COMPUTATION OF FIELD STRUCTURE AND AERODYNAMIC CHARACTERISTICS OF DELTA WINGS AT HIGH ANGLES OF ATTACK
vortex breakdown、angle of attack、flowfield characteristics、numerical investigation、numerical simulations、small perturbation、pressure gradients、lateral motion、axial velocity、straight line、delta wing
26
V211.41(基础理论及试验)
Foundation of Aeronautical Science99A53001
2005-07-21(万方平台首次上网日期,不代表论文的发表时间)
共10页
797-806