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- W2364993487 abstract "The research was done on a typical canard configuration with twin-tails to find why tails always reduce the lift at high angle-of-attack by using CFD method.It was found that the vortices passing above induced a sideslip flow field in the region tails located.The tails thus had higher pressure on the inboard side which put an adverse pressure gradient in the field.It was this gradient to weaken and destabilize the vortices and then to reduce the vortex lift on the whole model.Based on the findings,three improving measures were designed,which were small size vertical tails,toe-in vertical tails and different tail incline angles.The wind tunnel test results showed that the first two received expected effects." @default.
- W2364993487 created "2016-06-24" @default.
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- W2364993487 date "2012-01-01" @default.
- W2364993487 modified "2023-09-23" @default.
- W2364993487 title "A study on the measures to cut down twin-tails' unfavorable influences" @default.
- W2364993487 hasPublicationYear "2012" @default.
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