Author: Charles F. Whitcomb
Publisher:
ISBN:
Category :
Languages : en
Pages : 286
Book Description
An Investigation of Wing and Aileron Loads Due to Deflected Inboard and Outboard Ailerons on a 4-percent-thick 30 Degree Swepptback Wing at Transonic Speeds
An Investigation of Wing and Aileron Loads Due to Deflected Inboard and Outboard Ailerons on a 4-percent-thick 30 Degree Swepptback Wing at Transonic Speeds
An Investigation of Wing and Aileron Loads Due to Deflected Inboard and Outboard Ailerons on a 4-Percent-Thick 30 Deg Sweptback Wing at Transonic Speeds
An Investigation of Wing and Aileron Loads Due to Deflected Inboard and Outboard Ailerons on a 4-percent-thick 30° Sweptback Wing at Transonic Speeds
An Investigation of Wing and Alleron Loads Due to Deflected Inboard and Outboard Ailerons on a 4-percent-thick 30 Degrees Sweptback Wing at Transonic Speeds
Normal-force and Hinge-moment Characteristics at Transonic Speeds of Flap-type Ailerons at Three Spanwise Locations on a 4-percent-thick Sweptback-wing-body Model and Pressure-distribution Measurements on an Inboard Aileron
Author: Jack F. Runckel
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 60
Book Description
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 60
Book Description
A Wind-tunnel Investigation of the Wing Loads Due to Deflected Inboard Ailerons on a 45 Degree Sweptback Wing at Transonic Speeds
Loads on Wings Due to Spoilers at Subsonic and Transonic Speeds
Author: Alexander D. Hammond
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 18
Book Description
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 18
Book Description
Loads on Thin Wings at Transonic Speeds
Author: Don D. Davis (Jr.)
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 22
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 22
Book Description
Investigation at Transonic Speeds of the Loading Over a 45 Degree Sweptback Wing Having an Aspect Ratio of 3, a Taper Ratio of 0.2, and NACA 65A004 Airfoil Sections
Author: Jack F. Runckel
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 104
Book Description
An investigation at transonic speeds of the loading over a 45 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2, and NACA 65A004 airfoil sections has been conducted in the Langley16-foot transonic tunnel. Pressure measurements on the wing-body combination were obtained at angles of attack from 0 to 26 degrees at Mach numbers from 0.80 to 0.98 and from 0 to about 12 degrees at Mach numbers from 1.00 to 1.05. Reynolds number, based on the wing mean aerodynamic chord, varied from 7,000,000 to 8,500,000 over the test Mach number range.
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 104
Book Description
An investigation at transonic speeds of the loading over a 45 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2, and NACA 65A004 airfoil sections has been conducted in the Langley16-foot transonic tunnel. Pressure measurements on the wing-body combination were obtained at angles of attack from 0 to 26 degrees at Mach numbers from 0.80 to 0.98 and from 0 to about 12 degrees at Mach numbers from 1.00 to 1.05. Reynolds number, based on the wing mean aerodynamic chord, varied from 7,000,000 to 8,500,000 over the test Mach number range.