Author: A. Warner RobinsPublisher:
ISBN:
Category : Rockets (Aeronautics)
Languages : en
Pages : 32
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
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 RobinsLongitudinal Stability and Control Characteristics from a Flight Investigation of a Cruciform Canard Missile Configuration Having an Exposed Wing-canard Area Ratio of 16:1
Author: Martin T. MoulPublisher:
ISBN:
Category : Rockets (Aeronautics)
Languages : en
Pages : 42
Book Description
An Experimental Investigation of the Aerodynamic Characteristics of Several Nose-mounted Canard Configurations at Transonic Mach Numbers
Author: James R Burt (Jr.)Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 778
Book Description
Experimental aerodynamic investigations were conducted at the CALSPAN Corporation's transonic wind tunnel to determine the aerodynamic characteristics of several nose-mounted canard wing configurations. Canard position, geometry, angular orientation, and model nose shape were varied systematically to determine their effects on model aerodynamics. Angle of attack was varied from -3 to 12 degrees and Mach number was varied from 0.6 to 1.25. Aerodynamic loads were measured separately for each of the four canards and tail surfaces, and the total model.
Investigation of the Static Longitudinal Stability Characteristics of an Air-to-surface Canard Missile Configuration in the Transonic Mach Number Range
Author: Gerald L. HuntPublisher:
ISBN:
Category : Air-to-surface missiles
Languages : en
Pages : 24
Book Description
An Experimental Investigation of the Aerodynamic Characteristics of Nose Mounted Canard Configurations at Supersonic Mach Numbers (1.5 Through 4.5)
Author: James R Burt (Jr.)Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 352
Book Description
Experimental aerodynamic investigations were conducted in a supersonic wind tunnel to determine the aerodynamic characteristics of several nose mounted canard wing configurations. Canard position, geometry, angular orientation, and model nose shape were varied systematically to determine their effects on model aerodynamics. The model was tested at angles of attack of -5 to 13 degrees and Mach numbers of 1.5 to 4.5. Aerodynamic loads were measured separately on four canards and tail panels, and the total model. The vapor screen method was used to trace the paths of the vortices shed from the canards. Roll control effectiveness of canards, both with a planar tail and a ring tail was investigated.
Investigation of the Static Longitudinal Stability and Roll Characteristics of a Three-stage Missile Configuration at Mach Numbers from 1.77 to 2.87
Author: Donald T. GregoryPublisher:
ISBN:
Category : Stability of airplanes, Longitudinal
Languages : en
Pages : 36
Book Description
Longitudinal Stability and Control Characteristics of a Canard Missile Configuration for Mach Numbers from 1.1 to 1.93 as Determined from Free-flight and Wind-tunnel Investigations
Author: Howard J. Jr CurfmanEffects of Nose Bluntness on Aerodynamic Characteristics of Cruciform-finned Missile Configuration at Mach 1.50 to 2.86
Author: Lloyd S. JernellAerodynamic 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