• Title/Summary/Keyword: Flying Height

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Numercal Simulation of Unsteady Performance for 20D Surface Effect Airfoils (2차원 해면효과익의 비정상 성능에 대한 수치적 시뮬레이션)

  • Park, Il-Ryong;Jeon, Ho-Hwan
    • Journal of Ocean Engineering and Technology
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    • v.9 no.2
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    • pp.71-74
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    • 1995
  • A numerical model capable of simulating a 2-D airfoil flying over in the vicinity of the waves is discussed. Instead of treating the problem as a heaving oscillation one above the rigid flat wall, sources are distributed on the prescribed wave profile. The wave deformation due to the airfoil is assumed to be negligible and treated as a rigid undulated wall. The source and vortex are distributed on the surface of the foil. It is found that the variation of $C_L$ with wave steepness in severe and that the lift variation due to waves decreases as the wing height above the water surface increases.

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On the Rock Fragmentation with Plasma Blasting (플라즈마 장비의 발파공법)

  • 이경운
    • Explosives and Blasting
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    • v.17 no.2
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    • pp.19-35
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    • 1999
  • Rock fragmentation with plasma blasting technique has advantageous properties in contrast to the conventional blasting method controlling of flying rocks and ground vibrations, when residents are complaining or surrounding structures stay in protection from blasting operations. The experiences show in urban construction works that the plasma blasting is the most possible method to prevent damages and minimize adverse environmental impacts. The fragmentation energy level is evaluated by numerical simulation using PFC for various drill hole patterns and tested accordingly to get the feasibility. The energy output of plasma blasting system has been improved to a level of 1 MJ, which can break a 2-3 ㎥ granite boulder or 1.5m height bench face. Measurements are carried out to get the ground vibration level and propagation equation, so that control of the blasting operations can be performed more precisely and safely.

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Analysis of Energy and Ground Vibration of Plasma Blasting (플라즈마 발파의 폭력과 지반진동특성)

  • 이경운;박철환;신중호;류창하
    • Tunnel and Underground Space
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    • v.7 no.4
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    • pp.267-273
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    • 1997
  • Rock fragmentation with plasma blasting technique has advantageous properties in contrast to the conventional blasting method in controlling of flying rocks and ground vibrations, when residents are complaining or surrounding structures stay in protection from blasting operations. The experiences show in urban construction works that the plasma blasting is the most possible method to prevent damages and minimize adverse environmnetal impacts. The fragmentation energy level is evaluated by numerical simulation using PFC-2D for various drill hole pattern and tested accordingly to get the feasibility. The energy output of plasma blasting system has been improved to a level of 1 MJ, which can break a 2~3 ㎥ granite boulder or 1.5 m height bench face. Measurements are carried out to get the ground vibration level and propagation equation, so that the control of the blasting operations can be performed more precisely and safely.

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The analysis of Yurchenko's 900 Degree Twist Technique with Stretched Body (도마 Yurchenko 몸 펴 900도 비틀기 기술 분석)

  • Yeo, Hong-Chul
    • Korean Journal of Applied Biomechanics
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    • v.16 no.4
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    • pp.165-173
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    • 2006
  • The purpose of this study was to analyze Yurchenko's 900 degree twist technique between the highly scored and the lowly scored subjects during the 2003 TaeGu Universiad Championship. The following results was obtained by analyzing horizontal, vertical and resultant velocities on 1st, 2nd, 3rd and 4th phases. The highly scored subject took longer total performance time but shorter time in 2nd and 300 phases. The highly scored subject also took longer performance time in 4th phase. In the board contact phase the highly scored subject had bigger elbow joint angle and shoulder joint angle. The highly scored subject had longer flying time and had more higher vertical height but lower horizontal and resultant velocities on 4th phase.

Sampling and Analysis of Particles Generated in CSS-Mode of a Hard Disk Drive by Using a Particle Sampler (입자 샘플러를 이용한 하드디스크 CSS 동작 시 발생한 입자 샘플링 및 분석)

  • Lee Jae ho;Lee Dae Young;Kim Sang Yoon;Hwang Jung ho
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.29 no.5 s.236
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    • pp.599-608
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    • 2005
  • Controlling particle contamination is important to increase storage capacity as the flying height of a slider in a hard disk drive decreases. Since precise detection and analysis of particles are primary steps of particle control in a HDD, many researchers have used sampling methods. In this paper, we newly designed a particle sampler and conducted performance evaluation of the sampler. Also, we conducted particle sampling from the HDD using the particle sampler and analysis of sampled particles by SEM and AES. Experimental results show that the particles generated by the slide-disk interaction mainly came from the disk surface.

Wake Shapes Behind Wings in Close Formation Flight Near the Ground

  • Han Cheolheui;Cho Leesang;Cho Jinsoo
    • Journal of Mechanical Science and Technology
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    • v.19 no.2
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    • pp.674-681
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    • 2005
  • The unsteady evolution of trailing vortex sheets behind wings in close formation flight near the ground is simulated using a discrete vortex method. The ground effect is included by an image method. The method is validated by comparing computed results with other numerical results. For a lifting line with an elliptic loading, the ground has an effect of moving wingtip vortices laterally outward and suppressing the development of vortex evolution. The gap between wings in close formation flight has an effect of moving up wingtip vortices facing each other. For wings flying in parallel, the ground effect causes the wingtip vortices facing each other to move up, and it makes the opposite wing tip vortices to move laterally outward. When there is a relative height between the wings in ground effect, right-hand side wingtip vortices from a mothership move laterally inward.

Steady Aerodynamic Characteristics of a Wing Flying Over a Nonplanar Ground Surface Part I : Rail

  • Han Cheol-Heui;Kim Hak-Ki;Cho Jin-Soo
    • Journal of Mechanical Science and Technology
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    • v.20 no.7
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    • pp.1043-1050
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    • 2006
  • The aerodynamic interaction between a wing and a rail is investigated using a boundary-element method. The source and doublet singularities are distributed on the wing and its guide-way rail surface. The unknown strengths of the singularities are determined by inverting the aerodynamic influence coefficient matrices. Present method is validated by comparing computed results with the other numerical data. Rail width and rail height affect the aerodynamic characteristics of the wing only if the rail is narrower than the wing span. Although the present results are limited to the inviscid, irrotational flows, it is believed that the present method can be applied to the conceptual design of the high speed ground transporters moving over the rail.

Numerical Investigation of Contamination Particle's Trajectory in a Head/slider Disk Interface (헤드/디스크 인터페이스 내에서 오염 입자의 거동에 관한 수치적 연구)

  • Park, Hee-Sung;Hwang, Jung-Ho;Choa, Sung-Hoon
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.24 no.3
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    • pp.477-484
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    • 2000
  • Microcontamination caused by particle deposition on the head disk interface threatens the reliability of hard disk drive. Design of slider rail to control contamination becomes an important issue in magnetic recording. In this paper, how particles adhere to the slider and the disk is examined. To investigate accumulation mechanism of the particles, trajectory of the particles in a slider/disk interface is simulated with considering various forces including drag force, gravitational force, Saffman lift force, and electrostatic force. It is found that the charged particles can easily adhere to the slider or disk surface, if an electric field exists between the slider and the disk. It is supposed that the vertical motion of the particles should be related with not only Saffman force but also electrostatic force.

Ramp Load/Unload Velocity Control of VCM Using BEMF in HDD (램프 로드/언로드 HDD의 역기전력을 이용한 VCM 속도 제어)

  • 정준;강태식;김태수;정광조;이철우
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2004.05a
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    • pp.730-735
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    • 2004
  • Nowadays, most small form-factor drives adapt a load/unload mechanism and the flying height of the head becomes more and more low. So, the load/unload velocity also becomes one of the important factors to ensure the reliability of the load/unload operation. To control the load/unload velocity accurately, velocity sensing is most important because there is no special velocity sensor during the load/unload operation. In this paper, we proposed a very practical method that measures the velocity from the BEMF voltage of a VCM. Then, the proposed method is applied to the load/unload velocity control using 2.5' drives in order to verify its usefulness.

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Shape Optimization of HDD Head Slider for Enhancing Reliabilities (신뢰성 향상을 위한 HDD용 헤드 슬라이더의 형상최적설계)

  • 윤상준;최병렬;최동훈
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2004.05a
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    • pp.753-758
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    • 2004
  • This study is to suggest a probabilistic design determining configurations of slider air bearings with the dimensional manufacturing tolerances of the ABS. The probabilistic design problem is formulated to minimize the variation in flying height from a target value while satisfying the desired probabilities keeping the pitch and roll angles within suitable range. The proposed approach first solves the deterministic optimization problem. Then, beginning with this solution, the RBDO is continued with the probabilistic constraints affected by the random variables with a fixed standard deviation in normal distribution. The RBDO results are directly compared with the values of the initial design and the results of the deterministic optimization, respectively. The reliability analyses are performed by the descriptive sampling (DS) to show the effectiveness and accuracy of the proposed approach. It is demonstrated that the proposed RBDO approach can efficiently obtain an optimum solution satisfying all the desired probabilistic constraints.

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