Shock-wave energy and acoustic energy dissipation after laser-induced breakdown

1998 ◽  
Author(s):  
Alfred Vogel ◽  
Joachim Noack
Keyword(s):  
Shock Wave ◽  
Energy Dissipation ◽  
Wave Energy ◽  
Acoustic Energy ◽  
Shock Wave Energy ◽  
Laser Induced Breakdown

Shock Wave Energy Dissipation in Catalyst-Free Poly(dimethylsiloxane) Vitrimers

2020 ◽  
Vol 53 (12) ◽  
pp. 4741-4747 ◽  
Author(s):  
Jaejun Lee ◽  
Brian B. Jing ◽  
Laura E. Porath ◽  
Nancy R. Sottos ◽  
Christopher M. Evans
Keyword(s):  
Shock Wave ◽  
Energy Dissipation ◽  
Wave Energy ◽  
Wave Energy Dissipation ◽  
Catalyst Free ◽  
Shock Wave Energy

scholarly journals Mechanochemistry for shock wave energy dissipation

2017 ◽  
Author(s):  
William L. Shaw ◽  
Yi Ren ◽  
Jeffrey S. Moore ◽  
Dana D. Dlott
Keyword(s):  
Shock Wave ◽  
Energy Dissipation ◽  
Wave Energy ◽  
Wave Energy Dissipation ◽  
Shock Wave Energy

Shock‐wave energy deflection due to the presence of bone

2006 ◽  
Vol 120 (5) ◽  
pp. 3109-3109
Author(s):  
Thomas Matula ◽  
Juan Tu ◽  
Michael Bailey ◽  
Kirsten Fagnan ◽  
Randy LeVeque
Keyword(s):  
Shock Wave ◽  
Wave Energy ◽  
Shock Wave Energy

scholarly journals TNT equivalent of the shock wave energy generated during the supersonic flight of an aircraft

2021 ◽  
Vol 2124 (1) ◽  
pp. 012001
Author(s):  
Ya V Drobzheva ◽  
D V Zikunkova ◽  
V M Krasnov
Keyword(s):  
Shock Wave ◽  
Wave Energy ◽  
Acoustic Pulse ◽  
Nonlinear Effects ◽  
Aircraft Design ◽  
Resistance Force ◽  
Supersonic Speed ◽  
Tnt Equivalent ◽  
Shock Wave Energy ◽  
The Impact

Abstract To assess the impact on human health of the sonic boom that occurs when an aircraft is flying at supersonic speed, and, accordingly, to solve the problem of noise reduction by optimizing the aircraft design, it is proposed to evaluate the shock wave energy using the TNT equivalent of a cylindrical explosion. An example of calculating the shock wave energy during flights of F4 and F18 aircraft at different altitudes is considered. To calculate the evolution of an acoustic pulse during its propagation from the boundary of the shock wave transition to the acoustic one, the wave equation and its solution are used, taking into account the inhomogenei-ty of the atmosphere, nonlinear effects, absorption and expansion of the wave front, as well as the results of ground-based measurements of acoustic pulses. The results of calculations of the dependence of the explosion energy on the flight altitude, as well as on the type of aircraft are explained on the basis of the formula for the atmospheric resistance force.

Shock Wave Energy Absorption in Metal–Organic Framework

2019 ◽  
Vol 141 (6) ◽  
pp. 2220-2223 ◽  
Author(s):  
Xuan Zhou ◽  
Yu-Run Miao ◽  
William L. Shaw ◽  
Kenneth S. Suslick ◽  
Dana D. Dlott
Keyword(s):  
Shock Wave ◽  
Energy Absorption ◽  
Wave Energy ◽  
Metal Organic Framework ◽  
Shock Wave Energy ◽  
Metal Organic ◽  
Organic Framework

Shock Wave Energy: Explosions in Air, Ground, and Water

2017 ◽  
pp. 1307-1311
Author(s):  
Lippe D. Sadwin ◽  
Michael M. Swisdak ◽  
Y. Gitterman ◽  
Oren Lotan
Keyword(s):  
Shock Wave ◽  
Wave Energy ◽  
Shock Wave Energy
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