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>Calculated Drag of an Aerial Refueling Assembly Through Airplane Performance Analysis
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Calculated Drag of an Aerial Refueling Assembly Through Airplane Performance Analysis
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机译:通过飞机性能分析计算空中加油总成的阻力
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摘要
This viewgraph document reviews NASA Dryden's work on Aerial refueling, with specific interest in calculating the drag of the refueling system. The aerodynamic drag of an aerial refueling assembly was calculated during the Automated Aerial Refueling project at the NASA Dryden Flight Research Center. An F/A-18A airplane was specially instrumented to obtain accurate fuel flow measurements and to determine engine thrust
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