• 한국작물학회지
• /
• 제40권1호
• /
• pp.1-8
• /
• 1995

중ㆍ산간지대에 재배되는 참당귀의 화성억제에 의한 추대율 감소를 위하여 1992년 2월부터 1994년 11월까지 경북농림진흥원 북부시험장에서 육묘지대, 육묘지간 및 유기물 시용에 따른 화성 및 품질을 비교 분석한 결과를 요약하면 다음과 같다. 1. 육묘지대에 따른 추대율은 표고가 높을수록 현저히 낮았고, 아울러 지하부 생육 및 수량이 200, 400m인 지대보다 양호하여 참당귀의 육묘적지는 적어도 표고 600m 이상이 적당하다고 적당된다. 2. 중ㆍ산간 지대에서는 육묘기간이 짧아질수록 추대율이 현저하게 낮아서 수량은 증수되었지만, extract 및 decursin 함량은 육묘기간이 길어질수록 증가하여 육묘기간과 품질면에서는 반대되는 경향이었다. 3. 유기물 자원별에 따른 추대반응은 단비 시용구보다 유기물 시용구에서 추대율이 낮았으며, 특히 볏짚퇴비에서 가장 낮았고 수량 및 품질반응은 관행재배보다 유기물 시용구에서 양호하였지만 유기물 자원간에는 뚜렷한 차이를 보이지 않았다.

• 한국우주과학회:학술대회논문집(한국우주과학회보)
• /
• 한국우주과학회 2011년도 한국우주과학회보 제20권1호
• /
• pp.24.4-24.4
• /
• 2011

Frozen orbit concept is very useful in designing particular mission orbits including the Sun-synchronous and minimum altitude variation orbits. In this work, variety of frozen and Sun-synchronous orbit conditions around the Moon is investigated and analyzed. The first two zonal harmonics of the Moon, J2 and J3, are considered to determine mean orbital elements to be a frozen orbit. To check the long-term behavior of a frozen orbit, formerly developed YonSei Precise Lunar Orbit Propagator (YSPLOP) is used. First, frozen orbit solutions without conditions to be the Sun-synchronous orbit is investigated. Various mean semi-major axes having between ranges from 1,788 km to 1,938 km with inclinations from 30 deg to 150 deg are considered. It is found that a polar orbit (90 deg of inclination) having 100 km of altitude requires the orbital eccentricity of about 0.01975 for a frozen orbit. Also, mean apolune and perilune altitudes for this case is about 136.301 km and 63.694 km, respectively. Second, frozen orbit solutions with additional condition to be the Sun-synchronous orbit is investigated. It is discovered that orbital inclinations are increased from 138.223 deg to 171.553 deg when mean altitude ranged from 50 km to 200 km. For the most usual mission altitude at the Moon (100 km), the Sun-synchronous orbit condition is satisfied with the eccentricity of 0.01124 and 145.235 deg of inclination. For this case, mean apolune and perilune altitudes are found to be about 120.677 km and 79.323 km, respectively. The results analyzed in this work could be useful to design a preliminary mapping orbit as well as to estimate basic on-board payloads' system requirements, for a future Korea's lunar orbiter mission. Other detailed perturbative effects should be considered in the further study, to analyze more accurate frozen orbit conditions at the Moon.

• Safety and Health at Work
• /
• 제14권3호
• /
• pp.303-308
• /
• 2023

Background: Occupational workers at altitudes are more prone to falls, leading to catastrophic outcomes. Acrophobia, height-related anxiety, and affected executive functions lead to postural instabilities, causing falls. This study investigated the effects of repeated virtual height exposure and training on cognitive processing and height-related anxiety. Methods: Twenty-eight healthy volunteers (age 20.48 ± 1.26 years; mass 69.52 ± 13.78 kg) were recruited and tested in seven virtual environments (VE) [ground (G), 2-story altitude (A1), 2-story edge (E1), 4-story altitude (A2), 4-story edge (E2), 6-story altitude (A3), and 6-story edge (E3)] over three days. At each VE, participants identified occupational hazards present in the VE and completed an Attitude Towards Heights Questionnaire (ATHQ) and a modified State-Trait Anxiety Inventory Questionnaire (mSTAIQ). The number of hazards identified and the ATHQ and mSTAIQ scores were analyzed using a 7 (VE; G, A1, A2, A3, E1, E2, E3) x 3 (DAY; DAY 1, DAY 2, DAY 3) factorial repeated measures analysis of variance. Results: The participants identified the lowest number of hazards at A3 and E3 VEs and on DAY 1 compared to other VEs and DAYs. ATHQ scores were lowest at G, A1, and E1 VEs. Conclusion: Cognitive processing is negatively affected by virtual altitudes, while it improves with short-term training. The features of virtual reality, such as higher involvement, engagement, and reliability, make it a better training tool to be considered in ergonomic settings. The findings of this study will provide insights into cognitive dual-tasking at altitude and its challenges, which will aid in minimizing occupational falls.

• 한국응용곤충학회지
• /
• 제49권3호
• /
• pp.175-185
• /
• 2010

생물다양성(또는 종풍부성)에 미치는 고도 또는 위도 효과는 과거에서부터 현재까지 생물지리학자들의 최대관심사 중 하나라 할 수 있다. 본 연구는 제주도 한라산 24개 습지에 발생하는 수서곤충을 대상으로 고도구배에 따른 출현 종수(종풍부성)의 변화특성을 구명하고 Rapoport의 법칙을 검정하고자 실시하였다. 습지의 면적 효과를 제거하지 않았을 때 해발고도가 증가 할수록 수서곤충 출현 종수는 단조적으로(monotonical) 감소하였고 상관분석결과 통계적으로 유의한 역상관 관계를 보였다(r = -0.64). 고도와 출현 종수의 관계에서 출현 종수를 면적 대비 표준화하여 면적 효과를 제거한 결과 고도의 증가에 따라 처음에는 출현 종수가 증가하다가 최고점을 지나서는 감소하는 전형적인 고봉형 양상(hump-shaped pattern)을 나타냈다. 각 종의 평균 서식고도(수직분포의 중위값)와 수직서식분포 범위와의 관계는 평균 서식고도가 높을수록 분포범위가 증가하는 Rapport의 법칙을 따랐다. 노린재목을 제외하고 평균 서식고도와 수직분포 범위 간에는 정상관을 보였다(잠자리목: r = 0.75, 노린재목: r = -0.22, 딱정벌레목: r = 0.72, 전체: r = 0.55). 또한 상위영역 종은 평균 분포범위가 904.3m로 하위영역 종의 469.5m보다 통계적으로 유의하게 분포범위가 넓었다. 종합적으로 판단할 때 고도별 한라산 습지 수서곤충의 종풍부성 분포는 Rapoport의 법칙에 잘 일치되었다.

• The Korean Journal of Physiology and Pharmacology
• /
• 제18권4호
• /
• pp.313-320
• /
• 2014

The study was conducted to investigate the role of vitamin E in the high altitude hypoxia-induced damage to the intestinal barrier in rats. Sprague-Dawley rats were divided into control (Control), high altitude hypoxia (HH), and high altitude hypoxia + vitamin E (250 mg/kg $BW^*d$) (HV) groups. After the third day, the HH and HV groups were placed in a hypobaric chamber at a stimulated elevation of 7000 m for 5 days. The rats in the HV group were given vitamin E by gavage daily for 8 days. The other rats were given equal volume saline. The results showed that high altitude hypoxia caused the enlargement of heart, liver, lung and kidney, and intestinal villi damage. Supplementation with vitamin E significantly alleviated hypoxia-caused damage to the main organs including intestine, increased the serum superoxide dismutase (SOD) (p< 0.05), diamino oxidase (DAO) (p< 0.01) levels, and decreased the serum levels of interleukin-2 (IL-2) (p< 0.01), interleukin-4 (IL-4) (p<0.001), interferon-gamma ($IFN-{\gamma}$) (p<0.01) and malondialdehyde (MDA) (p<0.001), and decreased the serum erythropoietin (EPO) activity (p<0.05). Administration of vitamin E significantly increased the S-IgA (p<0.001) in ileum and significantly improved the expression levels of occludin and $I{\kappa}B{\alpha}$, and decreased the expression levels of hypoxia-inducible factor 1 alpha and 2 alpha ($HIF-1{\alpha}$ and $HIF-2{\alpha}$), Toll-like receptors (TLR4), P-$I{\kappa}B{\alpha}$ and nuclear factor-${\kappa}B$ p65(NF-${\kappa}B$ P65) in ileum compared to the HH group. This study suggested that vitamin E protectis from intestinal injury caused by high altitude hypoxia environment. These effects may be related to the HIF and TLR4/NF-${\kappa}B$ signaling pathway.

• International Journal of Aeronautical and Space Sciences
• /
• 제17권1호
• /
• pp.1-7
• /
• 2016

The influence of boundary condition of the bodies with gas flows is one of the most important problems in high-altitude aerodynamics. In this paper presents the results of the calculation of aerodynamic characteristics of aerospace vehicle using Monte-Carlo method based on three different gas-surface interaction models - Maxwell model, Cercignani-Lampis-Lord (CLL) model and Lennard-Jones (LJ) potential. These models are very sensitive for force and moment coefficients of aerospace vehicle in the hypersonic free molecular flow. The models, method and results can be used for new generation aerospace vehicle design.

• 한국군사과학기술학회지
• /
• 제7권4호
• /
• pp.138-145
• /
• 2004

Experimental study was conducted on cylindrical supersonic diffuser in order to investigate the effects of the ratios of diffuser area to nozzle throat area (Ad/At), diffuser area to nozzle exit area (Ad/Ae), nozzle exit area to its throat area (Ae/At), and diffuser length to its diameter (L/D), the free volume of vacuum chamber, and the relative distance between nozzle exit and diffuser inlet on the diffuser performance. The study showed that the minimum diffuser starting pressure (Po/Pa)st increased monotonically with increase in (Ad/At) as predicted by the normal shock and momentum theory models and the volume of vacuum chamber affected vacuum pressure level during diffuser operation at lower value of (Ad/Ae). The results of this investigation will be utilized in the design of real-scale high-altitude simulation test facility.

• 한국추진공학회:학술대회논문집
• /
• 한국추진공학회 2006년도 제27회 추계학술대회논문집
• /
• pp.344-352
• /
• 2006

Evacuation performance, starting transient, and plume blowback at diffuser breakdown of a straight cylindrical supersonic exhaust diffuser with no externally supplied secondary flow are investigated. Pressure records in the transitional periods are measured by a small-scale cold-gas simulator. Flow-fields evolving in the diffuser-type ejector are solved by preconditioned Favre-averaged Navier-Stokes equations with a low-Reynolds number $k-{\varepsilon}$ turbulence model edited for turbulence compressibility effects. The present RANS method is properly validated with measured static wall pressure distributions and evacuation level at steady operation as well as the pressure records during the transition regime.

• Journal of Astronomy and Space Sciences
• /
• 제14권1호
• /
• pp.87-93
• /
• 1997

Radiometers in UV and visible wavelengths were onboard the Korean Sounding Rocket(KSR)-1 and 2 which were launched on June 4th and September 1st, 1993. These radiometers were designed to capture the solar radiation during the ascending period of the rocket flight. The purpose of the instrument was to measure the vertical profiles of stratospheric ozone densities. Since the instrument measured the solar radiation from the ground to its apogee, it is possible to investigate the altitude variation of the measured intensity and to estimate the effect of atmospheric scattering by comparing the UV and visible intensity. The visible channel was a reference because the 450-nm wavelength is in the atmospheric window region, where the solar radiation is transmitted through the atmosphere without being absorbed by other atmospheric gases. The use of 450-nm channel intensity as a reference should be limited to the altitude ranges above the certain altitudes, say 20 to 25km where the signals are not perturbed by atmospheric scattering effects.

• 한국추진공학회:학술대회논문집
• /
• 한국추진공학회 2004년도 제23회 추계학술대회 논문집
• /
• pp.47-52
• /
• 2004

극초음속 스크램제트 흡입구의 설계는 다양한 공기열역학적인 현상을 수반한다. 이러한 현상은 무딘 앞전효과, 경계층 발달 문제, 천이, 점성/비점성 결합, 충격파 상호작용, 충격파 경계층 상호작용 및 유동 형상 등을 포함한다. 한정된 마하수와 고도 영역 내에서 운용되기 위해 설계되는 흡입구에서는 이러한 현상들 중 몇 가지 현상에 대한 이해가 요구된다. 본 연구에서는 HyShot 비행시험에서 발생할 수 있는 고도와 받음각 극단에서의 흡입구 성능을 연구하기 위해 몇 가지 중요한 유동 현상(점성 현상, 경계층 박리, 연소기 입구 유동 형상)들이 논의 될 것이다.