大百合属间杂交亲和性、离体培养及耐热生理研究

本实验以大百合和百合东方杂种系“索蚌”为材料，对大百合、百合杂交的亲和性、大百合离体培养及其耐热性进行了研究，以期为大百合与百合杂交育种及相应的耐热百合材料的筛选、种质保存、新品种快繁及栽培应用提供理论依据。 　　以大百合为母本，百合为父本，对属间杂交授粉后花粉管的行为进行观察，结果表明：大百合与百合属间杂交授粉后，百合的花粉在大百合的花柱内的伸长过程中，出现少部分花粉管末端分叉、膨胀或变细，胼胝质大量不规则沉淀，及部分花粉管在伸长过程中受阻等不亲和现象，但大部分花粉仍能够正常萌发，穿过花柱道，进入子房，到达胚珠，且能够观测到早期的胚。虽然杂交亲和性与花粉管的行为有关，但杂交的成功与否还受到受精后诸多因素的影响，还需要从胚胎学和遗传学方面进一步探讨。 　　以大百合的鳞片、叶柄和子房为外植体，进行离体培养，结果表明：大百合的鳞片和叶柄外植体均可成功地诱导小鳞茎，叶柄相对更容易。鳞茎诱导小鳞茎的最佳培养基为MS＋NAA0.5－1.0mg/ml +BA2.5mg/ml +KT2.5mg/ml +蔗糖3%＋琼脂0.7%，28周后，每个外植体平均可以分化4-11个小鳞茎;叶柄诱导小鳞茎的最佳培养基为MS＋NAA1.0－2.0mg/ +BA2.5-3.0mg/ml +KT2.5-3.0mg/ml +蔗糖3%＋琼脂0.7%，26周后，每个外植体平均可以分化3-9个小鳞茎。同时也发现，用鳞茎作为外植体，污染率较高。在大百合的子房离体培养实验中发现：BA和KT 是影响大百合子房分化途径的关键因素，其浓度分别为0.1-1.0mg/L、2.0-4.0 mg/L和高于4.0mg/L时，外植体分别分化为愈伤组织、芽和叶。外植体分化的基本培养基以N6、B5为佳。愈伤组织诱导小鳞茎的最佳培养基为MS+0.1-0.5mg/L NAA +2.5mg/L BA+2.5mg/L KT +10%蔗糖+0.7%琼脂。在1/2MS +3%的蔗糖+0.7%琼脂+1%活性炭的生根培养基上，生根率为100%。炼苗一周后移栽，长势良好。 　　对长至5－6片真叶的大百合植株在不同高温（30℃、35℃和40℃）下，分别进行4h、10h及24h(热胁迫10h，然后在22℃对照温度下缓苗14h)的热胁迫处理，测定了不同处理下，植株的净光合速率（Pn），实际光化学效率（φPS2），最大光化学效率（Fv/Fm）和叶片的相对电导率，游离脯氨酸含量，可溶性蛋白含量，以及叶片中超氧化物歧化酶（SOD）和过氧化氢酶(CAT)的活性。结果表明：大百合对30℃的高温胁迫有较好的适应能力，表现为可溶性蛋白、游离脯氨酸等渗透调节物质的积累，抗氧化酶活性的提高，以及缓苗后细胞膜的自我修复和光合能力的恢复;随着胁迫温度的升高（35℃、40℃）和胁迫时间的延长（4h、10h），大百合一方面对高温胁迫做出了积极的响应，另一方面，光系统的光合能力，细胞膜的稳定性，抗氧化酶的活性，也受到了一定程度的伤害，在缓苗后,细胞膜的稳定性、细胞的渗透势、抗氧化酶的活性等都在一定程度上得到恢复。 　　

Heat transfer and aerodynamics of turbine blade tips in a linear cascade

Local measurements of the heat transfer coefficient and pressure coefficient were conducted on the tip and near tip region of a generic turbine blade in a five-blade linear cascade. Two tip clearance gaps were used: 1.6% and 2.8% chord. Data was obtained at a Reynolds number of 2.3 × 10 5 based on exit velocity and chord. Three different tip geometries were investigated: a flat (plain) tip, a suction-side squealer, and a cavity squealer. The experiments reveal that the flow through the plain gap is dominated by flow separation at the pressure-side edge and that the highest levels of heat transfer are located where the flow reattaches on the tip surface. High heat transfer is also measured at locations where the tip-leakage vortex has impinged onto the suction surface of the aerofoil. The experiments are supported by flow visualisation computed using the CFX CFD code which has provided insight into the fluid dynamics within the gap. The suction-side and cavity squealers are shown to reduce the heat transfer in the gap but high levels of heat transfer are associated with locations of impingement, identified using the flow visualisation and aerodynamic data. Film cooling is introduced on the plain tip at locations near the pressure-side edge within the separated region and a net heat flux reduction analysis is used to quantify the performance of the successful cooling design. copyright © 2005 by ASME.

The effect of work processes on the casing heat transfer of a transonic turbine

This paper considers the effect of the rotor tip on the casing heat load of a transonic axial flow turbine. The aim of the research is to understand the dominant causes of casing heat-transfer. Experimental measurements were conducted at engine-representative Mach number, Reynolds number and stage inlet to casing wall temperature ratio. Time-resolved heat-transfer coefficient and gas recovery temperature on the casing were measured using an array of heat-transfer gauges. Time-resolved static pressure on the casing wall was measured using Kulite pressure transducers. Time-resolved numerical simulations were undertaken to aid understanding of the mechanism responsible for casing heat load. The results show that between 35% and 60% axial chord the rotor tip-leakage flow is responsible for more than 50% of casing heat transfer. The effects of both gas recovery temperature and heat transfer coefficient were investigated separately and it is shown that an increased stagnation temperature in the rotor tip gap dominates casing heat-transfer. In the tip gap the stagnation temperature is shown to rise above that found at stage inlet (combustor exit) by as much as 35% of stage total temperature drop. The rise in stagnation temperature is caused by an isentropic work input to the tip-leakage fluid by the rotor. The size of this mechanism is investigated by computationally tracking fluid path-lines through the rotor tip gap to understand the unsteady work processes that occur. Copyright © 2005 by ASME.

LES and hybrid LES/RANS simulations for conjugate heat transfer over a matrix of cubes

Large Eddy Simulation (LES) and a novel k -l based hybrid LES/RANS approach have been applied to simulate a conjugate heat transfer problem involving flow over a matrix of surface mounted cubes. In order to assess the capability and reliability of the newly developed k -l based hybrid LES/RANS, numerical results are compared with new LES and existing RANS results. Comparisons include mean velocity profiles, Reynolds stresses and conjugate heat transfer. As well as for hybrid LES/RANS validation purposes, the LES results are used to gain insights into the complex flow physics and heat transfer mechanisms. Numerical simulations show that the hybrid LES/RANS approach is effective. Mean and instantaneous fluid temperatures adjacent to the cube surface are found to strongly correlate with flow structure. Although the LES captures more mean velocity field complexities, broadly time averaged wake temperature fields are found similar for the LES and hybrid LES/RANS. Copyright © 2005 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.

Heat budget studies of the north Arabian Sea during summer and winter seasons, 1992

In this study heat budget components and momentum flux for August and January 1992 over the north Arabian Sea are computed. The marine meteorological data measured on board during the cruises of PAK-US joint project (NASEER) are used for the computation. Significant differences were found in the heat budget components as well as in the momentum flux during different monsoon periods over the north Arabian Sea. The latent heat flux was always positive and attributed to the large vapour pressure gradient. The computed moisture and latent heat fluxes in January were higher than August The highest value of latent heat flux 309 W/m2 at station 8 was evaluated. These higher latent heat fluxes were due to the large vapour pressure gradient, air-sea temperature difference, the wind speed, and the prevailing wind direction (from north and northeast). Negative values of sensible heat fluxes in both seasons indicate that the heat transfer was from the atmosphere to the ocean. The negative values of net heat gain indicate that the sea surface field became an energy sink: or the sea surface supplied more energy to the atmosphere than it received from it. Large variation in the momentum flux mainly attributed to the variation in the wind speed. Aerial averages of heat and momentum fluxes were also computed.