• Title/Summary/Keyword: Body performance

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Cavitation studies on axi-symmetric underwater body with pumpjet propulsor in cavitation tunnel

  • Suryanarayana, Ch.;Satyanarayana, B.;Ramji, K.;Rao, M. Nageswara
    • International Journal of Naval Architecture and Ocean Engineering
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    • v.2 no.4
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    • pp.185-194
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    • 2010
  • A pumpjet propulsor (PJP) was designed for an underwater body (UWB) with axi-symmetric configuration. Its performance was predicted through CFD study and models were manufactured. The propulsor design was evaluated for its propulsion characteristics through model tests conducted in a Wind Tunnel (WT). In the concluding part of the study, evaluation of the cavitation performance of the pumpjet was undertaken in a cavitation tunnel (CT). In order to assess the cavitation free operation speeds and depths of the body, cavitation tests of the PJP were carried out in behind condition to determine the inception cavitation numbers for rotor, stator and cowl. The model test results obtained were corrected for full scale Reynolds number and subsequently analyzed for cavitation inception speeds at different operating depths. From model tests it was also found that the cavitation inception of the rotor takes place on the tip face side at higher advance ratios and cavitation shifts towards the suction side as the RPS increases whereas the stator and cowl are free from cavitation.

A Study on the Behavior of Ambient Hydraulic Cycling Test for 70 MPa Type3 Hydrogen Composite Cylinder (70 MPa용 Type 3 수소 복합용기의 상온수압반복 거동에 관한 연구)

  • Cho, Sung-Min;Kim, Chang-Jong;Kim, Young-Gyu
    • Journal of the Korean Institute of Gas
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    • v.16 no.1
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    • pp.46-50
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    • 2012
  • The performance of the Type3 hydrogen composite cylinder whose pressure is 70 MPa using hydrostatic cycling test equipment was evaluted in this study. It also includes the finite element method analysis on the performance of the cylinder when the pressure is applied. As a result, cylinder body parts of the Type3 hydrogen composite cylinder, which draws attention with its safe status and the lightness, was ruptured first and the same result has been found out through the finite element method. The dome knuckle and the cylinder body were proved as the weakest parts since the cylinder body parts was expanded under the pressure.

Plasma Leptin and Performance of Purebred and Backcrossed Hereford throughout Grazing and Feedlot Fattening

  • Vega, R.A.;Hidari, H.;Matsunaga, N.;Kuwayama, H.;Manalo, D.D.;Lee, H.G.;Hata, H.
    • Asian-Australasian Journal of Animal Sciences
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    • v.17 no.7
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    • pp.954-959
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    • 2004
  • In a herd of 24 spring-born steers, plasma leptin and performance of selected purebred (n=5) and backcrossed Hereford (n=5) were compared in a year-round summer grazing and winter feedlot fattening. Bimonthly blood collection and body weight measurement were accomplished. The plasma samples were analyzed for leptin, insulin, total cholesterol, triglyceride, NEFA and glucose. The experimental design utilized one-way ANOVA with breed as the treatment. The purebred obtained higher plasma NEFA (p<0.001) compared to backcross, regardless of seasonal feeding systems (SFS). The backcross showed gradual increase and nonresponsiveness of plasma leptin to SFS. During summer grazing, attenuation of plasma leptin and sudden elevation when shifted to winter feedlot fattening were observed in purebred. Plasma leptin obtained linear relationship with body weight of purebred (r=0.53;p<0.001) and backcrossed Hereford (r=0.49; p<0.01). The purebred and backcrossed Hereford, when shifted to summer grazing, resulted to sustained and restricted daily gain, respectively. Therefore, cattle breeds of higher growth potential exhibit significant elevation of plasma leptin after 400 kg BW, when animal starts to deposit significant body fat.

PERFORMANCE AND CARCASS TRAITS OF DOCKED AND INTACT FAT-TAILED NAJDI LAMBS

  • Abouheif, M.A.;Kraidees, M.S.;Shatat, R.A.
    • Asian-Australasian Journal of Animal Sciences
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    • v.6 no.1
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    • pp.135-138
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    • 1993
  • Twelve intact and 12 docked Najdi lambs of equal numbers of males and females were utilized in the experiment. All lambs were raised under similar conditions until they attained 40 kg shorn and shrunk body weight. Thereafter, lambs were individually fed ad libitum on a diet formulated to contain 11.20 MJ ME/kg and slaughtered after 60 days feeding period. The results showed that Najdi rams averaged 6.14 kg more total gain (p < .05), required 6.80 kg less feed (p < .05) per kg of gain and produced 3.2 and 3.07 kg more (p < .05) carcass and salable cuts weights over the feeding period than comparable ewes. Body wall thickness and kidney and pelvic fat weight were greater (p < .05) for ewes than for rams; dressing percent, longissimus area and fat thickness were not significantly influenced by sex of lambs. Docked lambs kept for 60 days on feed required 1.80 kg less feed (p < .05) per kg of gain and produced 2.21 kg more (p < .05) salable wholesale cuts weight than intact lambs. Docking was not a significant source of variation for total gain, carcass weight, dressing percent, longissimus dorsi area, body wall thickness and fat thickness.

Modeling and Performance Analysis of MAC Protocol for WBAN with Finite Buffer

  • Shu, Minglei;Yuan, Dongfeng;Chen, Changfang;Wang, Yinglong;Zhang, Chongqing
    • KSII Transactions on Internet and Information Systems (TIIS)
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    • v.9 no.11
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    • pp.4436-4452
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    • 2015
  • The IEEE 802.15.6 standard is introduced to satisfy all the requirements for monitoring systems operating in, on, or around the human body. In this paper, analytical models are developed for evaluating the performance of the IEEE 802.15.6 CSMA/CA-based medium access control protocol for wireless body area networks (WBAN) under unsaturation condition. We employ a three-dimensional Markov chain to model the backoff procedure, and an M/G/1/K queuing system to describe the packet queues in the buffer. The throughput and delay performances of WBAN operating in the beacon mode are analyzed in heterogeneous network comprised of different user priorities. Simulation results are included to demonstrate the accuracy of the proposed analytical model.

Modeling and Autopilot Design of Blended Wing-Body UAV

  • Min, Byoung-Mun;Shin, Sung-Sik;Shim, Hyun-Chul;Tahk, Min-Jea
    • International Journal of Aeronautical and Space Sciences
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    • v.9 no.1
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    • pp.121-128
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    • 2008
  • This paper describes the modeling and autopilot design procedure of a Blended Wing-Body(BWB) UAV. The BWB UAV is a tailless design that integrates the wing and the fuselage. This configuration shows some aerodynamic advantages of lower wetted area to volume ratio and lower interference drag as compared to conventional type UAV. Also, BWB UAV may be increase payload capacity and flight range. However, despite of these benefits, this type of UAV presents several problems related to flying qualities, stability, and control. In this paper, the detailed modeling procedure of BWB UAV and stability analysis results using the linearized model at trim condition are represented. Finally, we designed the autopilot of BWB UAV based on a simple control allocation scheme and evaluated its performance through nonlinear simulation.

The development and Performance test of the Cook Top type Gas valve for the slim-line style Gas Range (슬림라인형 가스레인지용 쿡탑형 가스 밸브의 개발과 작동 성능 검증)

  • Kim, Sang-Ju;Lee, Sang-Cheol;Ju, Kwang-Myung;Lee, Han-Jong;Chang, In-Bae
    • 유체기계공업학회:학술대회논문집
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    • 2003.12a
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    • pp.568-572
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    • 2003
  • The height of valve body is limited to 30mm in the cook-top style gas valves for the domestic gas ranges. But the all the safety specifications of KS should be fulfilled and the magnetic power unit(MPU) should be installed in the valve body for the safety reason. The length of MPU body is longer than the 30mm that it should be located in the square direction of the knob shaft and therefore the implementation of the lever mechanism to transmit the press motion of the knob to the MPU valve is very difficult. In this paper, the hinged lever with inclined plate is used to transmit the press motion of the knob to the MPU valve. The analysis of the gas flow with using the commercial software of FLOW-3D shows that the gas flow capacity is fit for the domestic gas range. The performance and responsibility of the valve is tested for the mass production and the test results shows that the valve can be installed in the commercial gas range.

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Experimental Study on Hydrodynamic Performance and Wave Power Takeoff for Heaving Wave Energy Converter (수직 진자형 파력 발전 장치의 운동성능 및 파력 추출에 관한 실험적 연구)

  • Kim, Sung-Jae;Koo, WeonCheol;Min, Eun-Hong;Jang, Hoyun;Youn, Donghyup;Lee, Byeongseong
    • Journal of Ocean Engineering and Technology
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    • v.30 no.5
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    • pp.361-366
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    • 2016
  • The aim of this study was to experimentally investigate the hydrodynamic performance of a hemispheric wave energy converter (WEC) and its wave power takeoff. The WEC is a heaving body-type point absorber with a hydraulic-pump power take-off (PTO) system. The hydraulic PTO system consists of a hydraulic cylinder, hydraulic motor, and generator, with consideration given to the hydraulic pressure and flow rate. Two body model shapes, including the original hemisphere and a bottom-chopped hemisphere, were considered. The heave RAOs of the two models were evaluated for various body drafts. The effects of the hydraulic PTO system on the RAOs were also investigated.

Parametric geometric model and shape optimization of an underwater glider with blended-wing-body

  • Sun, Chunya;Song, Baowei;Wang, Peng
    • International Journal of Naval Architecture and Ocean Engineering
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    • v.7 no.6
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    • pp.995-1006
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    • 2015
  • Underwater glider, as a new kind of autonomous underwater vehicles, has many merits such as long-range, extended-duration and low costs. The shape of underwater glider is an important factor in determining the hydrodynamic efficiency. In this paper, a high lift to drag ratio configuration, the Blended-Wing-Body (BWB), is used to design a small civilian under water glider. In the parametric geometric model of the BWB underwater glider, the planform is defined with Bezier curve and linear line, and the section is defined with symmetrical airfoil NACA 0012. Computational investigations are carried out to study the hydrodynamic performance of the glider using the commercial Computational Fluid Dynamics (CFD) code Fluent. The Kriging-based genetic algorithm, called Efficient Global Optimization (EGO), is applied to hydrodynamic design optimization. The result demonstrates that the BWB underwater glider has excellent hydrodynamic performance, and the lift to drag ratio of initial design is increased by 7% in the EGO process.

Proposal of a hierarchical topology and spatial reuse superframe for enhancing throughput of a cluster-based WBAN

  • Hiep, Pham Thanh;Thang, Nguyen Nhu;Sun, Guanghao;Hoang, Nguyen Huy
    • ETRI Journal
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    • v.41 no.5
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    • pp.648-657
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    • 2019
  • A cluster topology was proposed with the assumption of zero noise to improve the performance of wireless body area networks (WBANs). However, in WBANs, the transmission power should be reduced as low as possible to avoid the effect of electromagnetic waves on the human body and to extend the lifetime of a battery. Therefore, in this work, we consider a bit error rate for a cluster-based WBAN and analyze the performance of the system while the transmission of sensors and cluster headers (CHs) is controlled. Moreover, a hierarchical topology is proposed for the cluster-based WBAN to further improve the throughput of the system; this proposed system is called as the hierarchical cluster WBAN. The hierarchical cluster WBAN is combined with a transmission control scheme, that is, complete control, spatial reuse superframe, to increase the throughput. The proposed system is analyzed and evaluated based on several factors of the system model, such as signal-to-noise ratio, number of clusters, and number of sensors. The calculation result indicates that the proposed hierarchical cluster WBAN outperforms the cluster-based WBAN in all analyzed scenarios.