NASA NACA-RM-L52G18-1952
當雷諾數為0.4x10(指數6)至3.0x10(指數6)時,變種對帶有矩形平面和三個低展弦比的對稱機翼低速空氣動力特性的影響研究
Investigation of the effects of variations in the Reynolds number between 0.4 x 10(exp 6) and 3.0 x 10(exp 6) on the low-speed aerodynamic characteristics of three low-aspect-ratio symmetrical wings with rectangular plan forms