Paper
17 September 2013 The influence of the inflow speed on air-breathing supersonic laser propulsion
Lei Shi, Hao Chen, Li-hua Ma, Yong-an Chen, Zhi-yan Xu, Hua Hong
Author Affiliations +
Proceedings Volume 8904, International Symposium on Photoelectronic Detection and Imaging 2013: High Power Lasers and Applications; 89040N (2013) https://doi.org/10.1117/12.2032968
Event: ISPDI 2013 - Fifth International Symposium on Photoelectronic Detection and Imaging, 2013, Beijing, China
Abstract
A model of coupled dynamics for supersonic airbreathing propulsion is developed to simulate the development process of the thruster’s flowfield. The influence of the inflow speed, from 1 to 4 Mach, on the laser propulsion performance is investigated numerically. The results indicate that the inflow speed has a marked effect on the propulsion efficiency. Under the same laser parameters, the larger inflow speed leads to lower thruster and impulse coupling coefficient. By analyzing the phenomena in the complex unsteady flowfield, we found that the bow shock occurring out of the surface of the thruster due to supersonic inflow is the real cause of the performance worsening and air drag reduction becomes a very important task at supersonic laser propulsion.
© (2013) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Lei Shi, Hao Chen, Li-hua Ma, Yong-an Chen, Zhi-yan Xu, and Hua Hong "The influence of the inflow speed on air-breathing supersonic laser propulsion", Proc. SPIE 8904, International Symposium on Photoelectronic Detection and Imaging 2013: High Power Lasers and Applications, 89040N (17 September 2013); https://doi.org/10.1117/12.2032968
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CITATIONS
Cited by 2 scholarly publications.
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KEYWORDS
Laser propulsion

Pulsed laser operation

Wave propagation

Plasma

Curium

Numerical simulations

Laser energy

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