• 제목/요약/키워드: Instability Condition

검색결과 504건 처리시간 0.02초

KSR-III 액체 로켓엔진 설계점 연소시험

  • 김승한;조규식;한영민;서성현;문일윤;이광진;김종규;설우석;이수용
    • 항공우주기술
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    • 제2권1호
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    • pp.164-170
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    • 2003
  • KSR-III 주 엔진에서 발생한 연소불안정 방지를 위한 필름 냉각방식의 내열재 배플을 장착한 확대비 5.04의 엔진의 40초 연소시험을 수행하였다. 시험 조건은 KRS-III 새로 설정한 설계점 조건으로 산화제 공급유량 42.04kg/sec, 연료공급 유량 17.96kg/s를 공급조건으로 설정하였다. 연소불안정을 방지하기 위해 필름 냉각방식의 내열재 배플을 장착한 EM#11호기 설계점 연소시험을 한 결과 설정 연소시간인 40초 동안 연소불안정이 발생하지 않았다.

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분포접선력을 받는 탄성지지된 보의 동적 불안정 (Dynamic Instability of Elastically Restrained Beams under Distributed Tangential Forces)

  • 류봉조;김인우;이규섭;임경빈;최봉문
    • 한국정밀공학회지
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    • 제15권10호
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    • pp.140-147
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    • 1998
  • The dynamic behavior of elastically restrained beams under the action of distributed tangential forces is investigated in this paper. The beam, which is fixed at one end, is assumed to rest on an intermediate spring support. The governing equations of motion are derived from the energy expressions, and the finite element formulation is employed to calculate the critical distributed tangential force. Jump phenomena for the critical distributed tangential force and instability types are presented for various spring stiffnesses and support positions. Stability maps are generated by performing parametric studies to show how the distributed tangential forces affect the frequencies and the stability of the system considered. Through the numerical simulations, the following conclusioils are obtained: (i) Only flutter type instability exists for the dimensionless spring stiffness K $\leq$ 97, regardless of the position of the spring support. (ii) For the dimensionless spring stiffness K $\leq$ 98, the transition from flutter to divergence occurs at a certain position of the spring support, and the transition position moves from the free end to the free end of the beam as the spring stiffness increases. (iii) For K $\leq$ 10$^{6}$ the support condition can be regarded as a rigid support condition.

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소득의 불안정성과 부동산가격변동에 대한 태도 및 부동산보유비중 조정의향 간의 관련성 (The Relationship between Income Instability and Psychological Condition of Real Estate Price Changes and Willingness to Adjust Real Estate Holding Ratio)

  • 이찬호
    • 한국융합학회논문지
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    • 제11권12호
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    • pp.199-205
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    • 2020
  • 오늘날 부동산 특히 주택과 관련한 많은 정부정책이 발표됨에 따라 주택시장에서의 가격에 대한 관심이 매우 높아졌다. 이에 본 연구에서는 소득의 불안정성과 부동산가격변동에 대한 심리상태와 부동산보유비중의 조정의향 간의 관련성을 분석하여 정부정책의 실효가능성을 살펴보고자 한다. 먼저 선행연구 검토를 통해 주요 변수를 추출하고 설문조사를 통해 자료를 수집하여 경로분석을 실시하였다. 분석결과 현재의 소득의 불안정성은 부동산가격변동에 대한 태도에 음(-)의 영향을, 부동산보유비율조정의향에는 양(+)의 영향을 미쳤으나, 부동산가격변동에 대한 태도가 부동산보유비율조정의향에는 통계적으로 유의한 영향을 미치지 않았다. 이에 연령대와 부양가족 수를 각각 2분하여 집단간 차이분석을 실시하였으며, 분석결과 부동산보유비중 의사결정은 연령대가 높은집단과 부양가족수가 많은집단에서 소득불안정성과 부동산가격변화에 대한 태도에 의해 영향을 받아 집단 간 차이를 보였다. 본 분석 결과는 정부의 부동산 정책 수립방향 설정과 각 가계의 부동산 관련 의사결정에 기초자료로 활용하는데 도움이 될 것이다. 한편 본 연구는 횡단면분석만을 실시한 한계점을 갖고 있으며 향후에는 시계열적 변화와 지역간 인식의 차이 등을 분석하고자 한다.

스월 분사와 삽입연료에 의한 하이브리드 로켓 연소의 저주파수 연소불안정 조절 (Controlling Low Frequency Instability in Hybrid Rocket Combustion With Swirl Injection and Fuel Insert)

  • 현원정;이창진
    • 한국항공우주학회지
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    • 제49권2호
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    • pp.139-146
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    • 2021
  • 하이브리드 로켓 연소에서 산화제 스월 분사는 회전방향 속도성분이 경계층 유동에 영향을 미쳐 연소안정화에 기여한다. 그러나 스월 강도가 증가할수록 연소성능을 과도하게 변화시키는 문제점이 나타난다. 따라서 참고문헌[7]의 삽입연료와 함께 사용하여 연소성능 변화를 최소화 하면서 연소불안정 억제를 시도하였다. 이를 위해, 일련의 실험을 계획하여 스월 강도와 삽입연료 위치를 변화하며 연소불안정의 발생과 연소성능 변화를 관찰하였다. 실험결과, 스월 각 6°, 삽입연료 위치 310 mm 조합에서 연소불안정이 억제되었으며 연소압력, O/F 비 그리고 연료 후퇴율 등의 변화가 최소인 것으로 확인하였다. 또한 고주파수 대역의 압력진동(p')와 열방출진동(q')의 위상차가 π/2로 음의 결합을 형성하도록 연소조건을 유지하는 것이 저주파수 연소불안정 발생을 억제하는 필요충분조건임을 재확인하였다.

확산화염의 진동불안성의 기원에 대해서 (On the Origin of Oscillatory Instabilities in Diffusion Flames)

  • 김종수
    • 한국연소학회지
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    • 제10권3호
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    • pp.25-33
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    • 2005
  • Fast-time instability is investigated for diffusion flames with Lewis numbers greater than unity by employing the numerical technique called the Evans function method. Since the time and length scales are those of the inner reactive-diffusive layer, the problem is equivalent to the instability problem for the $Li\tilde{n}\acute{a}n#s$ diffusion flame regime. The instability is primarily oscillatory, as seen from complex solution branches and can emerge prior to reaching the upper turning point of the S-curve, known as the $Li\tilde{n}\acute{a}n#s$ extinction condition. Depending on the Lewis number, the instability characteristics is found to be somewhat different. Below the critical Lewis number, $L_C$, the instability possesses primarily a pulsating nature in that the two real solution branches, existing for small wave numbers, merges at a finite wave number, at which a pair of complex conjugate solution branches bifurcate. For Lewis numbers greater than $L_C$, the solution branch for small reactant leakage is found to be purely complex with the maximum growth rate found at a finite wave number, thereby exhibiting a traveling nature. As the reactant leakage parameter is further increased, the instability characteristics turns into a pulsating type, similar to that for L < $L_C$.

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The effect of ion to electron mass ratio on Ion beam driven instability and ion holes by PIC simulation

  • 홍진희;이은상;민경욱
    • 천문학회보
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    • 제37권1호
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    • pp.92.2-92.2
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    • 2012
  • Previous simulations posed a problem that they used reduced ion to electron mass ratios to save computation time. It was assumed that ion and electron dynamics are sufficiently separated, but it was not clearly verified. In this study, we examine the effect of ion to electron mass ratios on the generation of ion holes by ion beam driven instability. Ion holes are generated via electron holes in an applied electric field with the given initial condition. First, the ion acoustic instability is excited and nonlinearly develops. After the ion acoustic instability nonlinearly develops, the ion two-stream instability is excited and develops into ion holes. This implies that the previously suggested ion beam driven instability is strongly affected by the coupling between ions and electrons and the ion to electron mass ratio is important on the development of the instability. The energy transition and detail variation is different as reduced mass ratio under the same observation value based on FAST satellite. Although, the parameters are rescaled by conserving the kinetic energy to obtain the proper results, the nonlinear evolution is not perfectly identical.

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모형 가스터빈 연소기내 연소불안정성에 대한 실험적 연구 (An Experimental Study on Combustion Instability Mechanism in a Dump Gas Turbine Combustor)

  • 이연주;이종호;전충환;장영준
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 추계학술대회논문집B
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    • pp.853-858
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    • 2001
  • The knowledge of flame structure is essential for control of combustion instability phenomena. Some results of an experimental study on mechanism of naturally occurring combustion oscillations with a single dominant frequency are presented. Tests were conducted in a laboratory-scale dump combustor at atmospheric pressure. Sound level meter was used to track the pressure wave inside the combustor. The observed instability was a longitudinal mode with a frequency of $\sim341.8Hz$. Instability map was obtained at the condition of inlet temperature of $360^{\circ}C$, mean velocities of $8.5\sim10.8m/s$ and well premixed mixture. It showed that combustion instability was susceptible to occur in the lean conditions. In this study, unstable flame was observed from stoichiometric to 0.7 in overall equivalence ratio. At selected unstable conditions, phase-resolved OH chemiluminescence images were captured to investigate flame structure with various mean velocities. As mean velocity is increased, the flame grows and global heat release was changed. Due to these effects, combustion instability can be maintained at more lean air-fuel ratio. Also, these results give an insight to the controlling mechanism for an increasing heat release at maximum pressure.

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이산형 열-음향 모델을 이용한 부하 변동시 가스터빈 연소 불안정 특성 (Combustion Instability of Gas Turbine with Segmented Dynamic Thermo-Acoustic Model under Load Follow-Up)

  • 정지웅;한재영;정진희;유상석
    • 한국수소및신에너지학회논문집
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    • 제29권5호
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    • pp.538-548
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    • 2018
  • The thermo-acoustic instability in the combustion process of a gas turbine is caused by the interaction of the heat release mechanism and the pressure perturbation. These acoustic vibrations cause fatigue failure of the combustor and decrease the combustion efficiency. This study is to develop a segmented dynamic thermo-acoustic model to understand combustion instability of gas turbine. Therefore, this study required a dynamic analysis rather than static analysis, and developed a segmented model that can analyze the performance of the system over time using the Matlab/Simulink. The developed model can confirm the thermo-acoustic combustion instability and exhaust gas concentration in the combustion chamber according to the equivalent ratio change, and confirm the thermo-acoustic combustion instability for the inlet temperature and the load changes. As a result, segmented dynamic thermo-acoustic model has been developed to analyze combustion instability under the operating condition.

Effect of Ankle Taping Type and Jump Height on Balance during Jump Landing in Chronic Ankle Instability

  • Kim, Mikyoung;Kong, Byungsun;Yoo, Kyungtae
    • 국제물리치료학회지
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    • 제11권2호
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    • pp.2077-2089
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    • 2020
  • Background: Chronic ankle instability is a common injury that decreases balance and negatively affects functional movements, such as jumping and landing. Objectives: To analyze the effect of taping types and jump heights on balance with eyes open and closed during jump landings in chronic ankle instability. Design: Within-subject design. Methods: The study involved 22 patients with chronic ankle instability. They performed both double-leg and single-leg drop jump landings using three conditions (elastic taping, non-elastic taping, and barefoot) on three different jump platforms (30, 38, and 46 cm). Balance was measured using the Romberg's test with eyes open and closed. Results: Interaction effect was not statistically significant. Balance with eyes open and closed was significantly improved in both the elastic taping and non-elastic taping conditions compared to the barefoot condition. There was no significant difference according to the jump height. Conclusion: Individuals with chronic ankle instability demonstrated increased balance ability with eyes open and closed when jump landing. Elastic taping and non-elastic taping on the ankle joint can positively affect balance during landing in individuals with chronic ankle instability.

저널 베어링의 동기화된 선회 운동에 관한 연구 (A Study on Synchronously Whirling Motion of Hydrodynamic Journal Bearings)

  • 김경웅;노병후
    • 대한기계학회논문집A
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    • 제25권9호
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    • pp.1432-1437
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    • 2001
  • In this paper, a control algorithm which is synchronously excitating the bearing with whirl speed of rotor is employed to suppress the whirl instability and unbalance response of the rotor-bearing system. Also, the cavitation algorithm implementing the Jakobsson-Floberg-Olsson boundary condition is adopted to predict cavitation regions in the fluid film more accurately than a conventional analysis with the Reynolds condition. The stabilities and unbalance responses of the rotor-bearing system are investigated for various control gains and phase differences between the bearing and journal motion. It is shown that the unbalance response of the system can be greatly improved by synchronous control of the bearing, and there is an optimum phase difference, which gives the minimum unbalance response of the system, for given operating condition. It is also found that the onset speed of the instability can be greatly increased by synchronous control of the bearing.