Frederick C. Grant
The Use of Pure Twist for Drag Reduction on Arrow Wings with Subsonic Leading Edges
The Use of Pure Twist for Drag Reduction on Arrow Wings with Subsonic Leading EdgesFrederick C. Grant
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Frederick C. Grant
The Use of Pure Twist for Drag Reduction on Arrow Wings with Subsonic Leading Edges

The Use of Pure Twist for Drag Reduction on Arrow Wings with Subsonic Leading Edges

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The results show a 6-percent drag reduction due to twisting a flat delta wing with sonic leading edges and a steady decrease in the gains as sweepback increases.