• Title/Summary/Keyword: twist angle distribution

Search Result 12, Processing Time 0.025 seconds

Study of the Electro-Optic Characteristics Depending on Electric Characteristic of the Black Matrix in a Homogeneous Liquid Crystal Cell Driven by Fringe-Electric Field (프린즈 전기장에 의해 구동되는 수평 배향 액정셀에서 black matrix의 전기적 특성이 셀의 전기광학 특성에 미치는 영향에 관한 연구)

  • 김미숙;김향율;고재완;이승희
    • Journal of the Korean Institute of Electrical and Electronic Material Engineers
    • /
    • v.16 no.11
    • /
    • pp.1008-1013
    • /
    • 2003
  • We have studied the effect of black matrix (BM) according to the dielectric anisotropy of liquid crystals (LCs) for a homogeneously aligned LC cell driven by fringe-electric field. The results show that for a LC with positive dielectric anisotropy (+LC) there is a large transmittance change when using a conductive BM, whereas the transmittance change is low for a LC with negative dielectric anisotropy (-LC). The conductive BM existing on top substrate produces vertical electric field, which makes the LC molecules be tilt upward from the substrate and have small twist angle for the +LC. However, for the -LC the conductive BM affects the LC distribution only slightly due to characteristic of the -LC orienting perpendicular to the field. Therefore, for the +LC the electro-optic characteristics are strongly dependent on conductivity of the BM on top substrate in a homogeneous liquid crystal cell driven by fringe-electric field.

Numerical Analyses and Wind Tunnel Tests of a Propeller for the MAV Propulsion (초소형 무인기 추진용 프로펠러의 전산해석 및 풍동시험)

  • Cho, Lee-Sang;Lee, Sea-Wook;Cho, Jin-Soo
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.38 no.10
    • /
    • pp.955-965
    • /
    • 2010
  • The MH-75 propeller for the MAV propulsion is designed using a free vortex design method which considers design parameters such as the hub-tip ratio, the twist angle distribution, the maximum camber location and the chord length of the propeller blade. Aerodynamic characteristics of the MH-75 propeller are predicted by changing the flight speed using the frequency domain panel method. And, the thrust characteristics of the MH-75 propeller are measured using the balance system of the subsonic wind tunnel for the validation of numerical results. The performance characteristics of the MH-75 propeller satisfied with design requirements. Numerical results of the MH-75, which are predicted by the frequency domain panel method, are more agree with experimental results compare with XFOIL.