Wind-tunnel Investigation of the Static and Dynamic Stability Characteristics of a 10 Degree Semivertex Angle Blunted Cone PDF Download

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Wind-tunnel Investigation of the Static and Dynamic Stability Characteristics of a 10 Degree Semivertex Angle Blunted Cone

Wind-tunnel Investigation of the Static and Dynamic Stability Characteristics of a 10 Degree Semivertex Angle Blunted Cone PDF Author: William R. Wehrend
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 28

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Book Description

Wind-tunnel Investigation of the Static and Dynamic Stability Characteristics of a 10 Degree Semivertex Angle Blunted Cone

Wind-tunnel Investigation of the Static and Dynamic Stability Characteristics of a 10 Degree Semivertex Angle Blunted Cone PDF Author: William R. Wehrend
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 28

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Book Description

Wind-Tunnel Investigation of the Static and Dynamic Stability Characteristics of a 10 Degree Semivertex Angle Blunted Cone

Wind-Tunnel Investigation of the Static and Dynamic Stability Characteristics of a 10 Degree Semivertex Angle Blunted Cone PDF Author: WILLIAM R. JR. WEHREND
Publisher:
ISBN:
Category :
Languages : en
Pages : 1

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Book Description

Wind-tunnel Investigation of the Static and Dynamic Stability Characteristics of a 10 O Semivertex Angle Blunted Cone

Wind-tunnel Investigation of the Static and Dynamic Stability Characteristics of a 10 O Semivertex Angle Blunted Cone PDF Author: William R. Wehrend (Jr.)
Publisher:
ISBN:
Category :
Languages : en
Pages :

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Book Description

Wind-tunnel Investigation of the Static and Dynamic Stability Characteristics of a 10° Semivertex Angle Blunted Cone

Wind-tunnel Investigation of the Static and Dynamic Stability Characteristics of a 10° Semivertex Angle Blunted Cone PDF Author: William R. Wehrend
Publisher:
ISBN:
Category :
Languages : en
Pages : 21

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Book Description

Static Aerodynamic Characteristics of a Short Blunt 10 Degree Semivertex Angle Cone at a Mach Number of 15 in Helium

Static Aerodynamic Characteristics of a Short Blunt 10 Degree Semivertex Angle Cone at a Mach Number of 15 in Helium PDF Author: Melvin J. Fohrman
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 48

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Book Description

Motions of a Short 10 Degree Blunted Cone Entering a Martian Atmosphere at Arbitrary Angles of Attack and Arbitrary Pitching Rates

Motions of a Short 10 Degree Blunted Cone Entering a Martian Atmosphere at Arbitrary Angles of Attack and Arbitrary Pitching Rates PDF Author: Victor L. Peterson
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 44

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Book Description

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

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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Book Description

Free-flight Measurements of the Static and Dynamic Stability and Drag of a 10 Degree Blunted Cone at Mach Numbers 3.5 and 8.5

Free-flight Measurements of the Static and Dynamic Stability and Drag of a 10 Degree Blunted Cone at Mach Numbers 3.5 and 8.5 PDF Author: Peter F. Intrieri
Publisher:
ISBN:
Category : Noses (Space vehicles)
Languages : en
Pages : 40

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Book Description

An Investigation of the Damping in Pitch Characteristics of a Ten Degree Cone

An Investigation of the Damping in Pitch Characteristics of a Ten Degree Cone PDF Author: Alfred Merle Morrison
Publisher:
ISBN:
Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 102

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Book Description
A series of one-degree-of-freedom dynamic wind tunnel measurements were made for a standard Supersonic Tunnel Association ten degree cone with varying bluntnesses of .25, .1, .0167, and .07. Variations of the stability coefficients with angle-of-attack, bluntness, Reynolds number, and Mach number are obtained including Mach 18 data points for which no previous data existed. An explanation of reported difference between measured dynamic stability as obtained from ballistic range and wind tunnel techniques is offered. The equations of motion, data reduction techniques and experimental methods are also developed.