• Title/Summary/Keyword: 동안

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Effect of Shock Waves on Dynamic Stability of Transonic Missiles (천음속 미사일의 동안정성에 대한 충격파 영향)

  • Park, Su-Hyeong;Gwon, Jang-Hyeok;Heo, Gi-Hun;Byeon, U-Sik
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.30 no.2
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    • pp.12-20
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    • 2002
  • Three dimentional unsteady Euler equations are solved and an integration method is presented to predict the dynamic stability derivatives of transonic missiles. Results for the Basic Finner model are compared with several experimental data to vaildate the prediction capability of the present method. The variations of dynamic stability derivatives are discussed with respect to angle of attack, Mach number, and rotation rate. Results show that shock waves between fins enhance the pitch-damping characteristics in transonic region. Results also imply that the Euler equations can give the damping coefficients with comparable accuracy.

A Study on the Measurement of Dynamic Stability Derivatives in the Rolling Motion of Aircraft (항공기의 롤운동 동안정미계수 측정에 관한 연구)

  • Cho, Hwan-Kee
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.21 no.4
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    • pp.41-46
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    • 2013
  • This paper deals with an experimental technique for the measurement of dynamic stability derivatives in the roll motion of aircraft. Experimental aquisition method for aircraft's dynamic stability derivatives is conducted on the oscillation condition of aircraft model in the subsonic wind tunnel. The oscillation of aircraft model was forced by the oscillation apparatus. The forced oscillation technique is the method getting data from the internal balance inserted into the aircraft model during oscillating it. Dynamic stability derivatives of rolling motion were calculated by data reduction from the measurements of rolling moment, frequency and amplitude of aircraft model due to forced oscillation under wind conditions. Results of experiment is obtained similar one with those of roll dynamic stability derivatives measured in other institutes.

Measurements of the Pitch Dynamic Stability Derivatives of a Standard Dynamics Model Using a Forced Vibration Technique (강제진동기법을 이용한 표준동역학 모델의 피치 동안정미계수측정)

  • Cho, Hwan-Kee;Kim, Seung-Pil;Baek, Seung-Woock;Chang, Jo-Won
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.35 no.6
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    • pp.489-495
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    • 2007
  • An experimental study was carried out in order to measure the pitch dynamic stability derivatives of a standard dynamics model in a low-speed wind tunnel. When a trigger signal is generated, the aircraft model starts oscillation with constant amplitudes and frequencies provided by DC electrical servomotor. The measured data are simultaneously recorded on a data recorder for 25 cycles of the model oscillation. The Phase shift needed to compute the dynamic stability derivatives is determined by calculating differences between the peak values of the input and output signals from the dynamic stability balance. Stabilator effects on the stability derivatives were also investigated with deflection angles. Although the driving apparatus and experimental equipments manufactured creatively for this study are different from other experiments, the variational trend of dynamic stability derivatives with the angle of attack is in a good accordance with the results of TPI, NAE, and FFA.

Effects of Ca Supplementation on Mineral Metabolism during Pregnancy and Lactation of Calcium-Deficient Young Adult Rats (칼슘섭취 부족 흰쥐에서 임신, 수유기 동안 칼슘보충 수준이 무기질 대사에 미치는 영향)

  • 박미나;김은애;이연숙
    • Journal of the Korean Society of Food Science and Nutrition
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    • v.33 no.6
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    • pp.958-964
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    • 2004
  • This study examined the effects of maternal calcium intake levels on mineral metabolism during pregnancy and lactation. Five week-old female Sprague-Dawley rats were fed normal Ca (NCa, 0.5%) and low Ca (LCa, 0.15%) diets for 5 weeks during preconception. The low Ca intake group was divided into three groups and fed low Ca (0.15%), normal Ca (0.5%) and high Ca (1.5%) diets for 6 weeks during pregnancy and lactation. All of the rats were mated with normal male rats. The control group was consistently fed a normal Ca diet for 11 weeks. Pups were adjusted to 10 per dam. After weaning, dams and their weaned rats were sacrificed. We measured total protein, albumin, alkaline phosphatase and mineral content in serum and weight, length, breaking force, ash and mineral content in bone and kidney. There was no significant difference in weight gain and food intake among the groups. Serum total protein and albumin were in the normal range but slightly decreased with a low Ca diet during preconception. Calcium supplementation above normal level increased bone weight, Ca content and breaking force in femur of maternal and their weaned rats. However, high maternal Ca intake significantly decreased Mg and Fe contents in maternal serum and bone and Mg and Zn contents in serum of weaned rats. Also, it induced Ca, P and Mg deposit in maternal kidney. Our experimental results suggest that Ca deficiency during preconception may deteriorate bone status of mother and their offsprings. Moreover, high Ca supplementation during pregnancy and lactation may lead to disturb mineral metabolism in bone and other tissues.

우리 나라의 반도분 산업 1974~1989

  • 김충기
    • The Magazine of the IEIE
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    • v.12 no.1
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    • pp.37-39
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    • 1985
  • 본 고에서는 1974년부터 1984년까지 10년 동안의 국내 반도체 산업의 발전을 웨이퍼 가공을 중심으로 살펴보고 앞으로 5년 동안의 발전을 예상하여 본다.

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Measurement of Dynamic Stability Derivatives of Tailless Lamda-shape UAV using Forced Oscillation Method (강제진동 기법을 이용한 무미익 비행체의 동안정 미계수 측정)

  • Yang, Kwangjin;Chung, Hyoungseog;Cho, Donghyun;An, Eunhye;Ko, Joonsoo;Hong, JinSung;Kim, Yongduk;Lee, MyungSup;Hur, Gi-Bong
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.44 no.7
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    • pp.552-561
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    • 2016
  • In this experimental study, the dynamic stability derivatives of a tailless lambda-shape UAV are estimated from time history data of aerodynamic moments measured from the internal balance while the test model is forced to oscillate at given frequencies and amplitudes. A 3-axis forced oscillation apparatus is designed to induce decoupled roll, yaw, pitch oscillations respectively. The results show that the roll damping derivatives remain stable at the entire range of angle of attack tested, whereas the pitch damping derivatives become unstable beyond $15^{\circ}$ angle of attack. The amplitude and frequency have little impact on roll damping derivatives while the smaller amplitude and frequency of oscillation improves the pitch stability. The yaw damping derivative values are fairly small as expected for a tailless configuration. The results indicate that the proposed methodology and test apparatus area valid for estimating the dynamic stability derivatives of a tailless UAV.

강제진동 풍동시험을 통한 비행선의 동안정성 분석

  • Chang, Byeong-Hee;Ok, Ho-Nam;Lee, Yung-Gyo
    • Aerospace Engineering and Technology
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    • v.2 no.2
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    • pp.1-10
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    • 2003
  • An airship is statically unstable, because it has no wing, comparatively small tail and large hull. Hence, an accurate prediction of dynamic stability is critical. In this study, dynamic stability data of the Mid-Size Airship is acquired through forced oscillation wind tests. The test was done in BAR LAMP which is Birhle Applied Research Inc's facility located in Germany. The test was composed with 16 static runs and 26 dynamic runs. As a result, dynamic characteristics of the airship depends on sideslip angle, angular rate and its direction as well as angle of attack. Generally, it is obtained that 3 directional moments have damping, but normal force, side force, and cross-derivatives are unstable. The dynamic derivatives are not sensitive to control surfaces, but have nonlinear dependency on sideslip angle.

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Dynamic Stability Flight Test for Small Aircraft using Modified Maximum Likelihood Estimation (최대공산 추정법을 이용한 항공기 동안정성 비행시험)

  • Lee, Sang-Jong;Park, Jeong-Ho;Chang, Jae-Won;Park, Il-Kyung;Kim, Keun-Taek;Seong, Kie-Jeong
    • Aerospace Engineering and Technology
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    • v.9 no.2
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    • pp.105-115
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    • 2010
  • This technical paper describes and summarizes the flight test results for the longitudinal and lateal-directional dynamic stability characteristics. The target aircraft is the 4-seat carnard type aircraft, FireFly, which has been developed by KARI. Airborne sensors and real-time telemetry system are constructed to obtain the flight test data. The dynamic stability characteristics should be analyzed and tested by estimaitng the aerodynamic parameters in the dymaic equations of motion. The maximum likelihood estimation technique has been applied to the flight data from chirp, 3211, and doublet control inputs.

Change of Microbial Communities in Kimchi Fermentation at Low Temperature (김치의 저온 발효 중 미생물 변화 양상)

  • 박정아;허건영;이정숙;오윤정;김보연;민태익;김치경;안종석
    • Korean Journal of Microbiology
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    • v.39 no.1
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    • pp.45-50
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    • 2003
  • The diversity and change of microbial communities during kimchi fermentation at $4^{\circ}C$ were analyzed by denaturing gradient gel electrophoresis (DGGE). Kimchi samples were taken every 5 days over the fermentation periods (for 60 days) to extract total DNA for DGGE analysis. Touchdown polymerase chain reaction was performed to amplify the V3 region of 16S rRNA gene. Sequencing results of partial 16S rDNA amplicons from DGGE profiles revealed that lactic acid bacteria (LAB), especially Weissella koreensis, Lactobacillus sakei and Leuconostoc gelidum were dominants in kimchi fermentation at $4^{\circ}C$. And we knew that W. koreensis steadily existed throughout the whole fermentation period, also Lb. sakei and Leuc. gelidum appeared from 10th day and 30th day of fermentation time, respectively and then these species were to be dominant microorganisms.