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    Effect of sweep angle on the pressure distributions and effectiveness of the ogee tip in diffusing a line vortex (1973)
    In:  CASI
    Details
    Publication Date: 2019-06-27
    Description: Low-speed wind tunnel tests were conducted to study the influence of sweep angle on the pressure distributions of an ogee-tip configuration with relation to the effectiveness of the ogee tip in diffusing a line vortex. In addition to the pressure data, performance and flow-visualization data were obtained in the wind tunnel tests to evaluate the application of the ogee tip to aircraft configurations. The effect of sweep angle on the performance characteristics of a conventional-tip model, having equivalent planform area, was also investigated for comparison with the ogee-tip configuration. Results of the investigation generally indicate that sweep angle has little effect on the characteristics of the ogee in diffusing a line vortex.
    Keywords: AERODYNAMICS
    Type: NASA-CR-132355 , RASA-73-07
    Format: application/pdf
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