• Title/Summary/Keyword: Quasi-Steady Analysis

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Unsteady wind loading on a wall

  • Baker, C.J.
    • Wind and Structures
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    • v.4 no.5
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    • pp.413-440
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    • 2001
  • This paper presents an extensive analysis of unsteady wind loading data on a 18 m long and 2 m high wall in a rural environment, with the wind at a range of angles to the wall normal. The data is firstly analyzed using standard statistical techniques (moments of probability distributions, auto- and cross-correlations, auto- and cross-spectra etc.). The analysis is taken further using a variety of less conventional methods - conditional sampling, proper orthogonal decomposition and wavelet analysis. It is shown that, even though the geometry is simple, the nature of the unsteady flow is surprisingly complex. The fluctuating pressures on the front face of the wall are to a great extent caused by the turbulent fluctuations in the upstream flow, and reflect the oncoming flow structures. The results further suggest that there are distinct structures in the oncoming flow with a variety of scales, and that the second order quasi-steady approach can predict the pressure fluctuations quite well. The fluctuating pressures on the rear face are also influenced by the fluctuations in the oncoming turbulence, but also by unsteady fluctuations due to wake unsteadiness. These fluctuations have a greater temporal and spatial coherence than on the front face and the quasi-steady method over-predicts the extent of these fluctuations. Finally the results are used to check some assumptions made in the current UK wind loading code of practice.

A FLUID TRANSIENT ANALYSIS ON THE PIPE NETWORK OF BIPROPELLANT PROPULSION SYSTEM WITH AN UNSTEADY FRICTION (이원추진제 추진시스템의 배관망에 대한 비정상 마찰을 고려한 과도기유체 해석)

  • Chae, Jong-Won;Han, Cho-Young;Kim, Jung-Hoon;Jun, Hyoung-Yoll
    • 한국전산유체공학회:학술대회논문집
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    • 2010.05a
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    • pp.487-490
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    • 2010
  • A fluid transient analysis on the pipe network of bipropellant propulsion system is conducted through numerical parametric studies in which unsteady friction results are compared with quasi-steady friction results and also show the pressure drop results during the liquid apogee engine firing. The fluid transient analysis program has verified through comparing with the original Zielke model, the full and recursive convolution model and quasi-steady model as a reference. And the pressure drop program also has verified through comparing with results of the well-known program, EPANET2. The bipropellant propulsion system has two different fluids as fuel and oxidizer, and mostly they are hypergolic combination so that the valve opening and closing of the thrusters, that cause the pressure waves, shall take place simultaneously to get proper performance. The different physical properties of the fuel and oxidizer result in the different responsive to the same valve opening and closing. The response results may be helpful to know the characteristics of the bipropellant propulsion system and design it.

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A Linear Stability Analysis of Unsteady Combustion of Solid Propellants (고체추진제 비-정상연소의 선형 안정성해석)

  • 이창진;김성인;변영환
    • Journal of the Korean Society of Propulsion Engineers
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    • v.2 no.1
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    • pp.59-66
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    • 1998
  • The combustion instability analysis of solid propellants is generally done by the simplified governing equations for chemically inert condensed phase region with QSHOD assumption. Since the gas phase and surface reaction layer can be more rapidly relaxed to the external perturbations than the condensed phase, these regions are treated as quasi-steady manner in the analysis. In this paper, the classical ZN(Zeldovic-Novozhilov)approach was re-examined with the presence of radiation augmented burning enhancement in the combustion. Also, the surface reaction was assumed to partially absorb the incident radiant heat fluxes and pass the remaining to the chemically inert condensed phase. As a result of the analysis, the burning rate response function was obtained which consists of a pressure response function and a radiation response function. The response function was shown to be able to predict the results of T-burner tests.

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An Active Auxiliary Quasi-Resonant Commutation Block Snubber-Assisted Three Phase Voltage Source Soft Switching PFC Rectifier using IGBTs

  • Hiraki Eiji;Nakaoka Mutsuo;Sugimoto Shigeyuki;Ogawa Shigeaki
    • Journal of Power Electronics
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    • v.5 no.1
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    • pp.29-35
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    • 2005
  • This paper presents a novel prototype of an active auxiliary quasi-resonant snubber(Auxiliary Quasi-Resonant Commutation Block-Link; ARCB)-assisted three phase voltage source soft switching space voltage vector modulated PFC rectifier, which uses Zero Voltage Soft Switching (ZVS) commutation. The operating principles of this digitally-controlled three phase soft switching PWM-PFC rectifier system with an instantaneous power feedback scheme are illustrated and its steady-state performance is evaluated using computer-aided simulation analysis.

Bidirectional Quasi-Cuk DC/DC Converter with Reduced Voltage Stress on Capacitor and Capability of Changing the Output Polarity

  • Asl, Elias Shokati;Sabahi, Mehran
    • Journal of Electrical Engineering and Technology
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    • v.12 no.3
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    • pp.1108-1113
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    • 2017
  • In this paper, a bidirectional topology for quasi-Cuk dc/dc converter with capability of zero-voltage and zero-current-switching (ZVZCS) is proposed. The bidirectional quasi-Cuk (BQ-Cuk) converter has different voltage and current transfer ratio, reduced voltage stress on capacitor and capability of changing the output polarity in comparison with conventional bidirectional Cuk converter. In this paper, steady-state analysis of the quasi-Cuk converter with capability of ZVZCS in turn-on is presented. Then, critical inductances for transient from this operation to two new operations are calculated. Next, besides values designing of used elements, maximum and minimum value of their current and voltage are calculated. Finally, experimental results to verify the accuracy of the proposed converter in different operating modes are presented.

A Study on the Magnetic Fluid driven by Electromagnetic Force (전자기력에 의한 자성유체의 구동에 관한 연구)

  • Nam Seong-won
    • Journal of computational fluids engineering
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    • v.4 no.2
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    • pp.31-38
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    • 1999
  • Numerical analysis is conducted on the deformation of free surface of magnetic fluid. Steady magnetic fields are induced by a circular current loop. Governing equations of magnetic fields are solved by using the concept of vector potential. The free surface of magnetic fluid is formed by the balance of surface force, gravity, pressure difference, magnetic normal pressure and magnetic body force. The deformations of free surface of magnetic fluid are qualitatively clarified. And, the patterns of steady non-uniform magnetic fields induced by a circular current loop are quantitatively presented. The shape of free surface attained by the polar fluid approach is rougher and higher than that attained by the quasi-steady approach.

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Linear Stability Analysis of Cellular Counterflow Diffusion Flames with Radiation Heat Loss (복사 열손실을 받는 셀모양 대향류 확산화염의 선형 안정성 해석)

  • Lee, Su Ryong
    • Journal of the Korean Society of Combustion
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    • v.18 no.2
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    • pp.42-50
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    • 2013
  • Linear stability analysis of radiating counterflow diffusion flames is numerically conducted to examine the instability characteristics of cellular patterns. Lewis number is assumed to be 0.5 to consider diffusional-thermal instability. Near kinetic limit extinction regime, growth rates of disturbances always have real eigen-values and neutral stability condition of planar disturbances perfectly falls into quasi-steady extinction. Cellular instability of disturbance with transverse direction occurs just before steady extinction. However, near radiative limit extinction regime, the eigenvalues are complex and pulsating instability of planar disturbances appears prior to steady extinction. Cellular instability occurs before the onset of planar pulsating instability, which means the extension of flammability.

Numerical Studies on the Performance Prediction of a Turbopump System for Liquid Rocket Engines (액체로켓용 터보펌프 성능예측에 대한 수치해석적 연구)

  • Choi, Chang-Ho;Lee, Geesoo;Kim, Jinhan;Yang, Soo Seok;Lee, Daesung
    • 유체기계공업학회:학술대회논문집
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    • 2001.11a
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    • pp.264-270
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    • 2001
  • The hydraulic performance analysis of an entire pump system composed of an inducer, impeller, volute and seal for the application on turbopumps is performed using three-dimensional Wavier-Stokes equations. A quasi-steady mixing-plane method is used on the impeller/volute interface to simulate the unsteady interaction phenomena. From this wort the effects of each component on the pump performance are investigated at design and off-design conditions through the analysis of flow structures and loss mechanisms. The computational results are in a good agreement with experimental ones in terms of the headrise and efficiency even though very complex flow structures are present. It is found that the asymmetric pressure distribution along the volute wall constitutes the main reason of the difference between experimental and computational results due to the limitation of the applying the quasi-steady method. Since the volute was found to be over-designed according to the pressure distribution of the volute wall, redesign of the volute has been performed resulting in an improved performance characteristic.

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Numerical Studies on the Performance Prediction of a Turbopump System for Liquid Rocket Engines (액체로켓용 터보펌프 성능예측에 대한 수치해석적 연구)

  • Choi, Chang-Ho;Lee, Gee-soo;Kim, Jin-han;Yang, Soo-Seok;Lee, Dae-sung
    • The KSFM Journal of Fluid Machinery
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    • v.5 no.2 s.15
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    • pp.15-21
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    • 2002
  • The hydraulic performance analysis of an entire pump system composed of inducer, impeller, volute and seal for the application of turbopumps is numerically performed using three-dimensional Navier-Stokes equations. A quasi-steady mixing-plane method is used on the impeller/volute interface to simulate the unsteady interaction phenomena. From this work, the effects of each component on the pump performance are investigated at design and off-design conditions through the analysis of flow structures and loss mechanisms. The computational results are in a good agreement with experimental ones in terms of the headrise and efficiency even though very complex flow structures are present. It is found that the asymmetric pressure distribution along the volute wall constitutes the main reason of the difference between experimental and computational results, due to the limitation of the quasi-steady method. Since the volute was found to be over-designed by the pressure distribution of the volute wall, re-design of the volute has been performed, resulting in an improved performance characteristic.

Load distribution analysis of a sprocket wheel tooth for a low head hydro-turbine power transmission system (저낙차용 수차의 동력전달 스프로켓 휠 이의 하중분포 해석)

  • 강용석;김현수;김현진
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.18 no.5
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    • pp.1087-1095
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    • 1994
  • Chain drive power transmission system was developed for a low head hydro-turbine which generates power by energy transformation on the turbine blades attached to chains. Also, experimental and theoretical analysis for the sprocket wheel tooth load distribution were performed. The tooth load was measured by the specially designed load sensor. It was found that the tooth load distribution for the steady state operation was in good accordance with the quasi-static state results showing the peak load at the final meshing tooth. The trend of the experimental results agreed with the theoretical results based on the spring model analysis and difference in the magnitude of the maximum tooth load was considered to be the effect of the variable spring constant due to the moving contact point between the roller and sprocket wheel tooth.