Author: George H. Holdaway
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 70
Book Description
Evaluation of Blended Wing-body Combinations with Curved Plan Forms at Mach Numbers Up to 3.50
Author: George H. Holdaway
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 70
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 70
Book Description
Evaluation of Blended Wing-body Combinations with Curved Plan Forms at Mach Numbers Up to 3.50 [with List of References]
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 66
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 66
Book Description
Investigation at Mach Numbers of 0.20 to 3.50 of Blended Wing-body Combinations of Sonic Design with Diamond, Delta and Arrow Plan Forms
Author: George H. Holdaway
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 82
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 82
Book Description
Investigation at Mach Numbers of 0.60 to 3.50 of Blended Wing-body Combinations with Cambered and Twisted Wings with Diamond, Delta and Arrow Plan Forms
Author: George H. Holdaway
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 82
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 82
Book Description
Investigation at Mach Numbers of 0.20 to 3.50 of Blended Wing-body Combinations of Sonic Design with Diamond, Delta, and Arrow Plan Forms [with List of References]
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 77
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 77
Book Description
Investigation at Mach Numbers of 0.06 to 3.50 of Blended Wing Body Combinations with Cambered and Twisted Wing with Diamond, Delta and Arrow Plan Forms
Author: George H. Holdaway
Publisher:
ISBN:
Category :
Languages : en
Pages : 76
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 76
Book Description
Investigation at Mach Numbers of 0.60 to 3.50 of Blended Wing-body Combinations with Cambered and Twisted Wings with Diamond, Delta and Arrow Plan Forms [with List of References]
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 76
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 76
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
Investigation at Mach Numbers of 0.20 to 3.50 of a Blended Diamond Wing and Body Combination of Sonic Design But with Low Wave-drag Increase with Increasing Mach Number
Author: George H. Holdaway
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 62
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 62
Book Description
The Flow Past a Straight- and a Swept-wing-body Combination and Their Equivalent Bodies of Revolution at Mach Numbers Near 1.0
Author: W. F. Lindsey
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 24
Book Description
Abstract: The complete flow fields past a straight and a swept wing-body combination and their equivalent bodies of revolution at Mach numbers around 1.0 have been observed by means of motion-picture schlieren photography. The results of these observations indicate that the shock growth and positions on the wing-body combinations are closely reproduced in the flow past their respective equivalent bodies.
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 24
Book Description
Abstract: The complete flow fields past a straight and a swept wing-body combination and their equivalent bodies of revolution at Mach numbers around 1.0 have been observed by means of motion-picture schlieren photography. The results of these observations indicate that the shock growth and positions on the wing-body combinations are closely reproduced in the flow past their respective equivalent bodies.