Research in the Area of Turbomachinery/Jet Egine Aerodynamics and Computational Fluid Dynamics

涡轮机械/喷气发动机空气动力学和计算流体动力学领域的研究该奖项是根据美国工业化国家科学家和工程师交流计划1987/1988竞赛提出的。该项目旨在使美国科学家和工程师能够在西欧工业化国家以及日本、澳大利亚和新西兰的研究机构进行长期研究。交换奖为进行联合研究和利用国外独特或互补的设施、专门知识和实验条件提供了机会。奖项的评选依据是与其科学领域相关的科学标准、申请人专业发展的前景潜力，以及与促进国际科学与工程合作有关的标准。该项目特别针对正在从事研究工作的科学家和工程师。本研究项目涉及超声速和跨声速涡轮机械转子中三维粘性流动的测量和计算，高速涡轮机械中转子/定子相互作用的研究，以及使用激光传输风速仪和其他高响应探头的流场研究。计算将涉及控制该装置流场的一组11个偏微分方程的解。该项目由宾夕法尼亚州立大学航空航天工程系Budugur Lakshminarayana教授和莱茵-威斯特法利州理工学院Strahlantriebe和Turboarbeitsmaschinen研究所所长H. E. Gallus教授指导，该研究所位于坦普尔格拉本55,5100亚琛。德意志联邦共和国。该奖励建议提供资金，酌情支付国际旅行，国外本地旅行，津贴，家属津贴（如果适用），语言培训（如果需要），以及美国本土机构250美元的固定行政津贴。

Research in the Area of Turbomachinery/Jet Engine Aerodynamics and Computational Fluid Dynamics This award recommendation is made under the U.S.-Industrialized Countries Program for the Exchange of Scientists and Engineers, 1987/1988 Competition. The program is designed to enable U.S. scientists and engineers to conduct long-term research at research institutions in the industrialized countries of Western Europe as well as Japan, Australia and New Zealand. Exchange awards provide opportunities for the conduct of joint research and the utilization of unique or complementary facilities, expertise and experimental conditions in foreign countries. Awards are selected on the basis of scientific criteria relevant to his/her field of science, the prospective potential of the applicants for professional growth, as well as criteria relevant to the furthering of international cooperation in science and engineering. The program is particularly directed to scientists and engineers who are embarking on their research careers. This research project addresses research related to the measurement and computation of three-dimensional viscous flow in supersonic and transonic turbomachinery rotors, a study of rotor/stator interaction in high speed turbomachines, and flow field using a laser transit anemometer as well as other higher response probes. The computation will involve the solution of a set of eleven partial differential equations governing the flow field in this device. The project is under the direction of Professor Budugur Lakshminarayana, Department of Aerospace Engineering, The Pennsylvania State University, University Park, PA 16802, U.S.A., and Professor H. E. Gallus, Director, Institut fuer Strahlantriebe und Turboarbeitsmaschinen, Rhein-Westfalische Technische Hochschule, Templergraben 55, 5100 Aachen, Federal Republic of Germany. This award recommendation provides funds to cover, as appropriate, international travel, local travel abroad, stipend, dependents allowance, if applicable, language training, if required, and a flat administrative allowance of $250 for the U.S. home institution.