Titlebook: Shock Waves @ Marseille III; Shock Waves in Conde Raymond Brun,Lucien Z. Dumitrescu Conference proceedings 1995 Springer-Verlag Berlin Heid

仔细阅读

很像弓]

Gastric

AGOG

Droplet Behaviour in Underexpanded Supersonic Jetsrmed. The outcome of the droplet break-up occuring under defined conditions in the converging nozzle, namely, the size distribution of the fragment droplets was measured using phase-Doppler anemometry. Furthermore, the interaction of the small fragment droplets with the strongly accelerating flow wi

六边形

Shock Tube Study of Droplet-Vapor Phase Transition of Hexane in Argon a rate of 10. cm..s. takes place. The growth process of the nuclei into droplets was monitored as well as the reevaporation of droplets after shock heating. Comparisons with model calculations were carried out.

织布机

表示向下

Drag Coefficient Measurement of Spheres in a Vertical Shock Tube and Numerical Simulationr not, and anyway by a reflected shock wave. Particle trajectories recorded with a high-speed motion picture camera are compared to analytical and simulated trajectories. The drag coefficients (0.50–0.62) obtained for this unsteady situation in a high Reynolds number range (5. × 10. · · · 1.2 × 10.) are higher than the standard steady value (0.4).

OFF

Needlework

Impact of Strong Shock Waves on Monodisperse Isopropanol Droplet Streamsf the shock tube. Droplet diameters range from 50 to 200 /.m, Weber numbers from 100 to 15000 and Reynolds numbers from 50 to 15000. Droplet spacing is adjustable between one and three droplet diameters. Shock Mach numbers can be varied between .. = 2 and .. = 6.

杀死