INFLUENCE OF NOSE PERTURBATIONS ON BEHAVIORS OF ASYMMETRIC VORTICES OVER SLENDER BODY
SLENDER BODY、asymmetric vortices、slender body、saddle point、topological structure、pressure measurement、machining tolerances、Reynolds number、wind tunnel、test model
18
O3(力学)
国家自然科学基金10172017;the Foundation of National Key Laboratory of Aerodynamic Design and Research00JS51.3.2 HK01
2007-07-26(万方平台首次上网日期,不代表论文的发表时间)
共13页
581-593