• Title/Summary/Keyword: 십자형낙하산

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A Wind Tunnel Test for Directional Control of Cruciform Parachutes (십자형 낙하산의 방향 제어에 관한 풍동시험 연구)

  • 임주창;김범수
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.34 no.9
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    • pp.20-24
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    • 2006
  • Wind tunnel tests were conducted to compare gliding and turning performance of normal cruciform parachutes with newly modified cruciform parachutes. Modified cruciform parachute has better gliding performance than original cruciform parachutes but, modified cruciform parachute has worse turning performance than original cruciform parachute.

An experimental study on reefing effect on aerodynamics characteristics of cruciform parachute (십자형 낙하산의 Reefing 효과에 따른 공력특성에 관한 실험연구)

  • Lee, Chang-Gu;Kim, Beom-Soo
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.36 no.7
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    • pp.628-633
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    • 2008
  • Cruciform parachute has advantage in manufacture and expanse compare with circular parachute. But it has disadvantage in stability. Wind tunnel test were conducted to investigate the effects of reefing-line on the cruciform parachutes with the purpose of finding aerodynamics characteristics of the parachute such as drag coefficient, normal force coefficient. Aerodynamics characteristics are measured accurately with 6-components pyramidal balance and load cells which were installed in the fixed-body. Four different models were tested and the test results were compared with each other. The aerodynamics characteristics were changed with reefing-line length. Separation edge was developed due to reefing-line also it made increasing of the stability. The cruciform parachute which improve stability is supposed to be used in variety purpose.

Effects of Time-Varying Mass on the Dynamic Behavior of a Descending Parachute System (질량 감소가 낙하산 시스템의 하강 고도 변화에 미치는 효과)

  • Jang, Woo-Young;Baek, Sang-Tae;Myong, Rho-Shin;Jin, Yeon-Tae
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.44 no.4
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    • pp.281-289
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    • 2016
  • Accurate prediction of the trajectory and time of a time-varying mass parachute system remains essential in the mission requiring a precision airdrop to the ground. In this study, we investigate the altitude-varying behavior of a cross-type parachute system designed to deliver a time-varying mass object like flare. The dynamics of the descending parachute system was analyzed based on the Runge-Kutta method of the ordinary differential system. The drag coefficients of the cross-type parachute and flare were calculated by a CFD code based on the incompressible Navier-Stokes equation. Finally, by using a simplified gust wind model in troposphere, the combined effects of gust wind and time-varying mass were examined in detail.