Low-speed Pressure Distributions Over the Drooped-nose Flap of a 42 Degree Sweptback Wing with Circular-arc Airfoil Sections at a Reynolds Number of 5.3 X (10)6

Low-speed Pressure Distributions Over the Drooped-nose Flap of a 42 Degree Sweptback Wing with Circular-arc Airfoil Sections at a Reynolds Number of 5.3 X (10)6 PDF Author: Stanley H. Spooner
Publisher:
ISBN:
Category :
Languages : en
Pages : 28

Get Book Here

Book Description


Effects 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

Effects 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 PDF Author: George L. Pratt
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 110

Get Book Here

Book Description


Investigation at Large Scale of the Pressure Distribution and Flow Phenomena Over a Wing with the Leading Edge Swept Back 47.5 Degrees Having Circular-arc Airfoil Sections and Equipped with Drooped-nose and Plain Flaps

Investigation at Large Scale of the Pressure Distribution and Flow Phenomena Over a Wing with the Leading Edge Swept Back 47.5 Degrees Having Circular-arc Airfoil Sections and Equipped with Drooped-nose and Plain Flaps PDF Author: Roy H. Lange
Publisher:
ISBN:
Category :
Languages : en
Pages : 72

Get Book Here

Book Description


Low-speed Characteristics in Pitch of a 340 Sweptforward Wing with Circular-arc Airfoil Sections

Low-speed Characteristics in Pitch of a 340 Sweptforward Wing with Circular-arc Airfoil Sections PDF Author: D. William Conner
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 70

Get Book Here

Book Description


Pressure Distributions and Aerodynamic Characteristics of Several Spoiler Controls on a 40 Degree Sweptback Wing at a Mach Number of 1.61

Pressure Distributions and Aerodynamic Characteristics of Several Spoiler Controls on a 40 Degree Sweptback Wing at a Mach Number of 1.61 PDF Author: Emma Jean Landrum
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 70

Get Book Here

Book Description


Effects of High-lift and Stall-control Devices, Fuselage, and Horizontal Tail on a Wing Swept Back 42 Degrees at the Leading Edge and Having Symmetrical Circular-arc Airfoil Sections at a Reynolds Number of 6.9 X (10)6

Effects of High-lift and Stall-control Devices, Fuselage, and Horizontal Tail on a Wing Swept Back 42 Degrees at the Leading Edge and Having Symmetrical Circular-arc Airfoil Sections at a Reynolds Number of 6.9 X (10)6 PDF Author: Robert L. Woods
Publisher:
ISBN:
Category :
Languages : en
Pages : 42

Get Book Here

Book Description


Studies of the Flow Field Behind a Large Scale 47.5 Degree Sweptback Wing Having Circular-arc Airfoil Sections and Equipped with Drooped-nose and Plain Flaps

Studies of the Flow Field Behind a Large Scale 47.5 Degree Sweptback Wing Having Circular-arc Airfoil Sections and Equipped with Drooped-nose and Plain Flaps PDF Author: Roy H. Lange
Publisher:
ISBN:
Category :
Languages : en
Pages : 57

Get Book Here

Book Description


Effect of Reynolds Number on the Lateral-stability Derivatives at Low Speed of Swept-back and Delta-wing-fuselage Combinations Oscillating in Yaw

Effect of Reynolds Number on the Lateral-stability Derivatives at Low Speed of Swept-back and Delta-wing-fuselage Combinations Oscillating in Yaw PDF Author: Charles P. Llewellyn
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 50

Get Book Here

Book Description
An investigation has been made to determine the effect of Reynolds number on the lateral-stability derivatives at low speed of sweptback- and delta-wing-fuselage combinations. Results were obtained from the models oscillating in yaw over an angle-of-attack ...

Low-Speed Characteristics in Pitch of a 42 Degree Swept-Back Wing with Aspect Ratio 3.9 and Circular-Arc Airfoil Sections

Low-Speed Characteristics in Pitch of a 42 Degree Swept-Back Wing with Aspect Ratio 3.9 and Circular-Arc Airfoil Sections PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 57

Get Book Here

Book Description


Low-speed Characteristics in Pitch of a 42 Degrees Sweptback Wing with Aspect Ratio 3.9 and Circular-arc Airfoil Sections

Low-speed Characteristics in Pitch of a 42 Degrees Sweptback Wing with Aspect Ratio 3.9 and Circular-arc Airfoil Sections PDF Author: Robert H. Neely
Publisher:
ISBN:
Category :
Languages : en
Pages : 42

Get Book Here

Book Description