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Wind Tunnel Test Data Report of a Powered 1/5Scale ARL/Bell V/STOL Aircraft Model. Phase II,

机译:动力1/5scale aRL / Bell V / sTOL飞机模型的风洞试验数据报告。第二阶段,

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摘要

Tests of a 1/5 scale powered V/STOL aircraft model were conducted in the Langley 7 x 10 wind tunnel. Vehicle aerodynamics and stability and control characteristics were investigated. The test results are presented without analysis.

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