• Title/Summary/Keyword: 임계질량

Search Result 59, Processing Time 0.022 seconds

Critical Loads of Tapered Cantilever Columns with a Tip Mass (자유단 집중질량을 갖는 변단면 캔틸레버 기둥의 임계하중)

  • Jeong, Jin Seob;Lee, Byoung Koo;Kim, Gwon Sik;Kim, Jong Ung
    • Journal of Korean Society of Steel Construction
    • /
    • v.17 no.6 s.79
    • /
    • pp.699-705
    • /
    • 2005
  • This paper investigates critical loads of tapered cantilever columns with a tip mass, subjected to a follower force. The linearly tapered solid rectangular cross-sections are adopted as the column taper. The differential equation governing free vibrations of such columns, also called Beck's columns, is derived using the Bernoulli-Euler beam theory. Both divergence and flutter critical loads are calculated from the load-frequency curves that are obtained by solving the differential equation. The critical loads are presented as functions of various non-dimensional system parameters, namely, the taper type, the subtangential parameter, and the mass ratio.

디퓨져의 확대각이 임계노즐 유동에 미치는 영향

  • 김재형;김희동
    • Proceedings of the Korean Society of Propulsion Engineers Conference
    • /
    • 2002.04a
    • /
    • pp.31-32
    • /
    • 2002
  • 임계노즐(critical nozzle)은 유동을 유로 최소단면부에서 초크시켜, 질량유량을 계측하기 위한 일종의 유체기구로, 최근 다양한 분야에서 널리 활용되고 있다. 압축성 기체역학의 관계식에 의하면, 임계노즐을 통하는 기체유동의 이론적인 질량유량은 노즐 목의 직경, 노즐 상류의 온도와 압력 그리고 기체의 비열비 등의 함수로 주어진다 그러나 실제 유동에서는 점성과 열전달 등의 초과로 인하여, 이론적 질량 유량과 실제유량의 비 즉 유출계수(discharge coefficient)의 값은 1.0으로 되지 않는다.

  • PDF

Critical Mass Minimization of a Cylindrical Geometry Reactor by Two Group Diffusion Equation

  • Lee, Chang-Kun
    • Nuclear Engineering and Technology
    • /
    • v.5 no.2
    • /
    • pp.115-131
    • /
    • 1973
  • L.S. Pontryagin's maximum principle is applied to the minimum critical mass problem without any restriction on the ranges of uranium enrichment. For the analysis, two group diffusion equation is adopted for a cylindrical reactor neglecting the vertical axis consideration. The result shows that the three-zoned reactor turns out to be most optimal: the inner and outer zones with the minimum enrichment ; whereas the middle 3one with the maximum enrichment. With the given three-zoned reactor, critical condition is derived, which leads to the calculation of the determinant. By finding the roots of the determinant the numerical calculation of the minimum critical mass is carried out for the case of Kori reactor geometry changing the minimum or the maximum enrichment. It is found from many computed values that the least possible critical mass turns out to be the case of 1.2% maximum enrichment for the middle zone and 0.65% minimum enrichment for the inner and out zones.

  • PDF

Additive Noise Reduction Algorithm for Mass Spectrum Analyzer (질량 스펙트럼 분석기를 위한 부가잡음제거 알고리즘)

  • Choi, Hun;Lee, Imgeun
    • Journal of the Korea Institute of Information and Communication Engineering
    • /
    • v.22 no.1
    • /
    • pp.33-39
    • /
    • 2018
  • An additive noise reduction algorithm for a mass spectrum analyzer is proposed. From the measured ion signal, we first used an estimated threshold from the mode of the measured signal to eliminate background noises with the white Gaussian characteristics. Also, a signal block corresponding to each mass index is constructed to perform a second order curve fitting and a linear approximation to signal block. In this process, the effective signal block composed of only the ion signal can be reconstructed by removing the impulsive noises and the sample signals which are insufficient to be viewed as normal ion signals. By performing curve fitting on the effective signal block, the noise-free mass spectrum can be obtained. To evaluate the performance of the proposed method, a simulation was performed using the signals acquired from the development equipment. Simulation results show the validity of the threshold setting from the mode and the superiority of the proposed curve fitting and linear approximation based noise canceling algorithm.

Stability Analysis of Beck's Column with a Tip Mass Restrained by a Spring (스프링으로 지지된 자유단에 집중질량을 갖는 Beck 기둥의 안정성 해석)

  • Li, Guangfan;Oh, Sang-Jin;Kim, Gwon-Sik;Lee, Byoung-Koo
    • Transactions of the Korean Society for Noise and Vibration Engineering
    • /
    • v.15 no.11 s.104
    • /
    • pp.1287-1294
    • /
    • 2005
  • The purpose of this paper is to investigate free vibrations and critical loads of the Beck's columns with a tip spring, which carry a tip mass. The ordinary differential equation governing free vibrations of Beck's column subjected to a follower force is derived based on the Bernoulli-Euler beam theory Both the divergence and flutter critical loads are calculated from the load-frequency corves that are obtained by solving the differential equation numerically. The critical loads are presented in the figures as functions of various non-dimensional system parameters such as the subtangential parameter, mass ratio and spring parameter.

Experimental Study on the Stability of the Cantilever Beam with Tip Mass Subjected to a Follower Force (종동력을 받는 첨단질량을 갖는 외말보의 안전성에 관한 실험적 연구)

  • 노광춘;박영필
    • Transactions of the Korean Society of Mechanical Engineers
    • /
    • v.10 no.2
    • /
    • pp.183-187
    • /
    • 1986
  • An experimental method to give a tangential follower force to a cantilever beam having a concentrated tip mass by the magnetic force of the electromagnet has been described. The dynamic behaviour of the beam under this nonconservative load has been analysed by experimentally as well as by theoretically. The theoretical and experimental results on the natural frequencies and the critical force of the systems are in good agreement with each other.

Critical Speed Analysis of the Liquid Rocket Turbopump (액체로켓 터보펌프의 임계 속도 해석)

  • Jeon, Seong-Min;Kwak, Hyun-Duck;Yoon, Suk-Hwan;Kim, Jin-Han
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.33 no.6
    • /
    • pp.92-99
    • /
    • 2005
  • Numerical analyses of critical speed and mass unbalance response are performed for a 30 ton thrust turbopump. The stiffness and damping of ball bearings and non-contact seals are quantified under aerodynamic and hydrodynamic loads induced by a fuel pump and turbine. Critical speed margin and tip displacements of the rotating parts are evaluated using a three-dimensional finite element method. The results are used to ensure the soundness of the rotordynamic design using an one-dimensional transfer matrix method. A further study shows that sufficient resonance margin may be assured via controlling the stiffness of the rotor support by employing an additional elastic ring to the bearing support.

Study on the Stability of Cantilevered Pipe Conveying Fluid Subjected to Distributed Follower Force (분포종동력을 받는 외팔 송수관의 안정성에 관한 연구)

  • Kong, Chang-Duk;Park, Yo-Chang
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.33 no.4
    • /
    • pp.27-34
    • /
    • 2005
  • The paper discussed on the stability of cantilevered pipe conveying fluid subjected to distributed follower force. Governing equations of motion are derived by extended Hamilton's principle, and the numerical scheme using finite element method is applied to obtain the discretized equations. The critical flow velocity as a function of the distributed follower force for the various mass ratio is determined. The flutter configurations of the pipes at the critical flow velocities are drawn graphically at every twelfth period to define the order of quasi-mode of flutter configuration The critical mass ratios, at which the transference of the eigenvalue branches related to flutter take place, are definitely determined. Also, the effect of damping on the stability of the system is considered.

A Study on Mass Transport for InGaAsP/InP Buried Heterostructure Laser Diode (매립형 InGaAsP/InP 레이저 다이오드 제작을 위한 질량 이동 현상에 관한 연구)

  • Choi, In-Hoon;Lee, Jong-Min;Sin, Dong-Suk;Singer, K.E.
    • Korean Journal of Materials Research
    • /
    • v.8 no.5
    • /
    • pp.419-423
    • /
    • 1998
  • The conditions for optimizing mass transport for making buried heterostructure (BH) InGaAsP/lnP lasers are discussed. The double heterostructure InGaAsP/lnP laser structures were grown by Liquid Phase Epitaxy (LPE) and etched into mesas. The active layer was selectively etched along [llO] and the mass transport was carried out in the LPE reactor to cover the sides of the active layer and form a BH structure. The threshold temperature for the appreciable mass transport is measured to be 670$670^{\circ}C$ when the holding time is set to 40 min. The width of the region re¬filled by mass transport is observed to increase as the temperature increases.

  • PDF

Rotordynamic design of a fuel pump and turbine for a 75 ton liquid rocket engine (75톤급 액체로켓 엔진용 연료펌프/터빈 회전체 동역학 설계)

  • Jeon, Seong-Min;Kwak, Hyun-Duck;Yoon, Suk-Hwan;Kim, Jin-Han
    • Aerospace Engineering and Technology
    • /
    • v.6 no.1
    • /
    • pp.201-208
    • /
    • 2007
  • A fuel pump and turbine rotordynamic design is performed for a 75 ton thrust liquid rocket engine. A distance from the rear bearing to the turbine was considered as a design parameter for load distribution of the bearings. Asynchronous eigenvalue analysis was performed as a function of rotating speeds, turbine mass and bearing stiffness to investigate critical speed of the fuel pump and turbine. From the numerical analysis, it is found that the effect of the front bearing stiffness is negligible in the critical speed due to the large mass moment of inertia of the turbine. With the rear bearing stiffness over $2{\times}10^{8}N/m$ and the turbine mass below 20 kg, the critical speed of the fuel pump and turbine in long shaft case is at least 70 % higher than the operating speed 11,000 rpm.

  • PDF