Shock impact simulation model along with the harmonic effect of the working device. [PDF]
Grządziela A +3 more
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Effects of Equal Channel Angular Pressing on the Microstructure and Mechanical Properties of Explosion-Welded Al-Cu Bimetallic Plates. [PDF]
Żaba K +8 more
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High-harmonic generation in Weyl semimetal β-WP2 crystals. [PDF]
Lv YY +14 more
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Propagatory dynamics of nucleus-acoustic waves excited in gyrogravitating degenerate quantum plasmas electrostatically confined in curved geometry. [PDF]
Dasgupta S, Karmakar PK.
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Preparation Technology, Reactivity and Applications of Nano-Aluminum in Explosives and Propellants: A Review. [PDF]
Guo H, Zhang W, Pang W.
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3D Simulation of a Detonation Wave in a Rotating Detonation Engine
O desenvolvimento de sistemas de propulsão eficientes é um aspeto crítico na engenharia aeroespacial, e os motores de detonação rotativa (RDEs) apresentam um avanço promissor em relação às tecnologias de propulsão convencionais devido às suas configurações compactas e alta eficiência térmica.
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Airborne metal nanoparticles released by azides detonation: determination and potential public exposure. [PDF]
Cen T +5 more
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Mesoscopic Kinetic Approach of Nonequilibrium Effects for Shock Waves. [PDF]
Qiu R, Yang X, Bao Y, You Y, Jin H.
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On methodology and application of smoothed particle hydrodynamics in fluid, solid and biomechanics. [PDF]
Xu F +5 more
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We describe the critical condition necessary for the inner cylinder radius of a rotating detonation engine (RDE) used for in-space rocket propulsion to sustain adequate thruster performance. Using gaseous C2H4 and O2 as the propellant, we measured thrust and impulse of the RDE experimentally, varying in the inner cylinder radius ri from 31 mm (typical ...
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