An Experimental Study of the Turbulent Wake Behind a Cone at Mach 5 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 Experimental Study of the Turbulent Wake Behind a Cone at Mach 5 PDF full book. Access full book title An Experimental Study of the Turbulent Wake Behind a Cone at Mach 5 by William C. Ragsdale. Download full books in PDF and EPUB format.
Author: William C. Ragsdale Publisher: ISBN: Category : Turbulence Languages : en Pages : 166
Book Description
An experimental study of the turbulent wake behind a 9° adiabatic cone at Mach 5 has been carried out in the U.S. Naval Ordnance Laboratory Hypersonic Tunnel. Cone models with base diameters of 2 inches and 4 inches were mounted in the wind tunnel test section with fine wires. Pitot pressure, pressure on a small cone probe and total temperature were measured with probes mounted on a vertical traversing mechanism. The measured pressures and temperatures were used to calculate the Mach number, static pressure, static temperature, velocity and density in the wake.
Author: William C. Ragsdale Publisher: ISBN: Category : Turbulence Languages : en Pages : 166
Book Description
An experimental study of the turbulent wake behind a 9° adiabatic cone at Mach 5 has been carried out in the U.S. Naval Ordnance Laboratory Hypersonic Tunnel. Cone models with base diameters of 2 inches and 4 inches were mounted in the wind tunnel test section with fine wires. Pitot pressure, pressure on a small cone probe and total temperature were measured with probes mounted on a vertical traversing mechanism. The measured pressures and temperatures were used to calculate the Mach number, static pressure, static temperature, velocity and density in the wake.
Author: William C. Ragsdale
Author: William C. Ragsdale
Author: Defense Documentation Center (U.S.)
Author: 
Author: 
Author: 
Author: 
Author: 
Author: 
Author: 
Author: