干旱区生态环境知识资源中心(Arid): Results of investigations on a 0.0405 scale model ATP version of the NR-SSV orbiter in the North American Aeronautical Laboratory low speed wind tunnel

Arid

报告编号	NASA-CR-120092, DMS-DR-2016
来源ID	NTRS_Document_ID: 19730013105
	Results of investigations on a 0.0405 scale model ATP version of the NR-SSV orbiter in the North American Aeronautical Laboratory low speed wind tunnel
	Mennell, R.; Vaughn, J. E.; Singellton, R.
英文摘要	Experimental aerodynamic investigations were conducted on a scale model space shuttle vehicle (SSV) orbiter. The purpose of the test was to investigate the longitudinal and lateral-directional aerodynamic characteristics. Emphasis was placed on model component, wing-glove, and wing-body fairing effects, as well as elevon, aileron, and rudder control effectiveness. Angles of attack from - 5 deg to + 30 deg and angles of sideslip from - 5 deg to + 10 deg were tested. Static pressures were recorded on base, fuselage, and wing surfaces. Tufts and talc-kerosene flow visualization techniques were also utilized. The aerodynamic force balance results are presented in plotted and tabular form.
英文关键词	SCALE MODELS SPACE SHUTTLE ORBITERS SPACECRAFT CONFIGURATIONS SPACECRAFT CONTROL WIND TUNNEL STABILITY TESTS AERODYNAMIC CHARACTERISTICS LATERAL STABILITY LONGITUDINAL STABILITY SUBSONIC SPEED
出版年	1973
报告类型	Technical Report
语种	英语
国家	美国
URL	http://hdl.handle.net/2060/19730013105
资源类型	科技报告
条目标识符	http://119.78.100.177/qdio/handle/2XILL650/258517
推荐引用方式 GB/T 7714	Mennell, R.,Vaughn, J. E.,Singellton, R.. Results of investigations on a 0.0405 scale model ATP version of the NR-SSV orbiter in the North American Aeronautical Laboratory low speed wind tunnel,1973.