Author: Roger H. FournierPublisher:
ISBN:
Category :
Languages : en
Pages : 30
Book Description
Effects of Nose Bluntness on the Static Aerodynamic Characteristics of a Cruciform Wing Missile at Mach Numbers 1.50 to 2.86
Author: Roger H. FournierEffects of Nose Bluntness on Aerodynamic Characteristics of Cruciform-finned Missile Configuration at Mach 1.50 to 2.86
Author: Lloyd S. JernellEffects 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. ShawPublisher:
ISBN:
Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 88
Book Description
Effects of Nose Bluntness on Aerodynamic Characteristics of Cruciform-finned Missle Configuration at Mach 1.550 to 2.86
Author: Lloyd S. JernellSome Effects of Nose Bluntness and Fineness Ration on the Static Longitudinal Aerodynamic Characteristics of Bodies of Revolution at Bussonic Speeds
Author: William C. HayesPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 70
Book Description
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. MontaPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 36
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 RobinsPublisher:
ISBN:
Category : Rockets (Aeronautics)
Languages : en
Pages : 32
Book Description
Aerodynamic Characteristics in Pitch of a Series of Cruciform-wing Missiles with Canard Controls at a Mach Number of 2.01
Author: M. Leroy SpearmanPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 44
Book Description
Aerodynamic Characteristics at Mach Numbers from 1.50 to 4.63 of a Maneuverable Missile with In-line Cruciform Wings and Canard Surfaces
Author: M. Leroy SpearmanPublisher:
ISBN:
Category : Guided missiles
Languages : en
Pages : 52
Book Description
An investigation has been conducted in the Langley Unitary Plan wind tunnel at Mach numbers from 1.50 to 4.63 to determine the aerodynamic characteristics of a maneuverable missile having in-line cruciform wings and canard surfaces oriented in 45° roll planes.
Author: David S. Shaw