Results 321 to 330 of about 2,038,462 (393)
Some of the next articles are maybe not open access.
The Physics of Fluids, 1966
Simple theoretical derivation is given of the empirical formula of Emrich and Wheeler which enables one to calculate the shock wave attenuation due to boundary layer effect from the initial pressure conditions in a shock tube.
openaire +1 more source
Simple theoretical derivation is given of the empirical formula of Emrich and Wheeler which enables one to calculate the shock wave attenuation due to boundary layer effect from the initial pressure conditions in a shock tube.
openaire +1 more source
1991
Abstract : This work was undertaken to increase the understanding of the fluid dynamics of shock wave reflection phenomena. Parametric height-of-burst (HOB) experiments were performed to establish a consistent set of HOB peak overpressure curves in the low pressure regime (< 100 psi) for hydrodynamically smooth and rough surfaces.
G. Scheklinski-Gluck, H. Reichenbach
openaire +1 more source
Abstract : This work was undertaken to increase the understanding of the fluid dynamics of shock wave reflection phenomena. Parametric height-of-burst (HOB) experiments were performed to establish a consistent set of HOB peak overpressure curves in the low pressure regime (< 100 psi) for hydrodynamically smooth and rough surfaces.
G. Scheklinski-Gluck, H. Reichenbach
openaire +1 more source
Review of experimental Richtmyer–Meshkov instability in shock tube: From simple to complex
, 2018Z. Zhai, L. Zou, Qiang Wu, Xisheng Luo
semanticscholar +1 more source
High-speed imaging of inhomogeneous ignition in a shock tube
, 2018A. Tulgestke +3 more
semanticscholar +1 more source
Shock-tube studies of Sarin surrogates
Shock Waves, 2018O. Mathieu, W. Kulatilaka, E. Petersen
semanticscholar +1 more source
Shock wave induced anatase to rutile TiO2 phase transition using pressure driven shock tube
, 2018S. Kalaiarasi +3 more
semanticscholar +1 more source
1954
The feasibility of using a shock tube for quantitative investigations of hypersonic flow phenomena at temperatures simulating free flight conditions is studied theoretically and experimentally. In the theoretical part, various aspects of the hypersonic shock tube problem are treated in logical order.
openaire +1 more source
The feasibility of using a shock tube for quantitative investigations of hypersonic flow phenomena at temperatures simulating free flight conditions is studied theoretically and experimentally. In the theoretical part, various aspects of the hypersonic shock tube problem are treated in logical order.
openaire +1 more source
Shock tube studies of ethanol preignition
Combustion and Flame, 2018M. Figueroa-Labastida +3 more
semanticscholar +1 more source