• Title/Summary/Keyword: 응답식 압력

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Controlling Factors of Open-Loop Combustion Response to Acoustic Pressures in Liquid Propellant Rocket Engine (강한 압력파동에 구속된 액체 추진제 연소응답의 지배인자)

  • Yoon Woongsup;Lee Gilyong
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2004.10a
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    • pp.267-273
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    • 2004
  • This paper targets to define controlling factors of pressure-coupled combustion response and estimate their effects on droplet evaporation process. Dynamic characteristics of hydrocarbon propellant vaporization perturbed by acoustic pressure are numerically simulated and analyzed. 1-D droplet model including phase equilibrium between two phases is applied and acoustic wave is expressed by harmonic function. Effects of various design factors and acoustic pressure on combustion response are investigated with parametric studies. Results show that driving frequency of acoustic perturbation and ambient pressure have important roles in determining magnitude and phase of combustion response. On the other hand, other parameters such as gas temperature, initial droplet size and temperature, and amplitude of acoustic wave cause only minor changes to magnitude of combustion response. Resultant changes in phase of heat of vaporization and thermal wave in droplet highly influence magnitude and phase of combustion response.

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A Study on the Sloshing Impact Response Analysis for the Insulation System of Membrane Type LNG Cargo Containment System (LNG 탱크 방열구조의 슬로싱 충격 응답 해석법에 관한 연구)

  • Nho, In-Sik;Ki, Min-Seok;Lee, Jae-Man;Kim, Sung-Chan
    • Proceedings of the Computational Structural Engineering Institute Conference
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    • 2011.04a
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    • pp.531-538
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    • 2011
  • To ensure the structural integrity of membrane type LNG tank, the rational assessment of impact pressure and structural responses due to sloshing should be preceded. The sloshing impact pressures acting on the insulation system of LNG tank are typical irregular loads and the structural responses caused by them also very complex behaviors including fluid structure interaction. So it is not easy to estimate them accurately and huge time consuming process would be necessary. In this research, a simplified method to analyze the dynamic structural responses of LNG tank insulation system under pressure time histories obtained by sloshing model test or numerical analysis was proposed. This technique basically based on the concept of linear combination of the triangular response functions which are obtained by the transient response analysis under the unit triangular impact pressure acting on structures in time domain. The validity of suggested method was verified through the example calculations and applied to the structural analysis of real Mark III type insulation system using the sloshing impact pressure time histories obtained by model test.

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Hydroelastic Analysis for a Very Large Floating Structure by Pressure Distribution Method (압력분포법에 의한 초대형 부유식 해양구조물의 유탄성 해석)

  • H.Y. Lee;H. Shin;H.S. Shin;I.K. Park
    • Journal of the Society of Naval Architects of Korea
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    • v.37 no.4
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    • pp.66-74
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    • 2000
  • In this paper, hydroelastic responses of the very large floating structure are studied based on the linear potential theory. A theoretical method is developed to analyze the hydroelastic reponses of very large floating structures(VLFS) using the pressure distribution method and the modal expansion method. The singularities distributed on a zero draft plate at the free surfaces and hydrodynamic pressures are evaluated. The deflections of structure are expanded approximately in terms of natural mode functions of free-free beam. The calculated items are pressure distributions. vertical motions, hydrodynamic coefficients and bending moments of VLFS. The numerical results are compared with those measured by experiments.

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Motion and Wave Transmission Effect on Floating OWC(Oscillating Water Column) Wave Energy Conversion System (진동수주형 파력발전 시스템에서 운동과 파랑회절의 영향)

  • Lee, Sang-moo;Kim Seoung-gun
    • Proceedings of the Korea Committee for Ocean Resources and Engineering Conference
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    • 2001.05a
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    • pp.20-25
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    • 2001
  • 부유식 파랑에너지 변환시스템(Oscillating Water Column)에서 에너지 변환은 입력파와 챔버, 챔버내 공기의 상호작용으로 이루어진다. 이 논문은 파랑에너지를 기계적 운동으로 변환하는 기계적 특성을 해석한다. 단일 진동수 규칙파가 입력되었을 때에 파에 의하여 챔버의 상하운동이 선형적으로 발생하며, 이 상하운동은 챔버내의 압력 변화에 영향을 받는다. 상하운동과 챔버내로 투과한 파, 그리고 챔버내 압력에 의해 발생되는 파에 의해 챔버내의 상대운동을 정하고, 그 상대운동에 의한 공기의 압축 팽창과 온도상승을 근사적 열역학적 방정식으로 해석하여 오리피스를 통한 유량과 압력을 기준으로 에너지 변환요율을 결정하였다. 얻어진 식은 간단하면서도 관련요소의 영향을 전반적으로 표현한다. 개구율 변화에 따른 운동응답을 비교하였다.

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Theoretical Analysis of the Steady Burning Rate for Homogeneous Solid Propellants with Surface Evaporation (표면 증발을 고려한 AP추진제의 정상 연소율 해석)

  • 이창진
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 1998.10a
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    • pp.2-2
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    • 1998
  • 고체 추진제의 연소율(burning rate)은 연소의 동적 기동을 이해할 수 있을 뿐 아니라 추진제의 성능을 판단할 수 있는 중요한 수단이기 때문에 많은 연구가 진행되어 왔다. 특히 AP계의 고체추진제 표면에서는 발열반응인 분해반응(decomposition) 이외에도 기체로 증발되는 증발되는(evaporation or sublimation)이 존재한다. 증발반응으로 인하여 연소율은 외부압력의 변화에 대하여 반응하게 되며 실험적으로 $r_{b}$= a $p^n$의 관계를 보여주고 있다. 즉, 연소율(burning rate)은 연소실 압력 P의 n승에 비례하며 여기서 n은 실험적으로 결정되는 지수이다. 그러나 압력지수 n은 일반적으로 온도와 압력의 함수이기 때문에 실험적으로 이 측정하기는 매우 어려운 일이다. 또한 QSHOD 가정을 사용하여 고체 추진제의 연소 응답함을 해석하기 위해서 추진제의 민감계수(sensitivity parameters)에 관한 관계식이 필요하며 이러한 관계식은 추진제의 정상연소율에 관한 관계식으로부터 얻을 수 있다.다.

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Optimization of Controller Execution Cycle Time for Digital Speed Governor (디지털 조속기용 제어기 실행주기 최적화)

  • Kim, Byoung-Chul;Jung, Chang-Gi;Kim, Jong-An;Choi, In-Kyu;Woo, Joo-Hee
    • Proceedings of the KIEE Conference
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    • 2006.07d
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    • pp.1883-1884
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    • 2006
  • 원자력발전소는 원자로의 증기발생기에서 생산한 증기의 압력으로 터빈발전기를 돌려서 발전을 하고 있다. 터빈속도를 제어하는 디지털식 터빈 조속기는 마이크로프로세서를 기반으로 하는 디지털식 제어기가 널리 사용하고 있으며, 조속기에 사용되는 제어기는 빠른 제어 응답성과 높은 신뢰성을 요구하고 있으므로 제어 프로그램의 실행속도에 따라서 제어의 특성과 질이 좌우 될 수 있다. 디지털식 제어기는 제어프로그램을 순차적으로 반복 실행하며, 중요도에 따라서 몇 개의 그룹으로 나누어 실행 주기를 달리함으로써 제어기의 과도한 부하율을 피하고 있다. 이렇게 함으로써 빠른 제어 응답성과 시스템 안정성을 모두 만족하는 실행주기로 최적화하는 과정이 필요하여 본 시험을 하였으며 이러한 제어특성을 사전에 확인하여 원자력발전소의 아날로그식 조속기를 디지털식 조속기로 개선을 하고자 시험한 사례를 소개한다.

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Dynamic response analysis of vertical pumps (입형펌프의 동적 응답해석)

  • 양보석;김원철;임우섭;권명래
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.13 no.3
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    • pp.362-372
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    • 1989
  • It is important in design of vertical pumps to consider external excitation in addition to rotor vibration due to unbalance. In this study, a model of a vertical pump was developed for the analysis of its dynamic response. The vertical pump was modeled with lumped masses and springs which represent multi-cylindrical and rotor structure. A dynamic simulation program was developed and numerical calculation on the above mentioned problems were carried out.

Measurement and Application of Pressure-Coupled Combustion Response of Solid Propellant with T-Burner (압력파동에 대한 고체추진제의 연소응답함수 측정 및 응용)

  • Lee Gil-Yong;Im Ji-Hwan;Yoon Woong-Sup;Yoo Ji-Chang
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2006.05a
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    • pp.268-271
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    • 2006
  • Combustion response function of a solid propellant is measured and calculated to study and model the feedback process between acoustic waves and combustion field. Standard Pulsed DB/AB method and related one-dimensional approximate analysis of T-burner are used to obtain the response function at a driving natural frequency. The problems related with simultaneous ignition of propellant samples are also mentioned and treated.

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Surface Elevation Recovery Methods from Pressure Gage for Irregular Waves (불규칙파(不規則波에) 대한 압력식(壓力式) 파고계(波高計)의 적용성(適用性)에 관한 연구(研究))

  • Kwon, Jung Gon;Kang, Ju Bok
    • KSCE Journal of Civil and Environmental Engineering Research
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    • v.12 no.4_1
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    • pp.129-136
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    • 1992
  • A precedure for recovering surface displacement from a time series of pressure measured by a pressure gage in a shallow water (that is, FFTM, LCM. IWM) is investigated with respect to a proper cut-off-frequency of a frequency response function for the accurate recovery of wave height and period. The authors examined the applicability of above mentioned three transformation procedures through field observations and laboratory experiments and the following results are obtained. i) The cut-off-frequency of the frequency response function used in FFTM is deeply depend on both the frequency response of the pressure sensor and the water depth at the sensor. In this study, a relatively accurate surface displacement can be recovered when the frequency response function is cut off at the frequency corresponding to kh=3.0 where k is a wave number at the depth of h. The frequency response function in the region higher than the cut-off-frequency is set constant to be the value at the cut-off-frequency. ii) The transformed surface displacements by LCM are affected by the small waves of short periods included in the measured pressure. It is found that pressure variation whose local frequency is higher than kh=1.5 has to be neglected to recover surface displacement sufficiently. iii) In IWM, the linear pressure response function is usually utilized by multiplying a coefficient N which is a function of the frequency (or kh) and takes a value around unity. However, in this study, a constant value of N(=1.0) gives a relatively accurate recovery of surface displacements.

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