Interferometric Investigation of Supersonic Flow Fields with Shock- Shock Interactions 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 Interferometric Investigation of Supersonic Flow Fields with Shock- Shock Interactions PDF full book. Access full book title Interferometric Investigation of Supersonic Flow Fields with Shock- Shock Interactions by Mark Paul Loomis. Download full books in PDF and EPUB format.
Author: Mark Paul Loomis
Publisher:
ISBN:
Category :
Languages : en
Pages : 266
Get Book Here
Book Description
Author: Mark Paul Loomis
Publisher:
ISBN:
Category :
Languages : en
Pages : 266
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 702
Get Book Here
Book Description
Author: J. Winckler
Publisher:
ISBN:
Category :
Languages : en
Pages : 24
Get Book Here
Book Description
In earlier reports (PB-118 682 and AD-604 112) of this series it was shown how quantitative values of density, pressure, temperature, velocity and Mach number in supersonic gas streams could be obtained optically by the use of an interferometer. The Mach number M may be obtained independently by making shadow photographs of the head wave of a narrow probe placed in the stream. Probe and interferometer Mach number values were in good agreement in a homogeneous stream from a Laval nozzle, but in complete disagreement in an inhomogeneous expanding air jet in the region where standing shock waves occur. This discrepancy was traced to the influence of the standing shocks on the air flowing at low velocity in the boundary layer along the probe. The shock pressure may cause a separation of the stream from the probe, and a configuration of normal and oblique shocks arises as a result at the region of separation. Further experiments made in a strictly one-dimensional stream show an analagous separation of flow when a normal standing shock wave intercepts the boundary layer. The theory of separation is discussed. This report includes the details of the methods of applying the Mach interferometer to an axially symmetric flow pattern. The density distribution in such an air jet from a circ(Author).
Author:
Publisher:
ISBN:
Category : Military research
Languages : en
Pages : 1194
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 920
Get Book Here
Book Description
Author: Alfred Curtis Hunting
Publisher:
ISBN:
Category :
Languages : en
Pages : 282
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 686
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 654
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 648
Get Book Here
Book Description
Author: Raymond L. Chuan
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 114
Get Book Here
Book Description
