论文信息 - Effect of leading-edge cross-sectional geometry on slender wing unsteady aerodynamics - 字舞流文

Effect of leading-edge cross-sectional geometry on slender wing unsteady aerodynamics

L. Ericsson | H. H. C. King

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[2] N. J. Wood,et al. Control of Vortical Lift on Delta Wings by Tangential Leading-Edge Blowing , 1988 .

[3] E. Polhamus. Predictions of vortex-lift characteristics based on a leading-edge suction analogy. , 1971 .