scholarly journals Effect of Off-Body Laser Discharge on Drag Reduction of Hemisphere Cylinder in Supersonic Flow-Part II

Author(s):  
Nadia Kianvashrad ◽  
Doyle D. Knight ◽  
Stephen P. Wilkinson ◽  
Amanda Chou ◽  
George B. Beeler ◽  
...  
Author(s):  
Nadia Kianvashrad ◽  
Doyle D. Knight ◽  
Stephen P. Wilkinson ◽  
Amanda Chou ◽  
Robert A. Horne ◽  
...  

2021 ◽  
Vol 2021 ◽  
pp. 1-14
Author(s):  
HaiLong Zhao ◽  
Ke Peng ◽  
ZePing Wu ◽  
WeiHua Zhang ◽  
JiaWei Yang ◽  
...  

Drag reduction is one of the important problems for the supersonic vehicles. As one of the drag reduction methods, aerospike has been used in some equipment because of its good drag reduction effect. In this paper, the numerical simulations of Carman curve bodies with different lengths of the aerospike and different radius of the flat cylindrical aerodisk in supersonic flow freestream are investigated. Based on the numerical simulations, the mechanism of drag reduction of the aerospike is discussed. The drag reduction effect influence of the parameters of the aerodisk radius and the aerospike length on the Carman curve body is analyzed. The aerodisk radius within a certain range is helpful for the drag reduction. The change of length of the aerospike has little effect on the drag of Carmen curve bodies. The drag reduction effect of the same aerospike becomes worse with the increase of the incoming Mach number.


1992 ◽  
Vol 63 (6) ◽  
pp. 1171-1175 ◽  
Author(s):  
V. Yu. Borzov ◽  
I. V. Rybka ◽  
A. S. Yur'ev

1985 ◽  
Vol 22 (6) ◽  
pp. 663-665 ◽  
Author(s):  
Eugen Serbanescu ◽  
George Savu

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.


1976 ◽  
Vol 75 (4) ◽  
pp. 751-764 ◽  
Author(s):  
L. F. Henderson ◽  
J. D. Atkinson

The shock wave equations for a perfect gas often provide more than one solution to a problem. In an attempt to find out which solution appears in a given physical situation, we present a linearized analysis of the equations of motion of a flow field with a shock boundary. It is found that a solution will be stable when there is supersonic flow downstream of the shock, and asymptotically unstable when there is subsonic flow downstream of it. It is interesting that both flows are found to be stable against disturbances of the d'Alembert type which grow from point sources; it is only when larger-scale line sources are considered that one can discriminate between the stabilities of the two types of flow. The results are applicable to supersonic flow over flat plates at incidence, to wedges, and to some cases of regular reflexion, diffraction and refraction of shocks.


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