Author: Rodger L. Naeseth
Publisher:
ISBN:
Category :
Languages : en
Pages : 44
Book Description
Lateral Control Characteristics of Two Structurally Similar Flexible Wings with 45 Degree Sweep
Author: Rodger L. Naeseth
Publisher:
ISBN:
Category :
Languages : en
Pages : 44
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 44
Book Description
LATERAL CONTROL CHARACTERISTICS OF TWO STRUCTURALLY SIMILAR FLEXIBLE WINGS WITH 45 Deg SWEEP: A SWEPTBACK WING AND A WING WITH M PLAN FORM.
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 53
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 53
Book Description
Lateral Control Characteristics of Two Structural Similar Flexible Wings with 45 Degrees Sweep: a Sweptback Wing and a Wing with M Plan Form
Author: Rodger L. Naeseth
Publisher:
ISBN:
Category : Ailerons
Languages : en
Pages : 44
Book Description
A low-speed wind-tunnel investigation was made to determine the static lateral control characteristics of flap-type and retractable spoiler-type ailerons on a rigid sweptback wing, a flexible sweptback wing, and a flexible M-wing. A few tests were also made with a half-delta tip control on the flexible sweptback wing. The semispan wing models were of aspect ratio 6.0, taper ratio of 0.6, and had NACA 65A009 airfoil sections parallel to the free-stream direction. The quarter-chord lines of the wings were swept 45 degrees and the break in the M-wing was at the half semispan location.
Publisher:
ISBN:
Category : Ailerons
Languages : en
Pages : 44
Book Description
A low-speed wind-tunnel investigation was made to determine the static lateral control characteristics of flap-type and retractable spoiler-type ailerons on a rigid sweptback wing, a flexible sweptback wing, and a flexible M-wing. A few tests were also made with a half-delta tip control on the flexible sweptback wing. The semispan wing models were of aspect ratio 6.0, taper ratio of 0.6, and had NACA 65A009 airfoil sections parallel to the free-stream direction. The quarter-chord lines of the wings were swept 45 degrees and the break in the M-wing was at the half semispan location.
Subject Index to Unclassified ASTIA Documents
Author: Defense Documentation Center (U.S.)
Publisher:
ISBN:
Category : Industrial arts
Languages : en
Pages : 906
Book Description
Publisher:
ISBN:
Category : Industrial arts
Languages : en
Pages : 906
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1006
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1006
Book Description
Aerodynamic Characteristics in Pitch of Three Structurally Similar Flexible Wings with 45 Degree Sweep
Author: John W. Mckee
Publisher:
ISBN:
Category :
Languages : en
Pages : 43
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 43
Book Description
STAR
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 920
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 920
Book Description
Aerospace Engineering Index
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 782
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 782
Book Description
Applied Mechanics Reviews
Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 1196
Book Description
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 1196
Book Description
Aeronautical Engineering Index
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 258
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 258
Book Description