Abstract : the flow field mesurement and visualization of the reduced sp ace shuttle model are introduced briefly . that includes the vortex field mesureme nt 、 body pressure distribution mesurement and oil flow visualization . the testing mach nos and angles of attack are 0 . 4 , 0 . 6 , 0 . 8 , 1 . 5 , = 0 ? 文摘:敘述航天飛機簡化模型流場測量與觀察,進行了旋渦場測量,機身壓力分布測量和組合體的油流觀察。