Longitudinal Stability and Control Characteristics from a Flight Investigation of a Cruciform Canard Missile Configuration Having an Exposed Wing-canard Area Ratio of 16:1 PDF Download

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Longitudinal Stability and Control Characteristics from a Flight Investigation of a Cruciform Canard Missile Configuration Having an Exposed Wing-canard Area Ratio of 16:1

Longitudinal Stability and Control Characteristics from a Flight Investigation of a Cruciform Canard Missile Configuration Having an Exposed Wing-canard Area Ratio of 16:1 PDF Author: Martin T. Moul
Publisher:
ISBN:
Category : Rockets (Aeronautics)
Languages : en
Pages : 42

Book Description

Longitudinal Stability and Control Characteristics from a Flight Investigation of a Cruciform Canard Missile Configuration Having an Exposed Wing-canard Area Ratio of 16:1

Longitudinal Stability and Control Characteristics from a Flight Investigation of a Cruciform Canard Missile Configuration Having an Exposed Wing-canard Area Ratio of 16:1 PDF Author: Martin T. Moul
Publisher:
ISBN:
Category : Rockets (Aeronautics)
Languages : en
Pages : 42

Book Description

Flight Investigation at Low Angles of Attack to Determine the Longitudinal Stability and Control Characteristics of a Cruciform Canard Missile Configuration with a Low-aspect-ratio Wing and Blunt Nose at Mach Numbers from 1.2 to 2.1

Flight Investigation at Low Angles of Attack to Determine the Longitudinal Stability and Control Characteristics of a Cruciform Canard Missile Configuration with a Low-aspect-ratio Wing and Blunt Nose at Mach Numbers from 1.2 to 2.1 PDF Author: Clarence A. Brown
Publisher:
ISBN:
Category : Charts, diagrams, etc
Languages : en
Pages : 37

Book Description
A full-scale rocket-powered model of a cruciform canard missile configuration with a low-aspect ratio wing and blunt nose has been flight tested by the Langley Pilotless Aircraft Research Division. Static and dynamic longitudinal stability and control derivatives of this interdigitated canard-wing missile configuration were determined by using the pulsed-control technique at low angles of attack and for a Mach number range of 1.2 to 2.1.

The Longitudinal Stability, Control Effectiveness, and Control Hinge-moment Characteristics Obtained from a Flight Investigation of a Canard Missile Configuration at Transonic and Supersonic Speeds

The Longitudinal Stability, Control Effectiveness, and Control Hinge-moment Characteristics Obtained from a Flight Investigation of a Canard Missile Configuration at Transonic and Supersonic Speeds PDF Author: Roy J. Niewald
Publisher:
ISBN:
Category :
Languages : en
Pages : 42

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

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 PDF Author: Howard J. Jr Curfman
Publisher:
ISBN:
Category :
Languages : en
Pages : 28

Book Description

Investigation of the Static Longitudinal Stability Characteristics of an Air-to-surface Canard Missile Configuration in the Transonic Mach Number Range

Investigation of the Static Longitudinal Stability Characteristics of an Air-to-surface Canard Missile Configuration in the Transonic Mach Number Range PDF Author: Gerald L. Hunt
Publisher:
ISBN:
Category : Air-to-surface missiles
Languages : en
Pages : 24

Book Description

Longitudinal Aerodynamic Characteristics at Mach 1.50 to 4.63 of a Missile Model Employing Various Canards and a Trailing Edge Flap Control

Longitudinal Aerodynamic Characteristics at Mach 1.50 to 4.63 of a Missile Model Employing Various Canards and a Trailing Edge Flap Control PDF Author: Charles D. Jr Trescot
Publisher:
ISBN:
Category :
Languages : en
Pages : 124

Book Description

Effect of Tail-fin Span on Stability and Control Characteristics of a Canard-controlled Missile at Supersonic Mach Numbers

Effect of Tail-fin Span on Stability and Control Characteristics of a Canard-controlled Missile at Supersonic Mach Numbers PDF Author: A. B. Jr Blair
Publisher:
ISBN:
Category :
Languages : en
Pages : 92

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

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 PDF Author: A. Warner Robins
Publisher:
ISBN:
Category : Rockets (Aeronautics)
Languages : en
Pages : 32

Book Description

An Investigation of the Subsonic Longitudinal Stability and Control Characteristics of a Canard Configuration with a Free-flying Horizontal Stabilizer

An Investigation of the Subsonic Longitudinal Stability and Control Characteristics of a Canard Configuration with a Free-flying Horizontal Stabilizer PDF Author: Daniel Bright
Publisher:
ISBN:
Category :
Languages : en
Pages : 87

Book Description

Effect on Tail-fin Span on Stability and Control Characteristics of a Canard-controlled Missile at Supersonic Mach Numbers

Effect on Tail-fin Span on Stability and Control Characteristics of a Canard-controlled Missile at Supersonic Mach Numbers PDF Author: A. B. Blair
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 92

Book Description

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