• Title/Summary/Keyword: Coning motion test

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Study on Coning Motion Test for Submerged Body (몰수체의 원추형시험에 관한 연구)

  • Park, Jong-Yong;Kim, Nakwan;Rhee, Key-Pyo;Yoon, Hyeon Kyu;Kim, Chanki;Jung, Chulmin;Ahn, Kyoungsoo;Lee, Sungkyun
    • Journal of Ocean Engineering and Technology
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    • v.29 no.6
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    • pp.436-444
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    • 2015
  • A submerged body is sensitive to changes in the roll moment because of the small restoring moment and moment of inertia. Thus, a method for predicting the roll-related hydrodynamic coefficients is important. This paper describes a deduction method for the hydrodynamic coefficients based on the results of a coning motion test. A resistance test, static drift test, and coning motion test were performed to obtain the coefficients in the towing tank of Seoul National University. The sum of the hydrodynamic force, inertial force, gravity, and buoyancy was measured in the coning motion test. The hydrodynamic force was deduced by subtracting the inertial force, gravity, and buoyancy from the measured force. The hydrodynamic coefficients were deduced using the regression method.

An Experimental Study on Flapping Motion of Forward Flight Condition used to Articulated Hub Rotor (관절형 허브 로터를 이용한 전진비행조건에서의 플래핑 운동에 대한 실험적 연구)

  • Ryi, Jae-Ha;Back, Dong-Min;Rhee, Wook;Choi, Jong-Soo;Song, Keun Woong
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.41 no.4
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    • pp.261-267
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    • 2013
  • In this paper, wind tunnel test and analytical prediction are compared for result of flapping motion in helicopter forward flight condition. Tests were performed at low speed wind tunnel at Chungnam National University, test section of wind tunnel has 1.8 by 1.8 meter open-jet test section area. According to the results of measured data for aerodynamic performance of model rotor in forward flight. It has to observed the difference of analytical and measured results of power coefficient for fixed thrust coefficient. And calculated and measured data of helicopter rotor flapping angles in forward flight are compared for a model rotor in a wind tunnel. A test was conducted to verify the measured data of coning and lateral/longitudinal flapping angle with predicted values.