• 제목/요약/키워드: time of stall

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Analytical Surge Behaviors in Systems of a Single-stage Axial Flow Compressor and Flow-paths

  • Yamaguchi, Nobuyuki
    • International Journal of Fluid Machinery and Systems
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    • 제9권1호
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    • pp.1-16
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    • 2016
  • Behaviors of surges appearing near the stall stagnation boundaries in various fashions in systems of a single-stage compressor and flow-path systems were studied analytically and were tried to put to order. Deep surges, which enclose the stall point in the pressure-mass flow plane, tend to have either near-resonant surge frequencies or subharmonic ones. The subharmonic surge is a multiple-loop one containing, for example, in a (1/2) subharmonic one, a deep surge loop and a mild surge loop, the latter of which does not enclose the stall point, staying only within the stalled zone. Both loops have nearly equal time periods, respectively, resulting in a (1/2) subharmonic surge frequency as a whole. The subharmonic surges are found to appear in a narrow zone neighboring the stall stagnation boundary. In other words, they tend to appear in the final stage of the stall stagnation process. It should be emphasized further that the stall stagnation initiates fundamentally at the situation where a volume-modified reduced resonant-surge frequency becomes coincident with that for the stagnation boundary conditions, where the reduced frequency is defined by the acoustical resonance frequency in the flow-path system, the delivery flow-path length and the compressor tip speed, modified by the sectional area ratio and the effect of the stalling pressure ratio. The real surge frequency turns from the resonant frequency to either near-resonant one or subharmonic one, and finally to stagnation condition, for the large-amplitude conditions, caused by the non-linear self-excitation mechanism of the surge.

진동하는 날개의 3차원 동실속에 관한 수치해석 (Numerical Analysis of Three Dimensional Dynamic Stall of an Oscillating Wing)

  • 고성호
    • 대한기계학회논문집B
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    • 제25권1호
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    • pp.62-70
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    • 2001
  • Three-dimensional dynamic stall over an oscillating wing has been analyzed by using a compressible Navier-Stokes code. The code solved the thin-layer Navirer-Stokes equations with a second-order time accuracy for a semispan wing with 0.3048m chord, a NACA 0015 airfoil section, and zero twist Computations were made for a freestream Mach number of 0.29, a chord Reynolds number of 1.95$\times$10(sup)6 and a reduced frequency equal to 0.1. Numerical results were compared with experimental data which include the hysteresis of lift, drag and moment at various wing span. The comparison reveals the quantitative as well as qualitative nature of the three-dimensional dynamic stall.

항공기의 고도, 속도 및 깊은 실속의 회복을 위한 자동회복장치 설계 및 검증에 관한 연구 (A Study on the Design and Validation of Automatic Pitch Rocker System for Altitude, Speed and Deep Stall Recovery)

  • 김종섭
    • 제어로봇시스템학회논문지
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    • 제15권2호
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    • pp.240-248
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    • 2009
  • Modem version of supersonic jet fighter aircraft must have been guaranteed appropriate controllability and stability in HAoA(High Angle of Attack). The HAoA flight control law have two parts, one is control law of departure prevention and the other is control law of departure recovery support. The control laws of departure prevention for advanced jet trainer consist of HAoA limiter, roll command limiter and rudder fader. The control laws of departure recovery support are consist of yaw-rate limiter and MPO(Manual Pitch Override) mode. The guideline of pitch rocking using MPO mode is simple, but operating skill of pitch rocking is very difficult by the pilot with inexperience of departure situation. Therefore, automatic deep stall recovery system is necessary. The system called the "Automatic Pitch Rocker System" or APRS, provided a pilot initiated automatic maneuver capable of an aircraft recoveries in situations of deep stall, speed and altitude. This paper addresses the design and validation for APRS to recovery of an deep stall without manual pitch rocking by the pilot. Also, this system is designed to recovery of speed, attitude and altitude after deep stall recovery using ATCS (Automatic Thrust Control System) and autopilot. Finally, this system is verified by real-time pilot evaluation using HQS (Handling Quality Simulator).

Effect of Different Feeding Systems on Carcass and Non-Carcass Parameters of Black Bengal Goat

  • Moniruzzaman, M.;Hashem, M.A.;Akhter, S.;Hossain, M.M.
    • Asian-Australasian Journal of Animal Sciences
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    • 제15권1호
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    • pp.61-65
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    • 2002
  • The experiment was conducted to find out the effect of four feeding systems namely; stall feeding, tethering, restricted grazing and grazing on carcass characteristics of Black Bengal goat. Twenty four does of approximately 1 year of age were randomly selected for four treatments of feeding systems having 6 replications in each. Stall fed goats were kept into house all time and adequate amount of natural grass were supplied for ad libitum feeding. Goats of tethering group were tethered for eating natural grass from 8 a.m. to 4 p.m. and were transferred after one hour interval for changing the grazing place. Goats of restricted grazing group were allowed for grazing from 8 a.m. to 1 p.m. Goats of grazing group were grazed for 8 a.m. to 4 p.m. Concentrate supplement was given at the rate of 150 g per day per goat for all of the treatment groups. Goats were slaughtered after the experiment of 219 days. Body length and height at wither were significantly higher in stall feeding group than others. Average dressing percentage were 42.18, 39.0, 36.79 and 34.0 for stall feeding, tethering, restricted grazing and grazing groups, respectively. Dressing percentage varied significantly (p<0.05) among feeding groups. Caul fat and empty gut weight differed significantly (p<0.05) in all of the feeding systems but others non-carcass parameters did not differ significantly. Percentage of dry matter and ether extract were also significantly (p<0.05) higher in stall fed groups. In conclusion, among four treatment groups, performance of stall fed goats were most satisfactory and then tethering showed better performance than any other groups.

A Comparison of Surge Behaviors in Multi-Stage and Single-Stage Axial Flow Compressors

  • Yamaguchi, Nobuyuki
    • International Journal of Fluid Machinery and Systems
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    • 제9권4호
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    • pp.338-353
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    • 2016
  • Information on the surge behaviors and stall stagnation boundaries for a nine-stage axial flow compressor are summarized on the basis of analytical data in comparison with those for a single-stage one, with attention to the pressure ratio effect. The general trends of the surge loop behaviors of the pressure-mass flow are similar for both compressors including the fact that the subharmonic surges tend to appear very near the stall stagnation boundaries. With respect to the nine-stage compressor, however, the mild loops in the subharmonic surges tend to be very small in size relative to the deep loops, and at the same time, insufficient surge recovery phenomenon, which is a kind of subharmonic surge, appears also far from the stagnation boundary for relatively short delivery flow-paths. The latter is found to be a rear-stage surge caused by unstalling and re-stalling of the rear stages with the front-stages kept in stall in the stalled condition of the whole compressor, which situation is caused by stage-wise mismatching in the bottom pressure levels of the in-stall multi-stage compressor. The fundamental information on the stall stagnation boundaries is given by a group of normalized geometrical parameters including relative delivery flow-path length, relative suction flow-path length, and sectional area-pressure ratio, and by another group of normalized frequency parameters including relative surge frequencies, modified reduced resonance frequencies, and modified reduced surge frequencies. Respective groups of the normalized parameters show very similar tendency of behaviors for the nine-stage compressor and the single-stage compressor. The modified reduced resonance frequency could be the more reasonable parameter suggesting the flow-induced oscillation nature of the surge phenomena. It could give the stall stagnation boundary in a more unified manner than the Greitzer's B parameter.

터보프롭 항공기의 스핀/실속 회복장치 설계 (Design for Spin/Stall Recovery Parachute System of Turbo-prop Airplane)

  • 이동훈;노병찬;강명각;강경우;이주하
    • 한국항공우주학회지
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    • 제40권8호
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    • pp.726-736
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    • 2012
  • 본 논문은 KC-100 소형민항기의 스핀시험을 위해 장착될 스핀회복장치의 설계 및 지상활주 전개 시험에 대해 기술하였다. 스핀회복장치에 대한 상세 설계 단계에서 공력, 구조, 안정성, 조종성 등에 대한 해석적 결과를 토대로 낙하산 단위면적당 라이저 길이, 낙하산 다공성, 낙하산 펼침 시간, 및 전개방법 등의 설계 변수를 결정했다. 본 시스템의 검증을 위해 항공기에 스핀회복장치를 장착한 상태에서 기능점검 후 KC-100 고속활주 중 스핀슈트 전개를 수행했다.

멀티코어 시스템에서 TLB Lockdown에 의한 TLB Miss 영향 분석 (Investigation on TLB Miss Impact through TLB Lockdown in Multi-core Systems)

  • 송대영;박시형;김형신
    • 대한임베디드공학회논문지
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    • 제17권1호
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    • pp.59-65
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    • 2022
  • Virtual memory is used as the method to ensure the safety of the system through memory protection in the real-time system. TLB miss caused by using virtual memory makes the real-time system WCET more pessimistically. TLB lockdown can be applied as a method to improve this problem. However, processors with limited TLB lockdown entries, a selection criterion is needed to efficiently utilize the TLB lockdown entry. In this paper, the most frequently accessed virtual pages in the process are applied to the TLB lockdown by analyzing memory profiling. The results showed that micro data TLB miss stall cycle and main data TLB miss stall cycle of the processor decreased by at least 4.7% and up to 29.7%.

도로변 구두수선대 실내.외의 이산화질소 농도 및 거리에 따른 이산화질소 감소 - 서울시와 아산시의 비교 연구 - (Indoor and Outdoor $NO_2$ Concentration of Shoe-stall near Busy Road and $NO_2$ Decay by Distance from Roadside - Comparative Study between Seoul and Asan -)

  • 양원호;손부순;박종안;김종오
    • 환경위생공학
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    • 제17권2호
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    • pp.85-91
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    • 2002
  • Workers who work at indoor and outdoor environment near busy road are suspected to be exposed to high-elevated air pollutant levels during working hours. This study evaluated the working-time nitrogen dioxide ($NO_2$) exposure for workers (repairmen and polishers) of shoe-stalls. Since shoe-stalls have particularly been located near busy road in Korea, workers might be high exposure to $NO_2$ from traffic exhaust as well as indoor sources of shoe-stall such as portable gas range (butane gas) during working hours. In this study, we measured the indoor and outdoor $NO_2$ concentrations of shoe-stalls. Simultaneously, outdoor $NO_2$ concentrations of building through sidewalk from shoe-stall were measured. High $NO_2$ exposure for workers of shoe-stalls was considered to be inflow of outdoor source of exhausted emission from vehicles and indoor source from usage of gas range to polish the shoe. Indoor/outdoor $NO_2$ concentration ratio ($0.94{\pm}0.22$) in Seoul was higher than that ($1.06{\pm}0.34$) in Asan, because ambient $NO_2$ level was high in Seoul and usage of gas range was prevalent in Asan. According to $NO_2$ concentrations by distance from roadside to building through sidewalk, $NO_2$ concentrations showed the decreased trend with distance. The results of this study can be utilized by municipal authorities in urban planning for evaluating effects of future traffic planning and land use.

동적실속 수동제어장치 최적설계 (Design Optimization of Passive Control Devices for Dynamic Stall Control)

  • 주완돈;이보성;이관중;이동호
    • 한국항공우주학회지
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    • 제33권1호
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    • pp.11-19
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    • 2005
  • 본 연구에서는 진동 운동하는 익형의 동적실속 특성을 향상시키기 위하여, 고정 앞전 Droop과 Gurney 플랩의 크기와 위치에 대한 최적설계를 수행하였다. 고정 앞전 Droop이 모멘트 특성의 개선에 효율적이나 양력특성의 저하를 유발 할 수 있다. 반면에 Gurney 플랩은 양력특성의 향상을 가져오지만, 모멘트특성을 악화시키는 특성이 있다. 고정앞전 Droop의 설계변수는 상호 보완적인 특성을 갖는 위치와 각도를 설정하였으며, Gurney 플랩은 그 길이를 설계변수로 설정하였다. 또한, 동적실속과 같이 비선형성이 강한 문제의 설계를 위해서 고차 다항식의 반응면 기법과 민감도 기반의 최적설계 기법을 사용하였다. 최적화는 양력과 모멘트 특성이 동시에 개선되도록 수행 하였다. 설계 결과 동적실속의 양력, 모멘트 및 항력특성의 향상을 가져올 수 있었으며, 가변 앞전 Droop과 Gurney 플랩을 결합한 능동제어장치에 버금가는 동적실속 제어 효과를 갖을 수 있음을 확인하였다.

Cacao bean husk: an applicable bedding material in dairy free-stall barns

  • Yajima, Akira;Owada, Hisashi;Kobayashi, Suguru;Komatsu, Natsumi;Takehara, Kazuaki;Ito, Maria;Matsuda, Kazuhide;Sato, Kan;Itabashi, Hisao;Sugimura, Satoshi;Kanda, Shuhei
    • Asian-Australasian Journal of Animal Sciences
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    • 제30권7호
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    • pp.1048-1053
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    • 2017
  • Objective: The objectives of the study were to assess the effect of cacao bean husk as bedding material in free-stall barn on the behavior, productivity, and udder health of dairy cattle, and on the ammonia concentrations in the barn. Methods: Four different stall surfaces (no bedding, cacao bean husk, sawdust, and chopped wheat straw) were each continuously tested for a period of 1 week to determine their effects on nine lactating Holstein cows housed in the free-stall barn with rubber matting. The lying time and the milk yield were measured between d 4 and d 7. Blood samples for plasma cortisol concentration and teat swabs for bacterial counts were obtained prior to morning milking on d 7. The time-averaged gas-phase ammonia concentrations in the barn were measured between d 2 and d 7. Results: The cows spent approximately 2 h more per day lying in the stalls when bedding was available than without bedding. The milk yield increased in the experimental periods when cows had access to bedding materials as compared to the period without bedding. The lying time was positively correlated with the milk yield. Bacterial counts on the teat ends recorded for cows housed on cacao bean husk were significantly lower than those recorded for cows housed without bedding. Ammonia concentration under cacao bean husk bedding decreased by 6%, 15%, and 21% as compared to no bedding, sawdust, and chopped wheat straw, respectively. The cortisol concentration was lowest in the period when cacao bean husk bedding was used. We observed a positive correlation between the ammonia concentrations in the barn and the plasma cortisol concentrations. Conclusion: Cacao bean husk is a potential alternative of conventional bedding material, such as sawdust or chopped wheat straw, with beneficial effects on udder health and ammonia concentrations in the barns.