干旱区生态环境知识资源中心(Arid): Point drag and total drag of navy struts no. 1 modified

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报告编号	NACA-TR-137
来源ID	NTRS_Document_ID: 19930091204
	Point drag and total drag of navy struts no. 1 modified
	Zahm, A F; Smith, R H; Hill, G C
英文摘要	This report deals with the results of tests on struts conducted at Washington Navy Yard. Two models of the modified Navy strut, no. 1, were tested in the 8 by 8 foot wind tunnel. The tests were made to determine the total resistance end effect and the pressure distribution at various wind-tunnel speeds with the length of the strut transverse to the current. Only the measurements made at zero pitch and yaw are given in this report.
英文关键词	AIRFOILS STRUTS AERODYNAMIC DRAG WIND TUNNEL TESTS DRAG MEASUREMENT PRESSURE DRAG FRICTION DRAG PRESSURE DISTRIBUTION AIRSPEED LENGTH THICKNESS NAVY
出版年	1923
语种	英语
国家	美国
URL	http://hdl.handle.net/2060/19930091204
资源类型	科技报告
条目标识符	http://119.78.100.177/qdio/handle/2XILL650/258196
推荐引用方式 GB/T 7714	Zahm, A F,Smith, R H,Hill, G C. Point drag and total drag of navy struts no. 1 modified,1923.