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NASA NTRS ยท 20150003181

Cross Flow Parameter Calculation for Aerodynamic Analysis

Abstract

A system and method for determining a cross flow angle for a feature on a structure. A processor unit receives location information identifying a location of the feature on the structure, determines an angle of the feature, identifies flow information for the location, determines a flow angle using the flow information, and determines the cross flow angle for the feature using the flow angle and the angle of the feature. The flow information describes a flow of fluid across the structure. The flow angle comprises an angle of the flow of fluid across the structure for the location of the feature.

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BibTeXRIS

Norman, David, Jr.. 2014-01-07. Cross Flow Parameter Calculation for Aerodynamic Analysis. https://ntrs.nasa.gov/citations/20150003181

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