Results are presented for a section of vanishing thickness in subsonic flow and an NACA 64A006 airfoil in supersonic flow. Good correlation is obtained ... weatherill, w. h. ehlers, f. e 被引量: 2发表: 1980年 Transonic and Supersonic Nonlinear Flutter Characteristics of a Swept-Back Compos...
Results are presented of measurements of the periodical motion of the shock waves on a NACA 64A006 airfoil with oscillating flap in two-dimensional attached transonic flow. It is shown that three different types of shock wave motion can ... H Tijdeman 被引量: 6发表: 1975年 Block implicit ...
NASA NACA-TR-766-1943 NACA模型第84系列流线型机身飞行外壳模型系族的空气动力和水利试验 NASA NACA-TN-1293-1947 带有板条和双开缝襟翼和抽吸边界层控制的NACA 64(下标1)A212翼剖面的试验 NASA NACA-RM-L7K06-1948 在高雷诺数时,带有高升力装置的NACA 65A006机翼的二维风洞研究 ...
NASA NACA-RM-L51K26-1952由美国宇航局 US-NASA 发布于 1952-01-01。 NASA NACA-RM-L51K26-1952 带有NACA 65A006截面和不同板条安排的大型49°后掠角半翼展机翼的力量和压力研究的最新版本是哪一版? NASA NACA-RM-L51K26-1952已经是当前最新版本。