Stereoscopic PIV of Supersonic Flow Past an Ogive-Cylinder in the Presence of Off-Axis Laser Energy Deposition

Author(s):  
Arastou Pournadali Khamseh ◽  
Ramez M. Kiriakos ◽  
Edward P. DeMauro
2022 ◽  
Author(s):  
Shankar Ghosh ◽  
Anurag Chauhan ◽  
Rohan Pattankar

Author(s):  
Mahsa Mortazavi ◽  
Doyle D. Knight ◽  
Olga A. Azarova ◽  
Jingchang Shi ◽  
Hong Yan

2020 ◽  
Vol 53 (26) ◽  
pp. 265201 ◽  
Author(s):  
Rajib Mahamud ◽  
Daniel W Hartman ◽  
Albina A Tropina

Energies ◽  
2019 ◽  
Vol 12 (20) ◽  
pp. 3914
Author(s):  
Seihwan Kim ◽  
Hyoung Jin Lee

In the present study, a two-dimensional axisymmetry unsteady numerical simulation that implements high-frequency laser energy deposition was performed to understand its influence on drag reduction in supersonic flow. The energy deposition was modeled as the increase of the temperature inside the focal region. The drag reduction characteristics were investigated by changing the frequency of the deposition, the distance between the focus of the deposition and the body, and the power of the laser. The results showed that drag could be reduced by 60% when there was a single energy deposition. As the operating frequency increased, up to 70% drag reduction was obtained. When the laser energy was deposed more frequently than 75 kHz, the normalized drag converged regardless of the deposition scenario, which resulted from the multiple interactions between the blast wave and the reflected shock. A similar tendency was found from the results of various focal distances. According to the results of this study on the effect of the deposition energy, it is expected to achieve the same effect as with low energy by increasing the frequency of the deposition.


1950 ◽  
Vol 1 (4) ◽  
pp. 305-318
Author(s):  
G. N. Ward

SummaryThe approximate supersonic flow past a slender ducted body of revolution having an annular intake is determined by using the Heaviside operational calculus applied to the linearised equation for the velocity potential. It is assumed that the external and internal flows are independent. The pressures on the body are integrated to find the drag, lift and moment coefficients of the external forces. The lift and moment coefficients have the same values as for a slender body of revolution without an intake, but the formula for the drag has extra terms given in equations (32) and (56). Under extra assumptions, the lift force due to the internal pressures is estimated. The results are applicable to propulsive ducts working under the specified condition of no “ spill-over “ at the intake.


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