Aerodynamic Investigation of Sharp Cone-cylinder Spikes on 120 ̊blunted Cones at Mach Numbers of 3.00, 4.50, and 6.00 PDF Download

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Aerodynamic Investigation of Sharp Cone-cylinder Spikes on 120 ̊blunted Cones at Mach Numbers of 3.00, 4.50, and 6.00

Aerodynamic Investigation of Sharp Cone-cylinder Spikes on 120 ̊blunted Cones at Mach Numbers of 3.00, 4.50, and 6.00 PDF Author: Robert J. McGhee
Publisher:
ISBN:
Category : Blunt bodies
Languages : en
Pages : 50

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Aerodynamic Investigation of Sharp Cone-cylinder Spikes on 120 ̊blunted Cones at Mach Numbers of 3.00, 4.50, and 6.00

Aerodynamic Investigation of Sharp Cone-cylinder Spikes on 120 ̊blunted Cones at Mach Numbers of 3.00, 4.50, and 6.00 PDF Author: Robert J. McGhee
Publisher:
ISBN:
Category : Blunt bodies
Languages : en
Pages : 50

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Aerodynamic Investigation of Sharp Cone-cylinder Spikes on 120 Degree Blunted Cones at Mach Numbers of 3.00, 4.50, and 6.00

Aerodynamic Investigation of Sharp Cone-cylinder Spikes on 120 Degree Blunted Cones at Mach Numbers of 3.00, 4.50, and 6.00 PDF Author: Robert J. McGhee
Publisher:
ISBN:
Category :
Languages : en
Pages : 39

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Aerodynamic Investigation of Sharp Cone-cylinder Spikes on 120° Blunted Cones at Mach Numbers of 3.00, 4.50, and 6.00

Aerodynamic Investigation of Sharp Cone-cylinder Spikes on 120° Blunted Cones at Mach Numbers of 3.00, 4.50, and 6.00 PDF Author: Robert J. MacGhee
Publisher:
ISBN:
Category :
Languages : en
Pages : 39

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Flow-field Investigation for Large-angle Cones with Short Spikes at a Mach Number of 9.6

Flow-field Investigation for Large-angle Cones with Short Spikes at a Mach Number of 9.6 PDF Author: W. Frank Staylor
Publisher:
ISBN:
Category : Blunt bodies
Languages : en
Pages : 42

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Stability Investigation of a Blunted Cone and a Blunted Ogive with a Flared Cylinder Afterbody at Mach Numbers from 0.30 to 2.85

Stability Investigation of a Blunted Cone and a Blunted Ogive with a Flared Cylinder Afterbody at Mach Numbers from 0.30 to 2.85 PDF Author: Lucille C. Coltrane
Publisher:
ISBN:
Category :
Languages : en
Pages : 34

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Longitudinal Aerodynamic Characteristics of Blunted Cones at Mach Numbers of 3.5, 4.2, and 6.0

Longitudinal Aerodynamic Characteristics of Blunted Cones at Mach Numbers of 3.5, 4.2, and 6.0 PDF Author: J. Wayne Keyes
Publisher:
ISBN:
Category : Cone
Languages : en
Pages : 72

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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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Wind-tunnel Investigation at Mach Numbers from 1.47 to 4.62 of Static Aerodynamic Characteristics of Twelve Nose Cones Designed for Supersonic Impact

Wind-tunnel Investigation at Mach Numbers from 1.47 to 4.62 of Static Aerodynamic Characteristics of Twelve Nose Cones Designed for Supersonic Impact PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 34

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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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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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