Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 34
Book Description
Aerodynamic Characteristics at Mach Number 2.05 of Series of Highly Swept Arrow Wings Employing Various Degrees of Twist and Camber [with List of References]
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
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
Pressure Distributions at Mach Number 2.05 on a Series of Highly Swept Arrow Wings Employing Various Degrees of Twist and Camber
Author: Harry W. Carlson
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 44
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 44
Book Description
Longitudinal Aerodynamic Characteristics at Mach Number 2.02 of a Series of Wing-body Configurations Employing a Cambered and Twisted Arrow Wing
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
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 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
Pressure Distributions at Mach Number 2.05 on a Series of Highly Swept Arrow Wings Employing Various Degrees of Twist and Camber /by Harry W. Carlson
Aerodynamic Characteristics at Mach Numbers from 1.6 to 2.8 of 74° Swept Arrow Wings with and Without Camber and Twist [with List of References]
Author: Dennis F. Hasson
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 38
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 38
Book Description