• 제목/요약/키워드: aerodynamic load

검색결과 236건 처리시간 0.024초

고도 보정용 E-D 노즐의 추력 특성에 대한 수치해석 연구 (Numerical Study on Thrust Characteristics of an E-D Nozzle for Altitude Compensation)

  • 황희성;허환일
    • 한국추진공학회지
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    • 제20권3호
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    • pp.87-95
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    • 2016
  • 본 논문에서는 E-D 노즐을 설계하여 고도 보정에 대한 효과와 Throttling에 대한 가능성 연구를 수행하였다. 고도 보정에 대한 효과를 확인하기 위하여 연소실 압력을 일정하게 유지하며, 총 3가지(해수면, 고도 10 km, 고도 16 km)의 외부 대기환경 조건을 이용하여 해석적 연구를 수행하였다. 그 결과 고도가 상승할수록 유효 노즐 출구 면적 역시 점점 증가하였으며 이로 인하여 추력도 증가하였다. 또한 Throttling에 대한 가능성을 파악하기 위하여 핀틀의 위치를 연소실 쪽으로 후진시켜 노즐 목 면적을 작게 모델링하여 해석적 연구를 수행하였다. 일반적인 핀틀 추력기와 동일하게 노즐 목 면적이 줄어들수록 연소실 압력이 상승하며 추력 역시 증가하였다.

능동 탭 로터 모델링 및 BVI 소음 저감 특성 해석 (Modeling of a Rotor System Incorporating Active Tab and Analysis of BVI Noise Reduction Characteristics)

  • 김도형;강희정;위성용;김승호
    • 한국항공우주학회지
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    • 제41권11호
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    • pp.855-864
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    • 2013
  • 능동 탭은 BVI 소음 저감을 위한 능동제어 기술 중 하나이며, 이를 이용한 소음 저감효과에 대한 해석은 기술 개발에 있어서 매우 중요한 과정의 하나이다. 능동 탭의 소음저감 성능 분석을 위하여 모델 로터시스템에 대한 구조 설계를 수행하고 CFD 해석을 통해 에어포일 공력 데이터를 생성하였으며, 이를 이용하여 통합해석 프로그램인 CAMRAD II 모델을 구성하였다. 하강 비행 상태에서 능동 탭을 HHC 방법으로 작동할 경우 로터에서 발생되는 공력 하중을 CAMRAD II를 이용하여 계산하고, 이에 따른 BVI 소음 변화를 자체 소음해석 프로그램으로 계산하였다. 능동 탭의 작동 길이 및 제어 위상의 변화에 따른 소음해석 결과 최대 -3.3dB의 BVI 소음 저감 효과를 얻을 수 있었다.

Study of random characteristics of fluctuating wind loads on ultra-large cooling towers in full construction process

  • Ke, S.T.;Xu, L.;Ge, Y.J.
    • Wind and Structures
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    • 제26권4호
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    • pp.191-204
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    • 2018
  • This article presents a study of the largest-ever (height = 220 m) cooling tower using the large eddy simulation (LES) method. Information about fluid fields around the tower and 3D aerodynamic time history in full construction process were obtained, and the wind pressure distribution along the entire tower predicted by the developed model was compared with standard curves and measured curves to validate the effectiveness of the simulating method. Based on that, average wind pressure distribution and characteristics of fluid fields in the construction process of ultra-large cooling tower were investigated. The characteristics of fluid fields in full construction process and their working principles were investigated based on wind speeds and vorticities under different construction conditions. Then, time domain characteristics of ultra-large cooling towers in full construction process, including fluctuating wind loads, extreme wind loads, lift and drag coefficients, and relationship of measuring points, were studied and fitting formula of extreme wind load as a function of height was developed based on the nonlinear least square method. Additionally, the frequency domain characteristics of wind loads on the constructing tower, including wind pressure power spectrum at typical measuring points, lift and drag power spectrum, circumferential correlations between typical measuring points, and vertical correlations of lift coefficient and drag coefficient, were analyzed. The results revealed that the random characteristics of fluctuating wind loads, as well as corresponding extreme wind pressure and power spectra curves, varied significantly and in real time with the height of the constructing tower. This study provides references for design of wind loads during construction period of ultra-large cooling towers.

A comparison of the forces on dome and prism for straight and tornadic wind using CFD model

  • Yousef, Majdi A.A.;Selvam, Panneer R.;Prakash, Jai
    • Wind and Structures
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    • 제26권6호
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    • pp.369-382
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    • 2018
  • Tornadoes are vertical swirling air formed because of the existence of layers of air with contrasting features of temperature, wind flow, moisture, and density. Tornadoes induce completely different wind forces than a straight-line (SL) wind. A suitably designed building for an SL wind may fail when exposed to a tornado-wind of the same wind speed. It is necessary to design buildings that are more resistant to tornadoes. In tornado-damaged areas, dome buildings seem to have less damage. As a dome structure is naturally wind resistant, domes have been used in back yards, as single family homes, as in-law quarters, man caves, game rooms, storm shelters, etc. However, little attention has been paid to the tornadic wind interactions with dome buildings. In this work, the tornado forces on a dome are computed using Computational Fluid Dynamics (CFD) for tornadic and SL wind. Then, the interaction of a tornado with a dome and a prism building are compared and analyzed. This work describes the results of the tornado wind effect on dome and prism buildings. The conclusions drawn from this study are illustrated in visualizations. The tornado force coefficients on a dome building are larger than SL wind forces, about 120% more in x- and y-directions and 280% more in z-direction. The tornado maximum pressure coefficients are also higher than SL wind by 150%. The tornado force coefficients on the prism are larger than the forces on the dome, about 100% more in x- and y-directions, and about 180% more in z-direction. The tornado maximum pressure coefficients on prism also are greater those on dome by 150% more. Hence, a dome building has less tornadic load than a prism because of its aerodynamic shape.

ADAMS를 이용한 항공기 착륙장치 작동 동적거동 해석 (An operational analysis and dynamic behavior for a landing gear system using ADAMS)

  • 최섭;권혁범;정상준;정창래;성덕용
    • 한국항공우주학회지
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    • 제31권6호
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    • pp.110-117
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    • 2003
  • 착륙장치 시스템의 올림/내림 작동특성은 다양한 설계변수, 운용조건 및 환경조건에 따라 변화한다. 최소한의 작동공간 및 성능 요구조건을 만족하기 위하여, 착륙장치 시스템은 관련계통의 영향성을 고려하여 기구학적/동역학적 작동해석이 요구된다. 본 연구에서는 T-50 착륙장치를 모델로 ADAMS를 이용하여 착륙장치 작동에 따른 동적거동을 해석할 수 있는 프로그램을 개발하였다. 설계변수 설정, 유압 압력/유량의 관계 정의, 운동방정식을 유도하여 공력하중, 기동하중, 온도의 영향에 대한 착륙장치 및 덮개문의 정상/비상 작동 동적거동 해석결과를 제시하고 분석하였다. 이러한 해석결과를 바탕으로 향후 새로운 착륙장치 개발시 범용적인 해석이 용이할 뿐만 아니라 지상/비행시험의 문제점 발생시 고장탐구 해결에 활용할 수 있다.

다단 마이크로터빈에서 단수 변화에 따른 터빈의 성능에 관한 실험적연구 (An Experimental Study of the Performance Characteristics on a Multi-Stage Micro Turbine with Various Stages)

  • 조종현;조수용;최상규
    • 한국항공우주학회지
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    • 제33권12호
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    • pp.76-82
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    • 2005
  • 본 연구에서는 축류형 마이크로터빈의 단 수를 단 단에서부터 최대 6단까지 변경하면서 각 단에서의 공력특성을 측정하였다. 실험에 사용된 마이크로터빈은 터빈입구에서 유량계수가 2.0, 부하계수가 3.25이며 유로의 평균직경이 25.8mm인 소형 축류형 다단터빈이 적용되었다. 정익과 동익의 솔리디티는 0.67~0.75 범위의 값이 적용되었으며 입구에 일정한 질유량과 전압력으로 조정한 후에 터빈의 부하를 변경하면서 탈설계 영역에서의 공력특성을 측정하였다. 본 실험에서는 단 당 최대 2kW/kg/sec의 비출력이 얻어졌으나 단수의 증가에 따라 비출력의 증가폭은 다소 완화되었으며, 토오크의 경우는 단수가 증가되면서 낮은 회전수 영역에서는 토오크의 증가폭이 일정하나 높은 회전수영역에서는 토오크의 증가폭이 둔화되었다. 블레이드의 높이에 비하여 팁간격의 영향이 크므로 터빈의 효율은 낮으나 단 수의 증가에 따라 증가가 가능하다.

유체-구조 연성해석을 이용한 원심압축기 운전익단간극과 성능 예측 (Study on the Performance of a Centrifugal Compressor Using Fluid-Structure Interaction Method)

  • 이호림;김창희;양장식;손창민;황윤제;정진희
    • 대한기계학회논문집B
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    • 제40권6호
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    • pp.357-363
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    • 2016
  • 본 연구에서는 날개 두께 분포가 다른 두 임펠러를 이용하여 유체-구조 연성해석을 통해 운전익단간극을 예측하고 임펠러의 변형이 성능에 미치는 영향에 대해 연구하였다. 임펠러는 작동조건에서 작용하는 원심력, 압력, 열 하중의 영향으로 변형이 발생하게 된다. 이로 인해 초기 설계된 익단간극이 비균일하게 변화하는 것을 확인하였다. 특히 임펠러 날개의 선단과 후단에서 가장 큰 익단간극 감소가 발생하였으며, 이로인해 간극누설유동이 19.4% 감소하였다. 또한 운전조건에서 익단간극 감소로 간극누설 유량이 감소하면서 효율은 0.72% 증가하는 것을 확인하였다. 원심압축기 작동조건에서의 정확한 운전익단간극의 예측과 익단간극의 변화가 성능에 미치는 영향에 대해서 확인하였다.

디젤연소가능 청정연료(ULSD, Bio-Diesel, DME)엔진의 극미세입자 정량화 및 촉매 영향 (Characteristics of Nano-particle Emitted by Auto-ignited Engine with ULSD, Bio-diesel and DME Fuel and Effects of Oxidation Catalyst on Its Reduction)

  • 이진욱;배충식
    • 한국자동차공학회논문집
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    • 제17권3호
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    • pp.81-89
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    • 2009
  • In this experimental study, the effects of clean alternative fuels compatible with diesel combustion on nano-sized particle emission characteristics were investigated in a 0.5L auto-ignited single-cylinder engine with a compression ratio of 15. Because the number concentration of nano-sized particles emitted by automotive engine, that are suspected of being hazardous to human health and environment, might increase with engine fuel considerably and recently attracted attention. So a ultra-low sulfur diesel(ULSD), BD100(100% bio-diesel) and Di-Methyl Ether(DME) fuels used for this study. And, as a particle measuring instrument, a fast-response particle spectrometer (DMS 500) with heated sample line was used for continuous measurement of the particle size and number distribution in the size range of 5 to 1000nm (aerodynamic diameter). As this research results, we found that this measurements involving the large proportion of particles under size order of 300nm and number concentration of $4{\times}10^9$ allowed a single or bi-modal distribution to be found at different engine load conditions. Also the influence of oxygen content in fuel and the catalyst could be a dominant factor in controlling the nano-sized particle emissions in auto-ignited engine.

공기저항 저감을 위한 컨테이너선 상부구조물 형상설계 및 성능평가 (Design and Performance Evaluation of Superstructure Modification for Air Drag Reduction of a Container Ship)

  • 김윤식;김광수;정성욱;정승규;반석호;김진
    • 대한조선학회논문집
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    • 제52권1호
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    • pp.8-18
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    • 2015
  • Reduction of the fuel oil consumption and corresponding greenhouse gas exhausted from ships is an important issue for today's ship design and shipping. Several concepts and devices on the superstructure of a container ship were suggested and tested in the wind tunnel to estimate the air drag reduction. As a preliminary performance evaluation, air drag contributions of each part of the superstructure and containers were estimated based on RANS simulation respectively. Air drag reduction efficiency of shape modification and add-on devices on the superstructure and containers was also estimated. Gap-protectors between containers and a visor in front of upper deck were found to be most effective for drag reduction. Wind tunnel tests had been carried out to confirm the drag reduction performance between the baseline(without any modification) configuration and two modified superstructure configurations which were designed and chosen based on the computation results. The test results with the modified configurations show considerable aerodynamic drag reduction, especially the gap-protectors between containers show the largest reduction for the wide range of heading angles. RANS computations for three configurations were performed and compared with the wind tunnel tests. Computation result shows the similar drag reduction trend with experiment for small heading angles. However, the computation result becomes less accurate as heading angle is increasing where the massively separated flow is spread over the leeward side.

Embossed Structural Skin for Tall Buildings

  • Song, Jin Young;Lee, Donghun;Erikson, James;Hao, Jianming;Wu, Teng;Kim, Bonghwan
    • 국제초고층학회논문집
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    • 제7권1호
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    • pp.17-32
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    • 2018
  • This paper explores the function of a structural skin with an embossed surface applicable to use for tall building structures. The major diagrid system with a secondary embossed surface structure provides an enhanced perimeter structural system by increasing tube section areas and reduces aerodynamic loads by disorienting major organized structure of winds. A parametric study used to investigate an optimized configuration of the embossed structure revealed that the embossed structure has a structural advantage in stiffening the structure, reducing lateral drift to 90% compared to a non-embossed diagrid baseline model, and results of wind load analysis using computational fluid dynamics, demonstrated the proposed embossed system can reduce. The resulting undulating embossed skin geometry presents both opportunities for incorporating versatile interior environments as well as unique challenges for daylighting and thermal control of the envelope. Solar and thermal control requires multiple daylighting solutions to address each local façade surface condition in order to reduce energy loads and meet occupant comfort standards. These findings illustrate that although more complex in geometry, architects and engineers can produce tall buildings that have less impact on our environment by utilizing structural forms that reduce structural steel needed for stiffening, thus reducing embodied $CO^2$, while positively affecting indoor quality and energy performance, all possible while creating a unique urban iconography derived from the performance of building skin.