Author: D. J. James
Publisher:
ISBN:
Category :
Languages : en
Pages : 46
Book Description
An Investigation of the Pressure Wave Propagated from the Open End of a 30x18 Inch Shock Tube
Author: D. J. James
Publisher:
ISBN:
Category :
Languages : en
Pages : 46
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 46
Book Description
An Investigation of the Pressure Wave Propagated from the Open End of a 30 X 18 In. Shock Tube
Author: D. J. James
Publisher:
ISBN:
Category :
Languages : en
Pages : 33
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 33
Book Description
Nuclear Science Abstracts
Author:
Publisher:
ISBN:
Category : Nuclear energy
Languages : en
Pages : 1144
Book Description
Publisher:
ISBN:
Category : Nuclear energy
Languages : en
Pages : 1144
Book Description
Preliminary Investigation of the Shock Wave Propagated from the Open End of a Cylindrical Shock Tube
Author: G. Beichler
Publisher:
ISBN:
Category : Shock waves
Languages : en
Pages : 18
Book Description
Publisher:
ISBN:
Category : Shock waves
Languages : en
Pages : 18
Book Description
A Study of Shock-tube Phenomena
Author: Harold Vincent Wright
Publisher:
ISBN:
Category : Shock waves
Languages : en
Pages : 262
Book Description
Publisher:
ISBN:
Category : Shock waves
Languages : en
Pages : 262
Book Description
Shock Tubes and Waves
Author: Charles E. Treanor
Publisher: SUNY Press
ISBN: 9780873955959
Category : Philosophy
Languages : en
Pages : 1130
Book Description
Proceedings from a symposium on shock tubes and waves held July 6-9, 1981.
Publisher: SUNY Press
ISBN: 9780873955959
Category : Philosophy
Languages : en
Pages : 1130
Book Description
Proceedings from a symposium on shock tubes and waves held July 6-9, 1981.
Experimental Investigation of Attenuation of Strong Shock Waves in a Shock Tube with Hydrogen and Helium as Driver Gases
Author: Jim J. Jones
Publisher:
ISBN:
Category : Helium
Languages : en
Pages : 716
Book Description
An experimental investigation has been made of the attenuation of strong shock waves in air in a shock tube. Time-history measurements were made of the static pressure at several stations in the wall of the tube. The internal diameter of the tube is 3.75 inches. shock-wave-velocity data were taken for a distance along the tube of about 120 feet.
Publisher:
ISBN:
Category : Helium
Languages : en
Pages : 716
Book Description
An experimental investigation has been made of the attenuation of strong shock waves in air in a shock tube. Time-history measurements were made of the static pressure at several stations in the wall of the tube. The internal diameter of the tube is 3.75 inches. shock-wave-velocity data were taken for a distance along the tube of about 120 feet.
Analysis of the Wave System Propagated Into a Conical Shock Tube from the Open End
Author: Jon J. Yagla
Publisher:
ISBN:
Category :
Languages : en
Pages : 45
Book Description
The method of characteristics was applied to compute the flow properties of the wave reflected from the open end of a conical shock tube. It was found that the resultant rarefaction wave is followed by a compression wave sufficiently strong to form a shock wave which travels back up the shock tube. The details of the rarefaction process were determined and the locus of the shock was plotted in the time-distance plane. The shock's strength and the properties of the subsequent flow were computed. (Author).
Publisher:
ISBN:
Category :
Languages : en
Pages : 45
Book Description
The method of characteristics was applied to compute the flow properties of the wave reflected from the open end of a conical shock tube. It was found that the resultant rarefaction wave is followed by a compression wave sufficiently strong to form a shock wave which travels back up the shock tube. The details of the rarefaction process were determined and the locus of the shock was plotted in the time-distance plane. The shock's strength and the properties of the subsequent flow were computed. (Author).
a study of cylidrical shock waves in a sector tube
Author: a. cole
Publisher:
ISBN:
Category :
Languages : en
Pages : 164
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 164
Book Description
The Shock Tube as an Instrument for the Investigation of Transonic and Supersonic Flow Patterns
Author: Frederick William Geiger
Publisher:
ISBN:
Category : Transportation
Languages : en
Pages : 218
Book Description
Publisher:
ISBN:
Category : Transportation
Languages : en
Pages : 218
Book Description