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- W2109146733 abstract "such as the ones encountered during takeoff and approach. This method is for rapid prototyping during the conceptual design stage with a goal to predict the performance or the change of lift coefficient within 5–10% of accuracy. This method includes three parts: an alternate approach for estimating jet speed without assuming the jet staticpressureattheexit,anempiricalapproachforestimatingtheliftcoefficientsofcirculation-controlairfoils,and a lifting-line theory for estimating wing-lift curves based on the airfoil-lift data. The validation against the windtunnel test data available for a modified Intruder A-6 aircraft with a circulation-control wing was deemed" @default.
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- W2109146733 date "2012-09-01" @default.
- W2109146733 modified "2023-10-18" @default.
- W2109146733 title "Rapid-Prototyping Method for Modeling a Circulation-Control Wing at Low Speeds" @default.
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- W2109146733 doi "https://doi.org/10.2514/1.c031742" @default.
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