On the spatio-temporal development of pulsed barrier discharges: influence of duty cycle variation

2012 ◽  
Vol 45 (24) ◽  
pp. 245201 ◽  
Author(s):  
M Kettlitz ◽  
H Höft ◽  
T Hoder ◽  
S Reuter ◽  
K-D Weltmann ◽  
...  
Author(s):  
Sithu Sudarsan ◽  
Vimalathithan Subramanian ◽  
Kenji Yoshigoe ◽  
Srini Ramaswamy ◽  
Remzi Seker ◽  
...  
Keyword(s):  

2020 ◽  
Vol 142 (5) ◽  
Author(s):  
Arne Berthold ◽  
Frank Haucke

Abstract The cooling ratio on a dynamically forced 7 × 7 impingement jet array is studied experimentally. The current study is focused on determining the influence of a phase shift between every row of nozzles as well as the impact of a duty cycle variation on the cooling ratio. Both parameters are studied in dependency of the impingement distance (H/D = 2, 3, 5), the (nozzle-) Reynolds-number (ReD = 3200, 5200, 7200), and the excitation frequency (f = 0 Hz − 1000 Hz). For every set of parameters, the phase shift between every row of nozzles is varied between Φ=0% and 90%, while the variation of the duty cycle is performed between duty cycle (DC) = 35% and 65%. During all investigations, the dimensionless distance between adjacent nozzles is fixed at Sx/D = Sy/D = 5, and liquid crystal thermography is used to acquire the wall temperatures, which are further processed to calculate the local Nusselt numbers. Generally, the implementation of an excitation frequency allows a case-depending increase in the cooling ratio of up to 52%. Further implementation of a phase shift yields an additional frequency-depending improvement of the cooling ratio. In case of duty cycle variation, the best case revealed an additional 19% improvement in the cooling ratio.


2006 ◽  
Author(s):  
C. J. Weiland ◽  
P. P. Vlachos

Supercavitation inception and formation was studied over blunt projectiles. The projectiles were fired using a gas gun method. In this method, projectiles are launched under the action of expanding detonation gases. Both qualitative and quantitative optical flow diagnostics using high speed digital imaging were used to analyze the spatio-temporal development of the supercavitating flow. For the first time, quantification of the supercavitation was achieved using Time Resolved Digital Particle Image Velocimetry (TRDPIV) detailing the two phase flow field surrounding the translating projectiles and the gas vapor bubble. Experimental results indicate that the supercavity forms at the aft end of the projectile and travels forward along the direction of projectile travel. The impulsive start of the projectile generates two asymmetric vortices which are shed from the blunt nose of the projectile. The vortices interact with the moving cavity and subsequently deform. This interaction is believed to directly contribute to the instabilities in the flight path.


2012 ◽  
Vol 4 (12) ◽  
pp. 3972-3994 ◽  
Author(s):  
Jana Edlinger ◽  
Christopher Conrad ◽  
John Lamers ◽  
Gulchekhra Khasankhanova ◽  
Thomas Koellner

2009 ◽  
Vol 96 (2) ◽  
pp. S25-S26
Author(s):  
Pankaj Gupta ◽  
Katherine Murphy ◽  
Matthew Nelson ◽  
Melissa Rusch ◽  
Zhenhong Nan ◽  
...  

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