Author: George Rudinger
Publisher:
ISBN:
Category :
Languages : en
Pages : 43
Book Description
Project SQUID: Effect of Boundary-Layer Growth in a Shock Tube on Shock Reflection from a Closed End
Author: George Rudinger
Publisher:
ISBN:
Category :
Languages : en
Pages : 43
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 43
Book Description
Effect of Boundary-layer Growth in a Shock Tube on Shock Reflection from a Closed End
Author: George Rudinger
Publisher:
ISBN:
Category :
Languages : en
Pages : 64
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 64
Book Description
The Influence of Shock and Boundary Layer Interaction on Shock Tube Flows
Author: L. Davies
Publisher:
ISBN:
Category :
Languages : en
Pages : 26
Book Description
During the last decade the study of the interaction between normal shocks and boundary layers in the shock tube has been carried out by many research workers. This interest has been fostered by the requirement to understand the effects that this phenomenon may have on the flow properties in the region between the reflected shock and the end of the tube. This so-called reflected shock region is important in chemical kinetics studies and as a reservoir of gas for hypersonic shock tunnels. In the paper a detailed review is given of the various analyses of the problem together with the results of experimental studies. Reflected and transmitted shock bifurcation, the rate of growth of the bifurcated foot, and the effects of transition to turbulence are discussed. The influence of bifurcation on the flow in the shock tube is assessed, especially as a mechanism for transporting cold driver gas to the end plate, causing early cooling of the gas in the reflected shock region. (Author).
Publisher:
ISBN:
Category :
Languages : en
Pages : 26
Book Description
During the last decade the study of the interaction between normal shocks and boundary layers in the shock tube has been carried out by many research workers. This interest has been fostered by the requirement to understand the effects that this phenomenon may have on the flow properties in the region between the reflected shock and the end of the tube. This so-called reflected shock region is important in chemical kinetics studies and as a reservoir of gas for hypersonic shock tunnels. In the paper a detailed review is given of the various analyses of the problem together with the results of experimental studies. Reflected and transmitted shock bifurcation, the rate of growth of the bifurcated foot, and the effects of transition to turbulence are discussed. The influence of bifurcation on the flow in the shock tube is assessed, especially as a mechanism for transporting cold driver gas to the end plate, causing early cooling of the gas in the reflected shock region. (Author).
U.S. Government Research Reports
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 744
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 744
Book Description
Observaciones sobre el recurso de casación interpuesto por D. Joaquín Gómez y Compañía, vecinos de la Habana, contra la sentencia dictada por una de las salas de aquella Audiencia Pretorial en el pleito con la heredera de D. José Antonio Bustamante, sobre indemnización de perjuicios y rendición de cuentas
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 64
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 64
Book Description
Growth of a laminar boundary layer behind incident shock waves in a shock tube
Author: Edward Steven Ehrhardt
Publisher:
ISBN:
Category : Fluid dynamics
Languages : en
Pages : 414
Book Description
Publisher:
ISBN:
Category : Fluid dynamics
Languages : en
Pages : 414
Book Description
Effects of Boundary Layer Buildup in Shock Tubes Upon Chemical Rate Measurements
Author: Marvin Warshay
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 26
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 26
Book Description
Effect of the Laminar Boundary Layer Development in a Shock Tube on Spectrum-line Reversal Temperature Measurements
Author: K. C. Lapworth
Publisher:
ISBN:
Category :
Languages : en
Pages : 24
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 24
Book Description
The Effect of a Laminar Boundary Layer on the Flow Behind a Shock Wave in a Shock Tube
Author: William Emil Simon
Publisher:
ISBN:
Category :
Languages : en
Pages : 122
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 122
Book Description
Project Squid. Remarks on the Interaction Between Shock Waves and Boundary Layer in Transonic and Supersonic Flow
Author: Lester Lees
Publisher:
ISBN:
Category :
Languages : en
Pages : 24
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 24
Book Description