Low-speed Static Stability Characteristics of a Cambered-delta-wing Model PDF Download
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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: 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: William C. Moseley
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 35
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Book Description
An investigation at high subsonic speeds was made in the Langley high-speed 7- by 10-foot tunnel to determine the static stability characteristics of a cambered-delta-wing model with wing dihedral angles of 20 to 50 degrees. The cambered delta wing was selected so that the projected plan form with a wing dihedral angle of zero degrees was the same as that of a 60 degree delta wing.
Author: Alex Goodman
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 82
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Book Description
An investigation was made to determine the effects of wing position and fuselage size on the low-speed static and rolling stability characterististics of airplane models having a triangular wing and vertical tail surfaces.
Author: Alex Goddman
Publisher:
ISBN:
Category :
Languages : en
Pages : 31
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Book Description
Author: Kenneth P. Spreemann
Publisher:
ISBN:
Category :
Languages : en
Pages : 30
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 382
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 750
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Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 806
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Book Description
Author: Joseph L. Johnson
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 19
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Book Description
A low-speed investigation has been conducted to determine the static longitudinal and lateral stability characteristics and the damping in yaw and damping in roll of a 60 degree delta wing, a 45 degree swept wing of aspect ratio 2.61, and an unswept wing of aspect ratio 3 over an angle-of-attack range from 0 to 90 degrees.
Author: William I. Scallion
Publisher:
ISBN:
Category : Delta wing airplanes
Languages : en
Pages : 64
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Book Description
