• Korean Journal of Optics and Photonics
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• v.14 no.4
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• pp.406-412
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• 2003

We have developed a radio frequency excited slab waveguide $CO_2$ laser. The dimension of active volume is 2${\times}$40${\times}$400 mm. One concave and one convex mirror are used to make the unstable resonator of the positive branch. The radio frequency is 123 MHz and RF input power is varied from 100 to 900 W. The laser gas is set to a pressure of 10∼60 torr and the mixing ratio is $CO_2$:$N_2$:He=1:1:3. The laser output power of 70.7 W was obtained which corresponds to laser power to RF power conversion efficiency of 9.2%.

• Korean Journal of Optics and Photonics
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• v.8 no.2
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• pp.107-110
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• 1997

We generated a diffraction free beam from Nd:YAG laser with an NBUR (negative branch unstable ring) resonator. The field inside the resonator had a plane wavefront and a homogeneous intensity distribution and the output beam through a scraper mirror of an annular type was used as a source. The outpur beam had an inner radius of 2.5 mm and an outer radius of 5 mm. In this experiment, we used a Fourier transformation lens with the focal length of 5 m to observe the far-field pattern. The lens was placed at a distance of the focal length from the scraper mirror and we found that the beam did not show any noticable diffraction over the distance of 13 m from the lens.

• Proceedings of the Optical Society of Korea Conference
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• 2000.02a
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• pp.310-311
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• 2000

Jo Bessel 빔은 무회절 빔으로서 빔이 전파해 가면서 강도 분포의 변화가 없는 빔이다.$^{[1]}$ 이 베셀빔을 구현하기 위해서는 무한대의 크기를 갖는 수렴렌즈를 사용하여야 하기 때문에 완벽한 베셀빔을 구현할 수는 없다. 그러나 원고리형 슬릿$^{[3]}$ , Axicon 및 Computer -Generated Hologram(CGH)을 사용하여 근사적인 Bessel 빔을 만들 수 있다. 본 실험에서는 Negative Branch Unstable Resonator(NBUR) 고리형 Nd:YAG 공진기와 scraper 출력경을 사용하여 원고리형 출력광을 얻으며, 이에 의한 Bessel 빔을 구현 하기 위한 이론적인 배경과 이의 전산시늉을 시도하고, 실험결과와의 비교, 분석하였다. (중략)

• Proceedings of the Optical Society of Korea Conference
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• 1991.06a
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• pp.9-12
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• 1991

방전가열형 구리증기레이저의 비축형 불안정공진기를 사용하여 레이저의 빔발산각을 안정공진기의 경우에 비해 25배 (200 $\mu$rad) 까지 줄였다. 이때 불안정공진기의 배율 M 은 50 이었으며, 평균출력은 안정공진기를 사용할 경우에 비해 53 %를 얻었다. 또한, M이 8.5 일 때 (750 $\mu$rad) 평균출력은 안정공진기의 94% 까지 도달하였다.

• Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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• 2003.05a
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• pp.424-428
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• 2003

We have developed the RF discharge Excited slab Waveguide $CO_2$ laser and measured the output power. We make used of concave and concave mirror, concave and convex mirror that negative branch and positive branch unstable resonator, respectively. The resonator active dimension is 2$\times$40$\times$400 mm and ratio frequency is 123 MHz. The gas mixing ratio is $CO_2$: $N_2$ : He=1 : 1 : 3. The pressure in resonator is from 10 to 60 torr and RF input power increased from 100 to 900 W. so that We obtained laser maximum output power of negative branch and positive branch resonator 50.9 W and 70.8 W and efficiency is 6.5 % and 9.2 %, respectively.

• Transactions of the Korean Society for Noise and Vibration Engineering
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• v.17 no.12
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• pp.1223-1229
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• 2007

Flow traveling over a cavity opening forms a vortex due to unstable shear layer and induces an aerodynamic pressure excitation from the diffusion of the vortex convecting out of the trailing edge of the opening. The interaction between the excitation force and the cavity response sustains resonance in the resonator(cavity) and locked-in vortex shedding at the leading edge of the opening. The aerodynamic excitation force can be described from the diffusion of the vortex over the trailing edge and the level of its diffusivity is related to the strength of vorticity seeded at the leading edge. In this study, the control scheme of the internal pressure oscillation was proposed from regulating the vorticity at the leading edge by use of an oscillating spoiler. It was found that the relative motion between the spoiler and the air mass at the cavity opening influenced vorticity strength and the control was achieved by direct feedback of the cavity pressure fluctuation to the actuator.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.34 no.8
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• pp.79-86
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• 2006

Swirl injector with adjustable backhole length was analyzed to suppress high-frequency combustion instability in Liquid Rocket Engines. In order to analyze the effect of variable backhole injector as an acoustic absorber, backhole injector was regarded as a quarter-wave resonator. As a result of theoretical approaches and acoustic tests, backhole injector with adjustable length could decrease the unstable modes of combustion chamber. And the damping efficiency was estimated by measuring damping rates experimentally.

• Korean Journal of Optics and Photonics
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• v.12 no.6
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• pp.496-502
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• 2001

We generated a nondiffracting beam and investigated its intensity profile on propagation. We first obtained an annular output beam from Nd:YAG laser with a negative branch unstable ring resonator and, using a 1m focal length lens, we generated a Bessel- Gauss beam. The inner radius of the annular output beam was 2.57 mm and the ring width was 0.145 mm. The intensity profile of the nondiffracting beam did not show any appreciable diffraction up to 33 m distance from the focal lens. This result was compared with the theory.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.34 no.10
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• pp.71-79
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• 2006

Swirl injector with multi-stage tangential entry was analyzed to suppress high-frequency combustion instability in Liquid Rocket Engines. In order to analyze the effect of swirl injector as an acoustic absorber, swirl injector was regarded as a quarter-wave resonator and it's damping capacity is verified in atmospheric temperature. It has a finite mode of vibration and natural frequencies which can be tuned to the natural frequencies of a model combustion chamber. The interior air core shape of injector is more stable in the case of using the swirl injector with multi-stage entry than with single-stage entry. Also, when the swirl injector with multi-stage entry is used, tuned-injector length for unstable mode is well agreed with the calculated length. From the experimental data, it is proved that if the interior air core shape of swirl injector is stable, the fine tuned swirl injector can decrease the unstable mode of model chamber effectively and increase the damping rate.

• Korean Journal of Optics and Photonics
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• v.15 no.4
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• pp.337-342
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• 2004

Laser optical power stabilization of a radio frequency excited $CO_2$ slab laser using the opto-Hertzian effect generated from the laser itself is achieved on the peak of the Doppler broadened gain curve. The opto-Hertzian signal was generated by a modulation of the optical flux circulating inside the laser cavity from a variation in the cavity length caused by the vibrations of the PZT. The opto-Hertzian signal is directly coupled from a RE discharge chamber via a loop antenna into a detector and applied to a lock-in stabilizer as an reference signal. The power stability of an RF excited slab laser is estimated to be better then 0.2%.