• Title/Summary/Keyword: Deviation velocity

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On-board Realtime Orbit Parameter Generator for Geostationary Satellite (정지궤도위성 탑재용 실시간 궤도요소 생성기)

  • Park, Bong-Kyu;Yang, Koon-Ho
    • Aerospace Engineering and Technology
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    • v.8 no.2
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    • pp.61-67
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    • 2009
  • This paper proposes an on-board orbit data generation algorithm for geostationary satellites. The concept of the proposed algorithm is as follows. From the ground, the position and velocity deviations with respect to the assumed reference orbit are computed for 48 hours of time duration in 30 minutes interval, and the generated data are up-loaded to the satellite to be stored. From the table, three nearest data sets are selected to compute position and velocity deviation for asked epoch time by applying $2^{nd}$ order polynomial interpolation. The computed position and velocity deviation data are added to reference orbit to recover absolute orbit information. Here, the reference orbit is selected to be ideal geostationary orbit with a zero inclination and zero eccentricity. Thanks to very low computational burden, this algorithm allows us to generate orbit data at 1Hz or even higher. In order to support 48 hours autonomy, maximum 3K byte memory is required as orbit data storage. It is estimated that this additional memory requirement is acceptable for geostationary satellite application.

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Validation of the Turbulent Burning Velocity Based on Asymptotic Zone Conditional Transport in Turbulent Premixed Combustion (영역조건평균에 기초한 난류예혼합 화염 전파 속도식 유도 및 검증)

  • Lee, Dong-Kyu;Huh, Kang-Y.
    • Journal of the Korean Society of Combustion
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    • v.13 no.1
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    • pp.23-30
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    • 2008
  • An analytical expression for the turbulent burning velocity is derived from the asymptotic zone conditional transport equation at the leading edge. It is given as a sum of laminar and turbulent contributions, the latter of which is given as a product of turbulent diffusivity in unburned gas and inverse scale of wrinkling at the leading edge. It was previously shown that the inverse scale is equal to four times the maximum flame surface density in the wrinkled flamelet regime [1]. The linear behavior between $U_T$ and u' shows deviation with the inverse scale decreasing due to the effect of a finite flamelet thickness at higher turbulent intensities. DNS results show that $U_T/S^0_{Lu}$ may be given as a function of two dimensionless parameters, $u'/S^0_{Lu}$ and $l_t/\delta_F$, which may be transformed into another relationship in terms of $u'/S^0_{Lu}$, and Ka. A larger $l_t/{\delta}_F$ or a smaller Ka leads to a smaller scale of wrinkling, hence a larger turbulent burning velocity in the limited range of $u'/S^0_{Lu}$. Good agreement is achieved between the analytical expression and the turbulent burning velocities from DNS in both wrinkled and thickened-wrinkled flame regimes.

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Twin Spray Characteristics Between Two Impinging F-O-O-F Type Injectors

  • Kang, Shin-Jae;Lee, Eun-Sang;Kwon, Ki-Chul;Oh, Je-Ha;Yu, Myoung-Jong
    • Journal of Mechanical Science and Technology
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    • v.16 no.5
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    • pp.732-742
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    • 2002
  • This paper presents twin spray characteristics of two impinging F-O-O-F type injectors in which fuel and oxidizer impinge on each other to atomize under the various conditions. The droplet size and velocity in the impinging spray flow field were measured using PDPA. The droplet size and velocity were investigated at the mixture ratios of 1.5, 2.0, 2.47 and 3.0 for four injectors in which two single F-O-O-F injectors were arranged at the intervals of 20.8, 31.2, 41.6 and 62.4mm respectively. In general, the arithmetic mean diameter, SMD and standard deviation of droplet size in the interaction area (X=0 and Y=0mm) were smaller, while the axial velocity in the interaction area was slightly higher. An empirical correlation is obtained for the (D$\_$10/)$\_$D//(D$\_$10/)$\_$c/ value under the assumptions of two identical droplets and these with different size and velocity. The droplets with low Weber numbers below 40 have possibility to coalesce, while those over 40 tend to disintegrate after impingement in the interaction area.

Radiation characteristics of A Circular Loop antenna In Moving Media (운동매질내에서의 Circular Loop Antenna의 개체특성)

  • 최병하
    • Journal of the Korean Institute of Telematics and Electronics
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    • v.7 no.3
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    • pp.12-18
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    • 1970
  • In this paper, the radiation characteristics of a Circular Loop Antenna is studied in a moving homogeneous, isotropic and linear media with a constant velocity much less than the speed of light. In Stuffing the radiation characteristics, Srst vector potential on the loop antenna is derived in the moving media by appling Maxwell-Minkowaski's theory. Next, using the derived relations, the electric and magnetic Seld is calculated for the spec-i Sed wave length ana velocity of the media. The Seld patterns in the moving media are compared with those of stationary media. We find that the intensity of the field is reduced in the direction of the media velocity and increased in the opposite direction only for the component parallel with the plane of the antenna. The deviation from the stationary media is proportional to the velocity of the media and the frequency of source current.

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A Study on the Vibration Reduction of Borehole by the Receive Distance (수진 거리에 따른 방진구의 진동 저감 연구)

  • Song, Jeong-Un;Kim, Seung-Kon;Hong, Woong-Ki
    • Journal of Environmental Impact Assessment
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    • v.23 no.3
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    • pp.169-176
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    • 2014
  • The purpose of this study is to estimate the vibration reduction effect of the borehole which is controlled the vibration propagation in the ground. For this study, we measured the vibration velocity before and after the borehole installation. The results are as follows: The peak particle velocity(PPV) and peak vector sum(PVS) was reduced by the borehole. And also, the deviation of vibration velocity before and after the borehole installation showed large values in longitudinal and vertical component depending on the receive distance, and increased depending on the size of vibration energy. Finally, the vibration isolation efficiency was 25~35 percentage at 1.5m receive distance, and was 4~14 percentage at 3.0m receive distance. It was found that the vibration isolation efficiency was good in small vibration energy, but was not good at long receive distance.

Modeling of Deviation Angle and Pressure Loss due to Rotor Tip Leakage Flow in Axial Turbines (축류터빈의 동익에서 끝간격 누설유동에 의한 편향각과 압력손실의 모형화)

  • 윤의수;오군섭;정명균
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 1998.04a
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    • pp.13-13
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    • 1998
  • A simple model of the tip leakage flow models of the rotor downstream flow is developed, based on Lakshminarayana's theoretical concept on the tip clearance flow and the experimental data published in open literature. And new spanwise distribution models of deviation angle and pressure loss coefficient due to the tip leakage flow are formulated for use in association with the streamline curvature method as a through flow analysis. Combining these new models and previous deviation and loss models due to secondary flow, a robust streamline curvature method is established for flow analysis of single-stage, subsonic axial turbines with wide ranges of turning angle, aspect ratio and blading type. At the exit from rotor rows, the flow variables are mixed radially according to a spanwise transport equation. The proposed streamline curvature method is tested against a forced vortex type turbine as well as a free vortex type one. The results show that the spanwise variations of flow angle, axial velocity and loss coefficients at rotor exit are predicted with good accuracy, being comparable to a steady three-dimensional Navier-Stokes analysis. This simple and fast flow analysis is found to be very useful for the turbine design at the initial design phase.

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A Study on Sensor Collection Planning based on Target Scheduling and Deviation Correction for Strategic UAV Surveillance and Reconnaissance (전략급 무인기의 감시정찰을 위한 표적 스케줄링 및 편차 보정 기반 촬영계획 자동화 기술 연구)

  • Junghee Cho;Yunjeong Choi;Hayrim Lee;Soyoung Jeong
    • Journal of the Korea Institute of Military Science and Technology
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    • v.27 no.2
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    • pp.177-188
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    • 2024
  • The strategic UAV for theater level ISR(Intelligence, Surveillance and Reconnaissance) mission typically has numerous ground targets over area of responsibility(AOR) or area of operation(AO). It is necessary to automatically incorporate these multitude of ground targets into mission planning process in order to collect ISR images before actual flight mission. In addition, weather information such as wind direction and/or velocity may have significant impacts on the qualities of collected sensor images, especially in SAR(Synthetic Aperture Radar) images. Thus weather factors in the operation altitude should also be considered in the mission planning stage. In this study, we propose a novel mission planning scheme based on target scheduling and deviation correction method incorporating weather factors.

Deformation Behavior of Slab by Two-Step Sizing Press in a Hot Strip Mill (열간 압연에서 2단 사이징 프레스 금형에 의한 슬래브의 변형거동 예측)

  • Lee S. H.;Kim D. H.;Byon S. M.;Park H. D.;Kim B. M.
    • Transactions of Materials Processing
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    • v.14 no.9 s.81
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    • pp.791-797
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    • 2005
  • Extensive width reduction of slabs is an important technology for achieving continuous production between the steelmaking and hot rolling processes. However, the vertical horizontal rolling process has many disadvantages, e.g., large width deviations and less efficient width reduction. This study was carried out to investigate the deformation of slab by sizing press with two steps die. To do it, dog-bone and camber are discussed in width sizing process considering the deformation behavior according to the deviation of anvil velocity and the deviation of initial slab temperature. In this paper, the various causes of the sizing press phenomena are mentioned for the purpose of understanding of rolling conditions. As a result, the optimal anvil shape having a minimum-forming load is obtained by FE-simulation and ANN.

A STUDY ON LAMP BANK DESIGN OF SOLAR SIMULATOR (솔라시뮬레이터의 램프뱅크 설계에 관한 연구)

  • Baek, S.H.
    • Journal of computational fluids engineering
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    • v.17 no.3
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    • pp.45-52
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    • 2012
  • This paper is a study on the design of the solar lamp bank which is a very important part of the solar simulator with the commercial metal halide lamps and infrared lamps. Lamp Bank is designed by the lamp bank design program based on point light source theory. The reliability of the program for lamp bank design is verified through irradiance variation experiments of a kind of lamp according to horizontal distance. Solar lamp bank facilitates heat distribution and satisfies the irradiance in the three wave length which test guidelines require. The shape of the ceiling board next to the lamp bank to promote the lamp cooling efficiency and to reduce temperature deviation and air velocity deviation in the chamber is so creative. The ceiling board of partial closed type is the best among several types.

A Roll-Bite Profile Map Approach for the Prediction of Front End Bending in Plate Rolling (후판 압연공정에서 선단부 굽힘 예측을 위한 롤 바이트 형상맵 기법에 관한 연구)

  • Byon, S.M.;Lee, J.H.;Kim, S.R.
    • Transactions of Materials Processing
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    • v.20 no.4
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    • pp.284-290
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    • 2011
  • The front end bending(FEB) behavior of material that usually occurs in plate rolling is investigated. In this paper, a rollbite profile map approach that systematically predicts the FEB slope is presented. It is based on the concurrent use of shape factors and reduction ratios to ensure an accurate value of the FEB and its slope. In order to obtain the unit roll-bite profile map, the FEB slope model was decomposed into a temperature deviation component and a roll-velocity deviation component. By mapping the results of a series of finite element analyses to the unit functions of the roll-bite profile map, it was possible to obtain a realistic prediction of the FEB slope applicable to an actual plate rolling process. Thereby, the usefulness of the present approach is clearly demonstrated.