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Leading edge channel for enhancement of lift/drag ratio and reduction of sonic boom
Leading edge channel for enhancement of lift/drag ratio and reduction of sonic boom
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机译:前缘通道可提高升/降比并减少音爆
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摘要
The leading edges of wings, nose assemblies, tails, fins, struts, and other components of aircraft, atmospheric entry vehicles and missiles in which the leading edge is blunted and the flight Mach number is supersonic, are provided with passive airflow channel, resulting in significantly reduced wave drag and total drag, significantly increased lift-to-drag ratio, and reduced sonic boom.
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