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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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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An Experimental Investigation of the Aerodynamic Characteristics of Slender Hypersonic Vehicles at High Angles of Attack

An Experimental Investigation of the Aerodynamic Characteristics of Slender Hypersonic Vehicles at High Angles of Attack PDF Author: Robert H. Feldhuhn
Publisher:
ISBN:
Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 148

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Pressure, heat transfer, force, flow field surveys and flow visualization measurements on an inclined cone were obtained in a wind tunnel at a nominal Mach number of 6. Force measurements were also obtained for a 2/3 power law body and two ducted-cone configurations.

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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Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author: United States. Superintendent of Documents
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Category : Government publications
Languages : en
Pages : 1320

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Monthly Catalog of United States Government Publications, Cumulative Index

Monthly Catalog of United States Government Publications, Cumulative Index PDF Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : United States
Languages : en
Pages : 1348

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Journal of the Royal Aeronautical Society

Journal of the Royal Aeronautical Society PDF Author:
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Category : Aeronautics
Languages : en
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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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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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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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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
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Pages : 40

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Book Description