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报告编号NACA-TN-2476
来源IDNTRS_Document_ID: 19810068677
An Empirical Method Permitting Rapid Determination of the Area, Rate and Distribution of Water-Drop Impingement on an Airfoil of Arbitrary Section at Subsonic Speeds
Bergrun, N. R.
英文摘要An empirical method for the determination of the area, rate, and distribution of water-drop impingement on airfoils of arbitrary section is presented. The procedure represents an initial step toward the development of a method which is generally applicable in the design of thermal ice-prevention equipment for airplane wing and tail surfaces. Results given by the proposed empirical method are expected to be sufficiently accurate for the purpose of heated-wing design, and can be obtained from a few numerical computations once the velocity distribution over the airfoil has been determined. The empirical method presented for incompressible flow is based on results of extensive water-drop. trajectory computations for five airfoil cases which consisted of 15-percent-thick airfoils encompassing a moderate lift-coefficient range. The differential equations pertaining to the paths of the drops were solved by a differential analyzer. The method developed for incompressible flow is extended to the calculation of area and rate of impingement on straight wings in subsonic compressible flow to indicate the probable effects of compressibility for airfoils at low subsonic Mach numbers.
英文关键词AERODYNAMIC INTERFERENCE AIRFOILS INCOMPRESSIBLE FLOW RAINDROPS ICE FORMATION NEPHANALYSIS SUBSONIC FLOW
出版年1951
报告类型Technical Report
语种英语
国家美国
URLhttp://hdl.handle.net/2060/19810068677
资源类型科技报告
条目标识符http://119.78.100.177/qdio/handle/2XILL650/258388
推荐引用方式
GB/T 7714
Bergrun, N. R.. An Empirical Method Permitting Rapid Determination of the Area, Rate and Distribution of Water-Drop Impingement on an Airfoil of Arbitrary Section at Subsonic Speeds,1951.
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