stability data for an unswept wing configuration are illustrated.
Author: Albert G. Few
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 80
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Book Description
The drag due to lift increases with increasing sweep through the Mach number range. Some increase in bag due to lift is evident decrease in taper ratio for wings having 300of sweep through most of the speed range.
Author: Kenneth P. Spreemann
Publisher:
ISBN:
Category :
Languages : en
Pages : 30
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Book Description
