• 한국신재생에너지학회:학술대회논문집
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• 한국신재생에너지학회 2011년도 춘계학술대회 초록집
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• pp.56.2-56.2
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• 2011

As rotor blade of a wind turbine becomes larger to satisfy the economic efficiency for offshore wind farm, the numerical analysis considering wind profile is getting emphasized. In this paper, the study for the power characteristic of a wind turbine is carried out using NREL phase VI wind turbine applied wind profile. The experimental data of NASA Ames wind tunnel for inflow velocity 7m/s is used and the numerical result is obtained by using CFD commercial solver(FLUENT).

• 전력전자학회:학술대회논문집
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• 전력전자학회 2006년도 전력전자학술대회 논문집
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• pp.191-193
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• 2006

The various wind turbines have been designed and developed for the century. The precision design of the blade and turbine system considering the wind circumstance is required for the high efficiency. In this paper, we investigated the output characteristics of the horizontal and vertical wind turbine related to the wind velocity. Furthermore we will intend to design the wind turbine blade adapted the urban wind circumstance.

• 한국지진공학회논문집
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• 제24권5호
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• pp.219-232
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• 2020

The slip-weakening model developed by Ohnaka and Yamashita is extended over the breakdown zone by equating the scaling relationships for the breakdown zone and the whole rupture area. For the extension, the study uses the relationship between rupture velocity and radiation efficiency, which was derived in the theory of linear elastic fracture mechanics, and the definition of f_max given in the specific barrier model proposed by Papageorgiou and Aki. The results clearly show that the extended scaling relationship is governed by the ratio of rupture velocity to S wave velocity, and the velocity ratio can be determined by the ratio of characteristic frequencies of a Fourier amplitude spectrum, which are corner frequency, f_c, and source-controlled cut-off frequency, f_max, or vice versa. The derived relationship is tested by using the characteristic frequencies extracted from previous studies of more than 130 shallow crustal events (focal depth less than 25 km, M_W 3.0~7.5) that occurred in Japan. Under the assumption of a dynamic similarity, the rupture velocity estimated from f_max/f_c and the modified integral timescale give quite similar scale-dependence of the rupture area to that given by Kanamori and Anderson. Also, the results for large earthquakes show good agreement to the values from a kinematic inversion in previous studies. The test results also indicate the unavailability of the spectral self-similarity proposed by Aki because of the scale-dependent rupture velocity and the rupture velocity-dependent f_max/f_c; however, the results do support the local similarity asserted by Ohnaka. It is also remarkable that the relationship between the rupture velocity and f_max/f_c is quite similar to Kolmogorov's hypothesis on a similarity in the theory of isotropic turbulence.

• 한국추진공학회지
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• 제17권5호
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• pp.37-46
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• 2013

2상유체 동축형 다공성재 분사기는 중심포스트에서 분사되는 액체제트 주위로 형성된 다공성재 실린더의 내부 표면에서 기체를 반경방향으로 분사한다. 동축형 다공성재 분사기의 추진제 혼합비에 따른 연소성능을 분석하기 위하여 에탄올/아산화질소 추진제를 사용한 단일 축소형 분사기의 연소시험이 수행되었으며, 수집된 데이터 및 계산된 성능인자들에 대하여 불확실도 해석이 이루어졌다. 연소시험에 의한 추진제 혼합비에 따른 특성속도 경향은 CEA 이론값과 유사하였으나 최대값을 가지는 혼합비 영역이 이론혼합비영역에 가까웠다. 특성속도효율은 산화제 과잉 영역으로 갈수록 더 높게 나타났다.

• 한국대기환경학회지
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• 제22권5호
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• pp.693-700
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• 2006

The important factor for the development of burner is the achievement of low emissions with maintaining combustibility. In case of maintaining high temperature flame and excess air to increase the combustibility, it is possible to achieve high combustion efficiency, due to the reduction of UHC(unborn hydrocarbon), carbon monoxide and soot. However, it is difficult to reduce the thermal NOx produced in the high temperature flame. To solve this problem, we developed externally oscillated oil burner which is possible for the high efficiency combustion and low NOx emission, simultaneously. The experiment of flame characteristics and NOx reduction were achieved according to the variation of frequency, amplitude and air velocity. Frequency, amplitude and air velocity are the most important parameter. The optimum operating conditions are frequency 1,900 Hz, amplitude 3 $V_{pp.}$ and air velocity 6.8 m/s. Reduction of NOx and CO are 47% and 22%, respectively.

• 대한기계학회논문집B
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• 제26권2호
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• pp.201-210
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• 2002

Experiments were done for performance and flow characteristics of a counter-rotating axial flow fan. Performance curves of a counter-rotating axial flow fan were obtained and compared by varying the blade pitch angles. The fan characteristic curves were obtained following the Korean Standard Testing Methods for Turbo Fans and Blowers (KS B 6311). The fan flow characteristics were measured using a five-hole probe and a slanted hot-wire. The velocity profiles between the hub and tip of the fans were measured and analyzed at the peak efficiency point. The peak efficiency of the counter-rotating axial flow fan was improved about 15% respectively, compared with the single rotating axial fan. The single rotating axial flow fan showed relatively law efficiency due to the swirl velocities behind rotor exit which produced pressure losses. The counter-rotating axial flow fan showed that the swirl velocity generated by the front rotor was eliminated by the rear rotor and the associated dynamic pressure is recovered in the from of the static pressure rise.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2005년도 제25회 추계학술대회논문집
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• pp.220-223
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• 2005

본 연구에서는 러시아, 미국, 유럽, 일본의 가스발생기 사이클 엔진 시스템 설계인자를 조사하여 비교 검토하였다. 연소기의 특성속도, 연소기 분사기 차압, 터보펌프 토출압, 펌프효율, 터빈의 비출력 등의 설계인자를 비교한 결과 연소기의 특성속도는 1700-1770 m/s, 분사기차압은 4-10bar, 터보 펌프 토출압은 연소기 압력의 120-230%, 펌프효율은 60-80%, 터빈의 비출력은 $0.28-0.58MW{\cdot}s/kg$의 범위에 있다. 터빈 입구의 가스온도는 터빈의 비출력과 밀접한 관련이 있으며 터빈재질로 인한 한계를 고려하여 결정되어야 한다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2009년도 제33회 추계학술대회논문집
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• pp.511-514
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• 2009

본 연구에서는 경사진 그레인 포트 형상을 가진 고체 연료를 사용한 하이브리드 로켓의 연소 특성을 실험적으로 고찰하였다. 수렴 형상의 그레인 포트를 가지는 연료를 사용함으로써 경사각이 없는 연료에 비해 후퇴율을 17.5% 증가시킬 수 있었으나 확산 형상 연료에서는 후퇴율의 차이가 없었다. 또한 수렴 형상을 사용한 경우 특성속도 효율이 증가하였으며 이를 통해 하이브리드 로켓 연료에서 수렴 형상의 그레인 포트가 연소 효율 및 성능을 개선하는데 효과적임을 확인하였다.

• 한국추진공학회지
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• 제24권1호
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• pp.9-16
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• 2020

200 N급 기체메탄/액체산소 소형로켓엔진의 성능시험평가 수행되었다. 산화제 공급압이 증가함에 따라 연소압과 추력이 증가하였으며, 이에 따라 비추력과 특성속도 및 그 효율이 증가하였다. 특성속도는 약 90%의 성능효율로 측정되었다. 시험조건의 연소실 종횡비 변화는 추력성능에 영향을 미치지 않았다. 또한, 시험결과의 신뢰도 확보를 위하여 불확도평가를 수행하였다.

• 한국항공운항학회지
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• 제19권1호
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• pp.7-14
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• 2011

In this study, the measurement uncertainty of combustion experimental system and experimental parameters for hybrid rocket were evaluated by B type evaluation method. The measurement uncertainty of all experimental parameters was lower than 3%. The highest value of expanded uncertainty was characteristic velocity efficiency with 2.83% and the expanded uncertainty of regression rate which is the design and performance parameter was indicated to 0.03%. These results shown that the reliability of hybrid combustion system was located within allowed limits.