Author: Robert W. Dunning
Publisher:
ISBN:
Category :
Languages : en
Pages : 26
Book Description
Aerodynamic Characteristics at Mach Number 4.04 of a Rectangular Wing of Aspect Ratio 1.33 Having a 6-percent-thick Circular-arc Profile and a 30-percent-chord Full-span Trailing-edge Flap
Author: Robert W. Dunning
Publisher:
ISBN:
Category :
Languages : en
Pages : 26
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 26
Book Description
Aerodynamic Characteristics of a Wing with Quarter-chord Line Swept Back 35©, Aspect Ratio 6, Taper Ratio 0.6, and NACA 65A006 Airfoil Section
Author: William C. Sleeman
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 36
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 36
Book Description
Aerodynamic Characteristics of Two Delta Wings and Two Trapezoidal Wings at Mach Number of 4.04
Author: Robert W. Dunning
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 24
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 24
Book Description
Aerodynamic Characteristics at Mach Numbers of 1.41 and 2.01 of a Series of Cranked Wings Ranging in Aspect Ratio from 4.00 to 1.74 in Combination with a Body
Author: John R. Sevier
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 44
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 44
Book Description
Aerodynamic Characteristics of Several Cranked Leading-edge Wing-body Combinations at Mach Numbers from 0.4 to 2.94
Author: Edward J. Hopkins
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 98
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 98
Book Description
Aerodynamic Characteristics of a 60° Sweptback-wing Airplane Configuration Having Tail Surfaces Located Outboard of the Wingtips at Mach Numbers of 2.30, 2.97, 3.51, and 4.06
Author: Sleeman, Jr. (William C.)
Publisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 56
Book Description
Publisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 56
Book Description
The Aerodynamic Characteristics of Several Thick Delta Wings at Mach Numbers to 6 and Angles of Attack 50°
Author: John B. McDevitt
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 114
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 114
Book Description
A Note on the Drag Due to Lift of Delta Wings at Mach Numbers Up to 2.0
Author: Robert S. Osborne
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 20
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 20
Book Description
Aerodynamic Characteristics of a 60 Degree Sweptback-wing Airplane Configuration Having Tail Surfaces Located Outboard of the Wing Tips at Mach Numbers of 2.30, 2.97, 3.51, and 4.06
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 54
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 54
Book Description
Effects at Mach Numbers of 1.61 and 2.01 of Camber and Twist on the Aerodynamic Characteristics of Three Swept Wings Having the Same Planform
Author: Emma Jean Landrum
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 52
Book Description
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 52
Book Description