• Title/Summary/Keyword: Longitudinal Pitch

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NUMERICAL ANALYSIS FOR LONGITUDINAL PITCH EFFECT ON TUBE BANK HEAT TRANSFER (관군 배열에서의 종간 간격이 열전달에 미치는 영향에 대한 수치 해석적 연구)

  • Lee, D.;Ahn, J.;Shin, S.
    • Journal of computational fluids engineering
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    • v.17 no.3
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    • pp.39-44
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    • 2012
  • In this study, a longitudinal pitch effect on in-line tube bank heat transfer has been analyzed numerically. To verify the accuracy of the solver model and boundary conditions, global Nusselt number(Nu) and pressure drop across the 2 row tube bank are compared with the existing experimental correlations under 500 ~ 2,000 Reynolds number(Re) range. By changing transverse pitch($S_T$) or longitudinal pitch($S_L$) separately in tube bank, we're trying to identify the each effect on heat transfer. We found that the effect of transverse pitch can be accounted for Reynolds number evaluated with maximum velocity($V_{max}$) at the smallest flow area similar to most existing correlations. Variation of the longitudinal pitch($S_L$) has a greater impact on the heat transfer compared to the transverse pitch($S_T$). Overall Nusselt number increases with larger longitudinal pitch($S_L$), however individual Nusselt number of the tube row has significant difference after the first row.

Experimental Study on Hydrofoil Arrangement and Longitudinal Moment Characteristics for Navigation Safety of High Speed Craft (고속선 운항 안정성을 위한 수중익 배치 및 종모멘트 특성에 관한 실험적 연구)

  • Park, Hwa-Pyeong;Kim, Sang-Hyun;Lim, Geun-Nam
    • Journal of the Korean Society of Marine Environment & Safety
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    • v.20 no.4
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    • pp.443-450
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    • 2014
  • In this study, we have discussed about the effect of hydrofoil arrangement and longitudinal moment characteristic on longitudinal motion stability of fully-submerged hydrofoil by the experiment of tandem hydrofoil model. First of all, tandem hydrofoil model that has canard wing arrangement has been made and characteristics of lift force and drag force by performing the lift force and drag force measuring experiment has also been estimated. Besides, tandem hydrofoil model's wing arrangement which has the initial stability and self stability of longitudinal motion has also been determined. In longitudinal stability experiment of tandem hydrofoil model, the motion characteristic of pitch and heave and the longitudinal stability of foil borne condition by variation of self stability of longitudinal moment and longitudinal distance are estimated. The result from the experiment and it's important conclusion can be described as below; Increase the self stability for longitudinal moment, the higher self stability for pitch motions in a constant pitch angles. By increasing the self stability for longitudinal moment, the range of fluctuation of pitch motion and heave motion for pitch angle also will change relatively small and longitudinal stability is excellent. Lastly, when the lift force of hydrofoil is remain constants, we can conclude that securing the enough self stability for longitudinal moment is essential for stable foil borne condition of tandem hydrofoil.

A Study on Longitudinal Phugoid Mode Affected by Application of Nonlinear Control Laws

  • Kim, Chong-Sup;Hur, Gi-Bong;Kim, Seung-Jun
    • International Journal of Aeronautical and Space Sciences
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    • v.8 no.1
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    • pp.21-31
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    • 2007
  • Relaxed Static Stability (RSS) concept has been applied to improve aerodynamic performance of modern version supersonic jet fighter aircraft. The T-50 advanced supersonic trainer employs the RSS concept in order to improve the aerodynamic performance. And the flight control system stabilizes the unstable aircraft and provides adequate handling qualities. The T-50 longitudinal control laws employ a proportional-plus-integral type controller based on a dynamic inversion method. The longitudinal dynamic modes consist of short period with high frequency and phugoid mode with low frequency. The design goal of longitudinal control law is optimization of short period damping ratio and frequency using Lower Order Equivalent System (LOES) complying the requirement of MIL-F-8785C. This paper addresses phugoid mode characteristics such as damping ratio and natural frequency that is affected by the nonlinear control laws such as angle of attack limiter, auto pitch attitude command system and autopilot of pitch attitude hold.

Longitudinal motion characteristics of a ship according to the location (선내 위치에 따른 선박의 종운동 특성)

  • Kang, Il-Kwon;Kim, Min-Seok;Park, Byung-Soo;Hong, Jin-Keun;Jeong, Seong-Jae;Ham, Sang-Jun
    • Journal of the Korean Society of Fisheries and Ocean Technology
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    • v.48 no.2
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    • pp.147-154
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    • 2012
  • In head sea, a ship has mainly the longitudinal motion such as vertical acceleration and pitch. In that case, the motion characteristics of a ship will have changed as the location different from each of place vertically and horizontally on board. The author carried out an experiment about the ship's vertical acceleration and pitch according to the location for the head sea, and analyzed the data with the aid of the statistical and spectral analyzing method to get the motion characteristics of the vessels. The response of vertical acceleration and pitch not deeply depend on the decks vertically, but displayed the relative big different value horizontally even if same deck. The biggest response of vertical acceleration and pitch among the accommodations was shown at scientist room, but the value of it not reached to the minimum requirement of ISO 2631-1 for working on board.

Study on Heat Transfer Characteristics of Discrete Fin-and-tube Heat Exchangers (독립 핀-튜브 열교환기의 열전달 성능특성에 관한 연구)

  • Lee, Ho-Seong;Kim, Yong-Han;Choi, Jong-Min;Kim, Yong-Chan
    • Proceedings of the SAREK Conference
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    • 2005.11a
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    • pp.274-280
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    • 2005
  • The objective of this study Is to investigate the heat transfer performance of plate discrete fin-and-tube heat exchangers with large fin pitch. In this study, twenty-two heat exchangers were tested with a variation of fin pitch, number of tube row, longitudinal tube pitch and fin alignment. Discrete fin type exchangers improved heat transfer performance more than 10% compared to tile continuous fin type heat exchangers. The air-side heat transfer coefficient decreased with a reduction of the fin pitch and an increase of the number of tube row, The staggered fin alignment improved heat transfer performance more than 6% compared to the inline fin alignment. The effect of longitudinal tube pitch was insignificant on the j-factor and experiments found opposite effects on the j-factor with respect to fin alignment. Heat transfer correlations were developed from the measured data for flat plate discrete fin-and-tube heat exchangers with large fin pitch. The correlations yielded good predictions of the measured data with mean deviations of 1,4% and 0.3% for tire inline and staggered tube alignment, respectively.

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A Case of Pitch Elevation Procedure after Transsexual Operation

  • 유영삼;이수성;장혁기;이창환
    • Proceedings of the KSLP Conference
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    • 1998.11a
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    • pp.199-199
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    • 1998
  • 국내 이비인후과 영역에서 성전환 수술과 병행하여 사용되는 pitch elevation 술식에 대한 보고는 거의 없다. pitch elevation 술식에는 cricothyroid approximation, A-P expansion of the thyroid ala, longitudinal incision in the cords, intrachondral injection of the steroid and evaporation of the cords by $CO_2$ laser 등의 술식이 있다. (중략)

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Study on High Performance and Compact Absorber Using Small Diameter Heat Exchanger Tube

  • Yoon Jung-In;Phan Thanh Tong;Moon Choon-Geun;Kim Eun-Pil;Kim Jae-Dol;Kang Ki-Cheol
    • Journal of Advanced Marine Engineering and Technology
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    • v.30 no.4
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    • pp.463-473
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    • 2006
  • The effect of tube diameter on heat and mass transfer characteristics of absorber in absorption chiller/heater using LiBr solution as a working fluid has been investigated by both of numerical and experimental study to develop a high performance and compact absorber. The diameter of the heat exchanger tube inside absorber was changed from 15.88mm to 12.70mm and 9.52mm. In numerical study a model of vapor pressure drop inside tube absorber based on a commercial 20RT absorption chiller/heater was performed. The effect of tube diameter, longitudinal pitch, vapor Reynolds number, longitudinal pitch to diameter ratio on vapor pressure drop across the heat exchanger tube banks inside absorber have been investigated and found that vapor pressure drop decreases as tube diameter increases, longitudinal pitch increases, vapor Reynolds number decreases and longitudinal pitch to diameter ratio increases. In experimental study, a system includes a tube absorber, a generator, solution distribution system and cooling water system was set up. The experimental results shown that the overall heat transfer coefficient, mass transfer coefficient. Nusselt number and Sherwood number increase as solution flow rate increases. In both of study cases, the heat and mass transfer performance increases as tube diameter decreases. Among three different tube diameters the smallest tube diameter 9.52mm has highest heat and mass transfer performance.

VALIDATION OF GRID AND BOUNDARY CONDITIONS FOR OPTIMAL DESIGN OF HEAT RECOVERY SYSTEM (열 회수 시스템의 최적 설계를 위한 격자 및 경계 조건 검증에 관한 연구)

  • Lee, D.G.;Shin, S.W.
    • 한국전산유체공학회:학술대회논문집
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    • 2011.05a
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    • pp.608-609
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    • 2011
  • In this study, we tried to validate FLUENT solver model and domain setting for the problem of convective heat transfer in multiple tube bank under transitional zone. We have paid special attention to verify proper boundary conditions and the grid convergence. Through validation work, it is found that unsteady solution method with two-dimensional simulation domain can produce reasonable accurate results compared with existing experimental data. Simulation results with steady solution generates relatively large error. We found that both steady and unsteady method for three-dimensional domain shows acceptable accuracy. Further parametric study for deriving correlation from transverse and longitudinal pitch is currently underway.

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비행선 자세각에 따른 부력중심 이동 및 종적 정안정성

  • Lee, Yung-Gyo;Kim, Dong-Min;Lee, Jin-Woo
    • Aerospace Engineering and Technology
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    • v.2 no.2
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    • pp.18-24
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    • 2003
  • Center of buoyancy moves along with pitch attitude variation, which causes Helium gas inclination. In this paper, movement of center of buoyancy and corresponding variation of longitudinal static stability were observed. The effect of separating wall, which is placed in the envelop to minimize movement of center of buoyancy was also investigated. Installation of separating wall was proved to be essential for current design, because movement of center of buoyancy aggravates longitudinal static stability. Investigation of longitudinal static stability for various speeds reveals a 50m airship is statically stable only in a low speed regime.

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