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Pressure Port Placement for Lift Distribution Measurement on a Model Aircraft with Optimized Trailing- Edge Flaps

机译：具有优化后缘襟翼的模型飞机的升力分布测量的压力端口位置

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《AIAA guidance, navigation and control conference and exhibit》|2008年|P.1-13|共13页
会议地点 Honolulu, HI(US)
作者
N. Guerreiro; J. Hubbard;
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作者单位

University of Maryland Hampton VA;

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