Wind-tunnel Investigation at Mach Numbers from 1.90 to 2.86 of a Canard-controlled Missile with Ram-air-jet Spoiler Roll Control PDF Download

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Wind-tunnel Investigation at Mach Numbers from 1.90 to 2.86 of a Canard-controlled Missile with Ram-air-jet Spoiler Roll Control

Wind-tunnel Investigation at Mach Numbers from 1.90 to 2.86 of a Canard-controlled Missile with Ram-air-jet Spoiler Roll Control PDF Author: A. B. Blair
Publisher:
ISBN:
Category :
Languages : en
Pages : 106

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Book Description

Wind-tunnel Investigation at Mach Numbers from 1.90 to 2.86 of a Canard-controlled Missile with Ram-air-jet Spoiler Roll Control

Wind-tunnel Investigation at Mach Numbers from 1.90 to 2.86 of a Canard-controlled Missile with Ram-air-jet Spoiler Roll Control PDF Author: A. B. Blair
Publisher:
ISBN:
Category :
Languages : en
Pages : 106

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Book Description

Wind-tunnel Investigations at Mach Numbers from 1.90 to 2.86 of a Canard-controlled Missile with Ram-air-jet Spoiler Roll Control

Wind-tunnel Investigations at Mach Numbers from 1.90 to 2.86 of a Canard-controlled Missile with Ram-air-jet Spoiler Roll Control PDF Author: A. B. Blair
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 101

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Book Description

Free-flight Investigation at Mach Numbers Between 0.5 and 1.7 of the Zero-lift Rolling Effectiveness and Drag of Various Surface, Spoiler, and Jet Controls on an 80° Delta-wing Missile

Free-flight Investigation at Mach Numbers Between 0.5 and 1.7 of the Zero-lift Rolling Effectiveness and Drag of Various Surface, Spoiler, and Jet Controls on an 80° Delta-wing Missile PDF Author: Eugene D. Schult
Publisher:
ISBN:
Category : Mach number
Languages : en
Pages : 58

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Book Description

Wind-tunnel Investigation of a Ram-jet Canard Missile Model Having a Wing and Canard Surfaces of Delta Plan Form with 70 Degree Swept Leading Edges - Longitudinal and Lateral Stability and Control Characteristics at a Mach Number of 1.60

Wind-tunnel Investigation of a Ram-jet Canard Missile Model Having a Wing and Canard Surfaces of Delta Plan Form with 70 Degree Swept Leading Edges - Longitudinal and Lateral Stability and Control Characteristics at a Mach Number of 1.60 PDF Author: M. Leroy Spearman
Publisher:
ISBN:
Category :
Languages : en
Pages : 63

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Book Description

Wind-tunnel Investigation at Supersonic Speeds of a Remote-controlled Canard Missile with a Free-rolling-tail Brake Torque System

Wind-tunnel Investigation at Supersonic Speeds of a Remote-controlled Canard Missile with a Free-rolling-tail Brake Torque System PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 44

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Book Description

An Experimental Wind-tunnel Investigation of a Ram-air-spoiler Roll-control Device on a Forward-control Missile at Supersonic Speeds

An Experimental Wind-tunnel Investigation of a Ram-air-spoiler Roll-control Device on a Forward-control Missile at Supersonic Speeds PDF Author: A. B. Blair (Jr)
Publisher:
ISBN:
Category :
Languages : en
Pages : 196

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Book Description

Wind-tunnel Investigation at Mach Numbers of 1.5 and 2.0 of a Canard Missile Configuration

Wind-tunnel Investigation at Mach Numbers of 1.5 and 2.0 of a Canard Missile Configuration PDF Author: J. Richard Spahr
Publisher:
ISBN:
Category :
Languages : en
Pages : 47

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Book Description

Wind-tunnel Investigation at Supersonic Speeds of a Canard-controlled Missile with Fixed and Free-rolling Tail Fins

Wind-tunnel Investigation at Supersonic Speeds of a Canard-controlled Missile with Fixed and Free-rolling Tail Fins PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 84

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Book Description

Wind-tunnel Investigation of a Ram-jet Canard Missile Model Having a Wing and Canard Surfaces of Delta Plan Form with 70° Swept Leading Edges

Wind-tunnel Investigation of a Ram-jet Canard Missile Model Having a Wing and Canard Surfaces of Delta Plan Form with 70° Swept Leading Edges PDF Author: M. Leroy Spearman
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 63

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Book Description

Wind-tunnel Investigation of a Ram-jet Model Having a Wing and Canard Surfaces of Delta Plan Form with 70 Degrees Swept Leading Edges

Wind-tunnel Investigation of a Ram-jet Model Having a Wing and Canard Surfaces of Delta Plan Form with 70 Degrees Swept Leading Edges PDF Author: Cornelius Driver
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 67

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Book Description
An investigation has been conducted in the Langley 4- by 4-foot supersonic pressure tunnel to determine the static stability and control characteristics of a ram-jet canard missile at a Mach number of 2.01. The missile had wings and canard surfaces of delta plan form with 70 degree swept leading edges. Two ram-jet nacelles were mounted in the vertical plane on unswept pylons near the rear of the body. The center of gravity of the model was at -19.5 percent of the wing mean aerodynamic chord. Force characteristics of the missile configuration and various combinations of its components were determined through an incidence angle range from -2 to about 26 degrees and at various roll angles from 0 to -90 degrees. The Reynolds number of the investigation was 3,470,000 based on the wing mean aerodynamic chord.