NASA NASA-TM-78813
NASA NASA-TM-78813 1979-JAN-01 Wnd-tunnel force and flow vsualzaton data at Mach numbers from 16 to 463 for a seres of bodes of revoluton at angles of attack from mnus 4 deg to 60 deg
Cart
(empty)
Flow visualization and force data for a series of six bodies of revolution are presented without analysis. The data were obtained in the Langley Unitary Plan wind tunnel for angles of attack from -4 deg to 60 deg. The Reynolds number used for these tests was 6,600,000 per meter.