Effect of Body Nose Blunting, Control Planform Area, and Leading-edge Bluntness on Aerodynamic Control of a 5 Degree Semivertex Cone at Mach Number 6.9 PDF Download

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Effect of Body Nose Blunting, Control Planform Area, and Leading-edge Bluntness on Aerodynamic Control of a 5 Degree Semivertex Cone at Mach Number 6.9

Effect of Body Nose Blunting, Control Planform Area, and Leading-edge Bluntness on Aerodynamic Control of a 5 Degree Semivertex Cone at Mach Number 6.9 PDF Author: Jim A. Penland
Publisher:
ISBN:
Category :
Languages : en
Pages : 66

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Book Description

Effect of Body Nose Blunting, Control Planform Area, and Leading-edge Bluntness on Aerodynamic Control of a 5 Degree Semivertex Cone at Mach Number 6.9

Effect of Body Nose Blunting, Control Planform Area, and Leading-edge Bluntness on Aerodynamic Control of a 5 Degree Semivertex Cone at Mach Number 6.9 PDF Author: Jim A. Penland
Publisher:
ISBN:
Category :
Languages : en
Pages : 66

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Book Description

Effect of Body Nose Blunting, Control Planform Area, and Leading-edge Bluntness on Aerodynamic Control of a 5 ̊semivertex Cone at Mach Number 6.9

Effect of Body Nose Blunting, Control Planform Area, and Leading-edge Bluntness on Aerodynamic Control of a 5 ̊semivertex Cone at Mach Number 6.9 PDF Author: Jim A. Penland
Publisher:
ISBN:
Category : Cone
Languages : en
Pages : 74

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Book Description

Effects 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 ̊

Effects 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 ̊ PDF Author: David S. Shaw
Publisher:
ISBN:
Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 88

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Book Description

Effect of Nose Bluntness on Transition for a Cone and a Hollow Cylinder at Mach Numbers 1.41 and 2.01

Effect of Nose Bluntness on Transition for a Cone and a Hollow Cylinder at Mach Numbers 1.41 and 2.01 PDF Author: William J. Monta
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 38

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Book Description

Pressure Measurements on Sharp and Blunt 5 Degreee and 15 Degree-half-angle Cones at Mach Number 3.86 and Angles of Attack to 100 Degrees

Pressure Measurements on Sharp and Blunt 5 Degreee and 15 Degree-half-angle Cones at Mach Number 3.86 and Angles of Attack to 100 Degrees PDF Author: James L. Amick
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 52

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Book Description

Effect of Unit Reynolds Number, Nose Bluntness, Angle of Attack, and Roughness on Transition on a 5° Half-angle Cone at Mach 8

Effect of Unit Reynolds Number, Nose Bluntness, Angle of Attack, and Roughness on Transition on a 5° Half-angle Cone at Mach 8 PDF Author: P. Calvin Stainback
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 82

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Transonic Investigation of the Effects of Nose Bluntness, Fineness Ratio, Cone Angle, and Base Shape on the Static Aerodynamic Characteristics of Short, Blunt Cones at Angles of Attack to 1800

Transonic Investigation of the Effects of Nose Bluntness, Fineness Ratio, Cone Angle, and Base Shape on the Static Aerodynamic Characteristics of Short, Blunt Cones at Angles of Attack to 1800 PDF Author: Cuyler W. Brooks
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 48

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Static Aerodynamic Characteristics of Short Blunt Cones with Various Nose and Base Cone Angles at Mach Numbers from 0.6 to 5.5 and Angles of Attack to 180 Degrees

Static Aerodynamic Characteristics of Short Blunt Cones with Various Nose and Base Cone Angles at Mach Numbers from 0.6 to 5.5 and Angles of Attack to 180 Degrees PDF Author: Stuart L. Treon
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 40

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Book Description

Effects 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 Degrees

Effects 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 Degrees PDF Author: David S. Shaw
Publisher:
ISBN:
Category :
Languages : en
Pages : 77

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Book Description

Effect of Nose Bluntness on Transition for a Cone and a Hollow Cylinder at Mach Numbers 1.41 and 2.01

Effect of Nose Bluntness on Transition for a Cone and a Hollow Cylinder at Mach Numbers 1.41 and 2.01 PDF Author: William J. Monta
Publisher:
ISBN:
Category :
Languages : en
Pages : 34

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Book Description