NASA NASA-TM-X-1658
NASA NASA-TM-X-1658 1968-JAN-01 Aerodynamc characterstcs of bodes of revoluton at Mach numbers from 150 to 286 and angles of attack to 180 deg
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Aerodynamic characteristics of bodies of revolution at Mach numbers from 1.50 to 2.86 and angles of attack to 180 deg