• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2007년도 제29회 추계학술대회논문집
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• pp.89-92
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• 2007

본 연구는 원형 용기에서 배수시 배수구멍의 위치가 중심선에서 벗어난 정도에 따른 배수율과 유동장의 변화를 이해하기 위하여 배수위치의 변화에 따른 배수흐름의 특성을 연구하였다. 이 연구의 목적은 서로 다른 위치의 배수구가 와류생성을 억제하는 원리에 대해 이해는 것이다. 원형 용기의 유동장을 가시화하기 위하여 PIV기법을 사용하였다. 그리고 배수가 있을 때와 없을 때에 대해, 각각 수직방향과 수평방향에서 결과를 얻었다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2004년도 제22회 춘계학술대회논문집
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• pp.634-643
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• 2004

In this paper are presented a concept of a new supersonic air inlet, which is designated a Multi-Row Disk (MRD) inlet, aiming at performance improvement under off-design conditions, and results of wind tunnel tests examined performance characteristics of the MRD inlet. The MRD inlet is frequently called ‘a skeleton inlet’ because of its appearance. The performance of a conventional axisymmetric inlet with a solid center body (spike) deteriorates under off-design Mach number conditions. It is due to the fact that total pressure recovery (TPR) governed by the throat area of inlet and mass capture ratio (MCR) governed by an incidence position of an oblique shock from the spike tip into the cowl can not be controlled independently in such air inlet. The MRD inlet has the spike that is composed of a tip cone and several disks arranged downstream of it, based on the experimental fact that several deep cavities on a conical surface have little negative effect on the boundary layer growth. The overall spike length of the MRD inlet is adjustable to the given flight speed by changing space between disks so that a spillage flow can be controlled independently from controlling the throat area. It could be made clear from the result of wind tunnel tests that the MRD inlet improves TPR by 10% compared with a conventional inlet with a solid spike under off-design conditions.