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

Effect of leading-edge geometry on delta wing unsteady aerodynamics

Lars E. Ericsson | H. H. C. King

[1] K. Gersten. Nichtlineare Tragflächentheorie insbesondere für Tragflügel mit kleinem Seitenverhältnis , 1961 .

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

[3] N. Yu,et al. Navier-Stokes calculations for attached and separated flows using different turbulence models , 1991 .

[4] Eli Turkel,et al. Effect of artificial viscosity on three-dimensional flow solutions , 1990 .

[5] J. P. Reding,et al. Unsteady Aerodynamics of Slender Delta Wings at Large Angles of Attack , 1975 .

[6] Ramesh K. Agarwal,et al. Navier-Stokes calculations of transonic viscous flow about wing/bodyconfigurations , 1987 .

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

[8] Eastman N. Jacobs,et al. Airfoil section characteristics as affected by variations of the Reynolds number , 1939 .

[9] L. E. Ericsson,et al. Rapid prediction of high-alpha unsteady aerodynamics of slender-wingaircraft , 1992 .

[10] Veer N. Vatsa,et al. Development of an efficient multigrid code for 3-D Navier-Stokes equations , 1989 .