• 대한기계학회논문집B
• /
• 제31권4호
• /
• pp.357-366
• /
• 2007

The present study investigated local heat/mass transfer characteristics on the surface of the rotating turbine blade with various incidence angles. The experiments are conducted in a low speed annular cascade with a single stage turbine. The blade has a flat tip with the mean tip clearance of 2.5% of the blade chord. A naphthalene sublimation method is used to measure detailed mass transfer coefficient on the blade. At design condition, the inlet Reynolds number is $Re_c=1.5{\times}10^5$ which results in the blade rotation speed of 255.8 rpm. Also, the effect of off-design condition is examined with various incidence angles between $-15^{\circ}$ and $+7{\circ}$. The results indicated that the incidence angle has significant effects on the blade surface heat transfer. In mid-span region, the laminar separation region on the pressure side is reduced and the laminar flow region on the suction side shrinks with increasing incidence angle. Near the tip, the effect of tip leakage flow increases in span wise and axial directions as the incidence angle decreases because the tip leakage flow is formed near the suction side surface. However, the effect of tip leakage flow is reduced with positive incidence angle.

• 대한기계학회논문집B
• /
• 제31권4호
• /
• pp.349-356
• /
• 2007

The present study investigated local heat/mass transfer characteristics on the tip of the rotating turbine blade with various incoming flow incidence angles. The experiments are conducted in a low speed annular cascade with a single stage turbine. The blade has a flat tip with a mean tip clearance of 2.5% of the blade chord. The incoming flow Reynolds number is $1.5{\times}10^5$ at design condition. To examine the effect of off-design condition, the experiments with various incidence angles ranging between $-15^{\circ}$ and $+7{\circ}$ were conducted. A naphthalene sublimation method is used to measure detailed mass transfer coefficient on the blade. The results indicated that the incidence angle strongly affects the behavior of tip leakage flow around the blade tip and consequently plays an important role in determining heat transfer characteristics on the tip. For negative incidence angles, the heat/mass transfer in the upstream region on the tip decreases by up to 20%. On the contrary, for positive incidence angles, much higher heat transfer coefficients are observed even with small increase of incidence angle.

• Wind and Structures
• /
• 제31권3호
• /
• pp.255-267
• /
• 2020

A systematic set of low-speed wind tunnel experiments was performed at Re = 6.5×10⁴ and 1.1×10⁵ to study the mean wind loading experienced by surface-mounted finite-height square prisms for different aspect ratios, incidence angles, and boundary layer thicknesses. The aspect ratio of the prism was varied from AR = 1 to 11 in small increments and the incidence angle was changed from α = 0° to 45° in increments of 1°. Two different boundary layer thicknesses were used: a thin boundary layer with δ/D = 0.8 and a thick boundary layer with δ/D = 2.0-2.2. The mean drag and lift coefficients were strong functions of AR, α, and δ/D, while the Strouhal number was mostly influenced by α. The critical incidence angle, at which the prism experiences minimum drag, maximum lift, and highest vortex shedding frequency, increased with AR, converged to a value of α_c = 18° ± 2° once AR was sufficiently high, and was relatively insensitive to changes in δ/D. A local maximum value of mean drag coefficient was identified for higher-AR prisms at low α. The overall behaviour of the force coefficients and Strouhal number with AR suggests the possibility of three flow regimes.

• 대한원격탐사학회지
• /
• 제13권1호
• /
• pp.57-73
• /
• 1997

본 연구는 산악 지형의 레이더(SAR) 영상자료에서 흔히 볼 수 있는 지형의 기복에 의한 화소값의 왜곡 보정과 관련된 것이다. 연구 자료로는 RADARSAT 위성에서 얻어진 서울 남쪽 관악산과 안양 지역의 SAR 영상자료를 이용하였고, 영상자료의 보정을 위하여 SAR 영상과 유사 한 해상력을 갖춘 수치고도자료(digital elevation model)를 제작하였다. 레이더 영상자료는 먼저 각 화소가 가지고 있는 기하학적 왜곡을 보정하여 정확한 지도좌표에 등록함으로써, 수치고도자 료로부터 각 화소 지점의 구체적인 지형적 특성에 관한 자료를 산출하였다. 영상의 각 화소값에 미치는 지형적 영향을 분석하기 위한 기하학적 인자로서 각 지점에 입사되는 레이더파와 경사면 의 연직선이 이루는 유효입사각(local incidence angle)을 산출하였다. 수치지도로 제작된 임상도 를 이용하여 동일한 임분특성을 가지고 있는 산림내에서 얻어지는 레이더 반사치와 유효입사각의 관계를 분석하였다. 영상자료의 지형효과 보장은 실험적인 방법에 의하여 수행되었는데, 유효입사 각과 레이더 반사치와의 관계에서 도출된 지형에 의한 영향을 나타내는 수식을 적용하였다. 보정 결과는 육안에 의한 영상의 비교와 함께 현지자료를 이용하여 검증하였다.

• 대한원격탐사학회:학술대회논문집
• /
• 대한원격탐사학회 2002년도 Proceedings of International Symposium on Remote Sensing
• /
• pp.435-440
• /
• 2002

The objective of this study is to analyze the relationship between polarimetric radar backscatters and stand characteristics over the mountainous forest area. L- and P-band full polarimetric airborne SAR data obtained in September 2000 were processed to compare with forest stand maps and ground collected stand variables. After the geometric registration of SAR image, mean radar backscatters were extracted for those ground plots where the stand parameters, such as tree height, DBH, and basal area, were measured during and after the SAR data acquisition. Preliminary analysis was focused on the topographic influence of radar backscattering under the homogeneous forest stand condition. Topographic effects, assessed by the local incidence angles, were different obvious in L-band data while it was not clear with P-band data.

• 대한원격탐사학회:학술대회논문집
• /
• 대한원격탐사학회 2006년도 Proceedings of ISRS 2006 PORSEC Volume I
• /
• pp.504-507
• /
• 2006

Airborn Lidar technology has been applied to diverse applications with the advantages of accurate 3D information. Further, Lidar intensity, backscattered signal power, can provid us additional information regarding target's characteristics. Lidar intensity varies by the target reflectance, moisture condition, range, and viewing geometry. This study purposes to generate normalized airborne LiDAR intensity image considering those influential factors such as reflectance, range and geometric/topographic factors (scan angle, ground height, aspect, slope, local incidence angle: LIA). Laser points from one flight line were extracted to simplify the geometric conditions. Laser intensities of sample plots, selected by using a set of reference data and ground survey, werethen statistically analyzed with independent variables. Target reflectance, range between sensor and target, and surface slope were main factors to influence the laser intensity. Intensity of laser points was initially normalized by removing range effect only. However, microsite topographic factor, such as slope angle, was not normalized due to difficulty of automatic calculation.

• Wind and Structures
• /
• 제4권5호
• /
• pp.399-412
• /
• 2001

Simultaneous pressure and force measurements have been conducted on a stationary box deck section model for two configurations (namely without and with New Jersey traffic barriers) at various angles of incidence. The mean and fluctuating aerodynamic coefficients and pressure coefficients were derived, together with their spectra and with the coherence functions between the pressures and the total aerodynamic forces. The mean aerodynamic coefficients derived from force measurements are first compared with those derived from the integration of the pressures on the deck surface. Correlation between forces and local pressures are determined in order to gain insight on the wind excitation mechanism. The influence of the angle of incidence on the pressure distribution and on the fluctuating forces is also analysed. It is evidenced how particular deck section areas are more responsible for the aerodynamic excitation of the deck.

• 대한기계학회논문집B
• /
• 제28권7호
• /
• pp.800-808
• /
• 2004

Wind tunnel test of an airplane model with forward swept wing was done in KARI LSWT to evaluate and measure the aerodynamic characteristics of initially designed configuration. Since the given wing planform did not fully satisfy the design requirements, local flow control devices such as vortilon, vortex generator and flow fence were used to delay separation and to enhance aerodynamic characteristics. Also decision making processes of design parameters such as vertical tail boom length, the location, size and the incidence angle of horizontal tail were discussed. The general aerodynamic characteristics of forward swept wing for various control surface deflection conditions of flap, aileron and elevator were also given.

• 한국수자원학회:학술대회논문집
• /
• 한국수자원학회 1987년도 제29회 수공학연구발표회논문초록집
• /
• pp.87-87
• /
• 1987

교각은 때때로 국소세굴에 의헤 손상을 받는다. 교각구조의 국소세굴 문제는 광범위하게 연구되었지만, 세굴심을 정량적으로 산정하는 것은 어렵다. 본연구는 정적세굴 조건하에서 여러형태로 배치된 반원 및 장방형 교각주변의 국소세굴에 대한 것으로 차원해석을 통하여 세굴심은 $$, $$ 및 $$등에 관계됨을 파악하여 무차원 시간에 따른 무차원 세굴심의 변화(토사수, 교각경과 길이, 영각의 영향), 와도, 저항력에 따른 세굴심의 변화들이 세굴심산정공식을 얻기위해 설험적으로 연구되었으며 최재 세굴심 산정공식이 얻어졌다.

• 물과 미래
• /
• 제20권1호
• /
• pp.41-47
• /
• 1987

교각은 때때로 국소세굴에 의해 손상받는다. 교각주변의 국소세굴 문제는 광법위하게 연구되었지만, 세굴심을 정량적으로 산정하는 것은 어렵다. 본연구는 정적세굴 조건하에서 형태로 배치된 반원 및 장방형 교각주변의 국소세굴에 대한 것으로 차원해석을 통하여 세굴심은 Re, Fr, 및 Ns등에 관계됨을 파악하여 무차원 시간에 따른 무차원 세굴심의 변화(상사수, 교각경과 길이 , 영각의 영향), 와도, 저항력에 따른 세굴심의 변화들이 세굴심산정공식을 얻기위해 실험적으로 연구되었으며 최대 세굴심 산정공식이 얻어졌다.