干旱区生态环境知识资源中心(Arid): An experimental investigation of internal area ruling for transonic and supersonic channel flow

Arid

报告编号	NASA-CR-169638, NAS 1.26:169638
来源ID	NTRS_Document_ID: 19830005797
	An experimental investigation of internal area ruling for transonic and supersonic channel flow
	Roberts, W. B.; Vanrintel, H. L.; Rizvi, G.
英文摘要	A simulated transonic rotor channel model was examined experimentally to verify the flow physics of internal area ruling. Pressure measurements were performed in the high speed wind tunnel at transonic speeds with Mach 1.5 and Mach 2 nozzle blocks to get an indication of the approximate shock losses. The results showed a reduction in losses due to internal area ruling with the Mach 1.5 nozzle blocks. The reduction in total loss coefficient was of the order of 17 percent for a high blockage model and 7 percent for a cut-down model.
英文关键词	CHANNEL FLOW SUPERSONIC FLOW TRANSONIC FLOW PRESSURE MEASUREMENT TRANSONIC WIND TUNNELS TRAPEZOIDAL WINGS
出版年	1982
报告类型	Technical Report
语种	英语
国家	美国
URL	http://hdl.handle.net/2060/19830005797
资源类型	科技报告
条目标识符	http://119.78.100.177/qdio/handle/2XILL650/258931
推荐引用方式 GB/T 7714	Roberts, W. B.,Vanrintel, H. L.,Rizvi, G.. An experimental investigation of internal area ruling for transonic and supersonic channel flow,1982.