An Investigation of the Damping in Pitch Characteristics of a Ten Degree Cone PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download An Investigation of the Damping in Pitch Characteristics of a Ten Degree Cone PDF full book. Access full book title An Investigation of the Damping in Pitch Characteristics of a Ten Degree Cone by Alfred Merle Morrison. Download full books in PDF and EPUB format.
Author: Alfred Merle Morrison
Publisher:
ISBN:
Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 102
Get Book Here
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.
Author: Alfred Merle Morrison
Publisher:
ISBN:
Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 102
Get Book Here
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.
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 88
Get Book Here
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.
Author: William R. Wehrend
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 28
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1572
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 628
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Government reports announcements & index
Languages : en
Pages : 882
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 538
Get Book Here
Book Description
Author: United States. Air Force. Office of Aerospace Research
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 368
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Research
Languages : en
Pages : 360
Get Book Here
Book Description
Author: United States. Air Force. Office of Aerospace Research
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 528
Get Book Here
Book Description
