• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.39 no.9
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• pp.816-822
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• 2011

In this study, a program has been coded to evaluate propeller thrust rapidly following the effects of propeller shapes and the environmental facts. At this time, Semi-infinite Helical Vortices model is used to predict the induction factor which is introduced by Kawada. This program is based on Wrench's Propeller lifting line theory, and it can predict aerodynamic coefficients such as thrust, power, and efficiency. First of all, this program is compared with test results of NACA reports to verify of the reliability. Secondly, subsonic wind tunnel test has been performed following variations of propeller's rpm and inflow velocities.

• Journal of the Korean Society of Propulsion Engineers
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• v.7 no.3
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• pp.45-52
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• 2003

Detailed flowfield resulting from the secondary sonic gas injection into a divergent section of supersonic conical nozzle has been numerically investigated. The three-dimensional flowfield associated with the bow-shock/boundary-layer interaction inside the nozzle has been solved by Reynolds-averaged Navier-Stokes equations with an algebraic and $\kappa$-$\varepsilon$ turbulence model. The numerical results have been compared with the experimental results for the identical flow conditions, and it is shown that the comparison is satisfactory Effects of different injection pressures of the secondary jet on the shock/boundary-layer interactions and the overall flow structure inside the nozzle have been investigated. The vortex structures behind the shock interaction and wall pressure variations have also been studied.

• Aerospace Engineering and Technology
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• v.12 no.1
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• pp.207-212
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• 2013

To investigate the possibility of using artificial means for the control of shear layers in swirl jets, a shear excitation device is introduced. The device consists of co-centric dual nozzles with internal lobes (i.e., convex surfaces) of small height to induce disturbance. The number of convexities can be varied to produce the various modes in azimuthal direction. The acquired velocity data of the swirling jets, with and without the lobes, are numerically simulated in 2-D contour plots and 3-D particle trace plots. The results are compared with the baseline (i.e., no excitation case) at various excitation modes. Conclusively it is observed that the artificial excitation method is effective in the control of the vortical structure in swirling jets.

• Journal of the Korean Society of Propulsion Engineers
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• v.22 no.5
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• pp.81-87
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• 2018

In hypersonic aircraft, increase of aerodynamic and engine heat lead thermal load in airframe. It could lead structural change of aircraft's component and malfunctioning. Endothermic fuels are liquid hydrocarbon fuels which absorb the heat load by undergoing endothermic reactions. In this study, we investigated the relationship between product, coke formation and catalytic properites of endothermic catalysts by using exo-tetrahydrodicyclopentadiene as a fuel in a fixed bed flow reactor similar to the actual reaction conditions.

• The Journal of the Acoustical Society of Korea
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• v.6 no.4
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• pp.64-73
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• 1987

Low frequency sound propagation in a range-dependent shallow water environment of the Korea Strait has been studied by using the adiabatic coupled mode, ADIAB. The range-dependent environment is unique in terms of horizontal variations of sound velocity profiles, sediment thickness and attenuation coefficients and water depths. For shallow source and receiver depths, the most important mechanism involved in the propagation loss is the depth changing character of mode functions that strongly depends on the local sound velocity profile. Application of the adiabatic coupled mode theory to shallow water environment is reasonable when higher modes are attenuated due to bottom interaction effects. Underwater sound propagation in a range-dependent shallow-water environment.

• Proceedings of the Acoustical Society of Korea Conference
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• spring
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• pp.365-368
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• 2002

수중에서와 같이 전자기파의 사용이 곤란한 환경에서 정보의 전달 방법으로 초음파를 사용하는 것이 일반적이다. 그러나 기존의 방법은 음파의 전파 경로 상에 있어서 잡음, 온도, 음속 등의 환경에 많은 영향을 받기 때문에 정확한 정보의 전달이 곤란한 경우가 있다. 본 연구에서는 전기적 용량으로 특성을 제어할 수 있는 2층 구조 압전 트랜스듀서에 있어서 전기적 용량 변화에 따른 공진 모드간의 효율 비의 변화를 이용하여 전파 경로 상의 환경 변화에 독립적인 원격 물리 계측법을 제안하고 그 가능성을 확인하였다.

• The Journal of the Acoustical Society of Korea
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• v.12 no.6
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• pp.5-12
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• 1993

고주파 음원을 사용하여 측정한 천해 해역에서의 잔향음 특성 변화와 해양 환경요소와의 연관성을 고찰하고자 하였다. 여름철에 실시한 현장실험에서 획득한 잔향음신호를 분석하여 다음과 같은 결과를 얻었다. 1) 수직 음속이 음의 기울기를 갖고 있어서 해저면 잔향음이 우세하다. 2) 음파발사 방위각에 따라 19dB 이상의 해저면 잔향음준위 차이를 보인다. 3) 계산된 해저면 후방산란 강도는 기존의 측정자료에 비해 약간 높게 나타난다.

• Proceedings of the KWS Conference
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• 2004.05a
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• pp.321-323
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• 2004

전자 제품에 사용되는 부품 ㆍ소재의 신뢰성 품질 평가를 위해 정밀한 모터의 제어기술, 첨단신호처리 기술, 압전소자 기술의 발달로 미세변화 계측의 재현성, 고분해능, 표면과 내부의 이미지관찰, 또한 미소부위에서 재료의 누설탄성표면파의 음속측정이 가능한 초음파현미경에 대한 연구가 최근 들어 활발히 진행되고 있다. (중략)

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 1996.05a
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• pp.41-47
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• 1996

데토네이션 현상은 화학반응면이 음속 이상으로 진행하는 경우로 연소와는 다른 분야로 취급된다. 국내에서는 발파나 무기에 응용되고 있지만 이 분야의 선진국에서는 산업의 여러 분야에 적용되며 이 분야에 많은 기초연구가 행해져 왔다. 본 연구는 이러한 데토네이션 현상을 콘크리이트나 금속의 절단이나 노화된 구조물의 해체에 응용하는 것에 관한 내용으로 고체폭약에 비해 위험하여 취급이 어려운 액체 폭약을 보다 안전하고 현상변화가 자유로운 액체의 잇점을 살려 절단에 있어 최대의 효율을 내는 형상을 단지 케이스의 가공만으로 가능하므로 경제적이다.

• The Journal of the Acoustical Society of Korea
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• v.38 no.2
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• pp.214-221
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• 2019

In this paper, a temperature dependent acoustic receiving characteristics of underwater acoustic sensor is studied by theoretical and experimental investigations. Two different types (low mid frequency sensor and high frequency sensor) of underwater acoustic sensors are designed with different configuration of baffle and conditioning plate. The temperature dependent characteristics of the acoustic sensors are investigated within the temperature range from $-2^{\circ}C$ to $35^{\circ}C$. The material properties of the piezoelectric ceramics, molding and baffle, which are the primary materials of the acoustic sensors, are measured with temperature change. The temperature dependent RVS (Receiving Voltage Sensitivity) characteristics of the acoustic sensors are simulated by using the measured material properties. The RVS changes of the acoustic sensors are measured by changing temperature in the watertank where the acoustic sensors are installed. The measured and the simulated data show that the temperature dependent characteristics of the acoustic sensors are mainly dependent for the sound speed changes of the molding material.