Author: Emma Jean Landrum
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 24
Book Description
Effect of Shape Changes on the Aerodynamic Characteristics of a Twisted and Cambered Arrow Wing at Mach Number 2.03
Author: Emma Jean Landrum
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 24
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 24
Book Description
Effects of Shape Changes on the Aerodynamic Characteristics of a Twisted and Cambared Arrow Wing at Mach Number 2.03
Longitudinal Aerodynamic Characteristics at Mach Number 2.02 of a Series of Wing-body Configurations Employing a Cambered and Twisted Arrow Wing
Effects of Twist and Camber and Thickness on the Aerodynamic Characteristics of a 75° Swept Arrow Wing at a Mach Number of 2.91
Author: James N. Mueller
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 72
Book Description
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 72
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
Aerodynamic Characteristics at Mach Numbers from 1.6 to 2.8 of 740 Swept Arrow Wings with and Without Camber and Twist
Author: Dennis F. Hasson
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 42
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 42
Book Description
Off-design Aerodynamic Characteristics at Mach Numbers 1.61 and 2.20 of a Series of Highly Swept Arrow Wings Designed for Mach Number 2.0 Employing Various Degrees of Twist and Camber
Author: Wilbur D. Middleton
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 32
Book Description
Aerodynamic Characteristics at Mach Numbers from 2.29 to 4.65 of 80 Deg Swept Arrow Wings with and Without Camber and Twist
Aerodynamic Characteristics at Mach Number 2.05 of a Series of Highly Swept Arrow Wings Employing Various Degrees of Twist and Camber
Author: Harry W. Carlson
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 38
Book Description
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 38
Book Description