Static Stability and Drag Characteristics of the HAST Missile at Mach Numbers 2.25, 3.0, and 4.0 PDF Download

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Static Stability and Drag Characteristics of the HAST Missile at Mach Numbers 2.25, 3.0, and 4.0

Static Stability and Drag Characteristics of the HAST Missile at Mach Numbers 2.25, 3.0, and 4.0 PDF Author: J. T. Best (Jr.)
Publisher:
ISBN:
Category : Drag (Aerodynamics)
Languages : en
Pages : 194

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Book Description
Static-force tests were conducted at Mach number 2.25, 3, and 4 on a 0.25 -scale model of the High Altitude Supersonic Target (HAST) missile.

Static Stability and Drag Characteristics of the HAST Missile at Mach Numbers 2.25, 3.0, and 4.0

Static Stability and Drag Characteristics of the HAST Missile at Mach Numbers 2.25, 3.0, and 4.0 PDF Author: J. T. Best (Jr.)
Publisher:
ISBN:
Category : Drag (Aerodynamics)
Languages : en
Pages : 194

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Book Description
Static-force tests were conducted at Mach number 2.25, 3, and 4 on a 0.25 -scale model of the High Altitude Supersonic Target (HAST) missile.

Static Stability and Drag Characteristics of the HAST Missile at Mach Numbers 2.25, 3.0, and 4.0

Static Stability and Drag Characteristics of the HAST Missile at Mach Numbers 2.25, 3.0, and 4.0 PDF Author: J. T. Best (Jr.)
Publisher:
ISBN:
Category : Drag (Aerodynamics).
Languages : en
Pages : 0

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Book Description
Static-force tests were conducted at Mach number 2.25, 3, and 4 on a 0.25 -scale model of the High Altitude Supersonic Target (HAST) missile.

Aerodynamic Characteristics of the HAST Missile at Mach Numbers 2.25, 3.0, and 4.0

Aerodynamic Characteristics of the HAST Missile at Mach Numbers 2.25, 3.0, and 4.0 PDF Author: J. H. Jones
Publisher:
ISBN:
Category : Drag (Aerodynamics)
Languages : en
Pages : 220

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Book Description
Static-force tests were conducted at Mach number 2.25, 3, and 4 on a 0.25 -scale model of the Beech High Altitude Supersonic Target (HAST) missile.

Investigation of the Static Longitudinal Stability and Roll Characteristics of a Three-stage Missile Configuration at Mach Numbers from 1.77 to 2.87

Investigation of the Static Longitudinal Stability and Roll Characteristics of a Three-stage Missile Configuration at Mach Numbers from 1.77 to 2.87 PDF Author: Donald T. Gregory
Publisher:
ISBN:
Category : Stability of airplanes, Longitudinal
Languages : en
Pages : 36

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Book Description

Longitudinal Stability and Drag Characteristics at Mach Numbers from 0.70 to 1.37 of Rocket-propelled Models Having a Modified Triangular Wing

Longitudinal Stability and Drag Characteristics at Mach Numbers from 0.70 to 1.37 of Rocket-propelled Models Having a Modified Triangular Wing PDF Author: Rowe Jr Chapman
Publisher:
ISBN:
Category :
Languages : en
Pages : 35

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Book Description

Static Stability and Separation Characteristics of a Two-stage Rocket Configuration at Mach Numbers from 1.57 to 4.50

Static Stability and Separation Characteristics of a Two-stage Rocket Configuration at Mach Numbers from 1.57 to 4.50 PDF Author: Kenneth L. Turner
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 44

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Book Description

Static Stability and Drag Characteristics of a Low Cost Full-Scale Target at Mach Numbers from 0.2 to 1.3

Static Stability and Drag Characteristics of a Low Cost Full-Scale Target at Mach Numbers from 0.2 to 1.3 PDF Author: J. B. Carman
Publisher:
ISBN:
Category :
Languages : en
Pages : 56

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Book Description
The static stability and drag characteristics were investigated for a 0.05-scale model of a Low Cost Full-Scale Target (LCFST) at Mach numbers from 0.2 to 1.3. Free-stream Reynolds number, based on the mean aerodynamic chord, varied between 0.9 and 2.2 million for angles of attack and sideslip of -2 to 8 deg and -3 to 3 deg, respectively. Data were obtained for horizontal tail deflections of -0.5 and -2 deg. Test results indicated that the target vehicle was statically stable in both the pitch and yaw planes. Negative deflection of the horizontal tail produced a substantial increase in pitching-moment coefficient at alpha = 0. (Author).

Static Longitudinal Stability and Control Characteristics at a Mach Number of 2.01 of a Hypersonic Missile Configuration Having All-movable Wing and Tail Surfaces

Static Longitudinal Stability and Control Characteristics at a Mach Number of 2.01 of a Hypersonic Missile Configuration Having All-movable Wing and Tail Surfaces PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 32

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Book Description

Static Stability Investigation of a Sounding-rocket Vehicle at Mach Numbers from 1.50 to 4.63

Static Stability Investigation of a Sounding-rocket Vehicle at Mach Numbers from 1.50 to 4.63 PDF Author: C. Donald Babb
Publisher:
ISBN:
Category : Sounding rockets
Languages : en
Pages : 82

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Book Description

Longitudinal Stability and Control Characteristics at Mach Numbers of 2.01, 4.65, and 6.8 of Two Hypersonic Missile Configurations, One Having Low-aspect-ratio Cruciform Wings with Trailing-edge Flaps and One Having a Flared Afterbody and All-movable Cont

Longitudinal Stability and Control Characteristics at Mach Numbers of 2.01, 4.65, and 6.8 of Two Hypersonic Missile Configurations, One Having Low-aspect-ratio Cruciform Wings with Trailing-edge Flaps and One Having a Flared Afterbody and All-movable Cont PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 36

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Book Description