Author: Edward F. Jr WhittlePublisher:
ISBN:
Category :
Languages : en
Pages : 51
Book Description
Effect on the Low-speed Aerodynamic Characteristics of a 49 Degree Sweptback Wing Having an Aspect Ratio of 3.78 of Blowing Air Over the Trailing-edge Flap and Aileron
Author: Edward F. Jr WhittleEffect on the Low-speed Aerodynamic Characteristics of a 49 Degrees Sweptback Wing Having an Aspect Ratio of 3.78 of Blowing Air Over the Trailing-edge Flap and Aileron
Author: Jr. Edward F. WhittleEffect on the Low-speed Aerodynamic Characteristics of a 49° Sweptback Wing Having an Aspect Ratio of 3.78 of Blowing Air Over the Trailing-edge Flap and Aileron
Author: Edward F. WhittlePublisher:
ISBN:
Category : Ailerons
Languages : en
Pages : 0
Book Description
Effect on the Low-speed Aerodynamic Characteristics of a 49° Sweptback Wing Having an Aspect Ratio of 3.78 of Blowing Air Over the Trailing-edge Flap and Aileron
Author: Edward F. WhittlePublisher:
ISBN:
Category : Ailerons
Languages : en
Pages : 51
Book Description
Aerodynamic Characteristics of Low-aspect-ratio Wings in Close Proximity to the Ground
Author: Marvin P. FinkEffects of Twist and Camber on the Low-speed Longitudinal Stability Characteristics of a 45© Swept-back Wing of Aspect Ratio 8 at Reynolds Numbers from 1.5 X 106 to 4.8 X 10 as Determined by Pressure Distributions, Force Tests, and Calculations
Author: George L. PrattPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 110
Book Description
Aerodynamic Characteristics in Sideslip of a Large-scale 49 Degree Sweptback Wing-body-tail Configuration with Blowing Applied Over the Flaps and Wing Leading Edge
Author: H. Clyde McLemoreLow-speed Aerodynamic Characteristics of a Large-scale 45 Degree Swept-back Wing with Partial-span Slats, Double-slotted Flaps, and Ailerons
Author: Harry A. JamesWind-tunnel Investigation at Low Speed of the Effect of Varying the Ratio of Body Diameter to Wing Span from 0.1 to 0.8 on the Aerodynamic Characteristics in Pitch of the 45© Sweptback-wing--body Combination
Author: Harold S. JohnsonPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 36
Book Description
Investigation of Transonic Flutter Characteristics of a Thin 10 Degree Sweptback Wing Having an Aspect Ratio of 4 and a Taper Ratio of 0.6
Author: George W. JonesPublisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 22
Book Description
A flutter investigation has been made in the Langley transonic blowdown tunnel at Mach numbers between 0.79 and 1.34 on a thin 10 degree sweptback wing having an aspect ratio of 4 and a taper ratio of 0.6. The data obtained have been compared with data from NACA Research Memorandum L55I13A for zero and 30 degree sweptback wings of the type investigated, the flutter boundary for the 10 degree sweptback wing falls between those for the zero degree and 30 degree sweptback wings in the low supersonic Mach number range. However, the subsonic level (around a Mach number of 0.8) of the flutter boundary for the 10 degree sweptback wing lies above those for the zero and 30 degree sweptback wings. In addition, the amount of rise in the flutter boundary from the subsonic level to the supersonic values is about the same for the wings with angles of sweepback of 10 degrees and zero degrees, but is much greater for the wing with an angle of sweepback of 30 degrees.