Author: Lloyd S. Jernell
Publisher:
ISBN:
Category :
Languages : en
Pages : 36
Book Description
Effects of Nose Bluntness on Aerodynamic Characteristics of Cruciform-finned Missile Configuration at Mach 1.50 to 2.86
Effects of Nose Bluntness on Aerodynamic Characteristics of Cruciform-finned Missle Configuration at Mach 1.550 to 2.86
Aerodynamic Characteristics at Mach Numbers from 1.60 to 2.16 of a Blunt-nose Missile Model Having a Triangular Cross Section and Fixed Triform Fins
Author: William J. Monta
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 36
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 36
Book Description
Effects of Nose Bluntness on the Static Aerodynamic Characteristics of a Cruciform Wing Missile at Mach Numbers 1.50 to 2.86
Effects of Nose Bluntness, Fineness Ratio, Cone Angle, and Model Base on the Static Aerodynamic Characteristics of Blunt Bodies at Mach Numbers of 1.57, 1.80, and 2.16 and Angles of Attack Up to 180 ̊
Author: David S. Shaw
Publisher:
ISBN:
Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 88
Book Description
Publisher:
ISBN:
Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 88
Book Description
Preliminary Investigation of the Effects of Several Seeker-nose Configurations on the Longitudinal Characteristics of a Canard-type Missile at a Mach Number of 1.60
Author: A. Warner Robins
Publisher:
ISBN:
Category : Rockets (Aeronautics)
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category : Rockets (Aeronautics)
Languages : en
Pages : 32
Book Description
Effect of Nose Bluntness and Afterbody Shape on Aerodynamic Characteristics of a Monoplanar Missile Concept with Bodies of Circular and Elliptical Cross Sections at a Mach Number of 2.50
Author: Ernald B. Graves
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 100
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 100
Book Description