Pressure Distributions on a Flat-plate Delta Wing Swept 65 Deg at a Mach Number of 5.97 at Angles of Attack from 65 Deg to 115 Deg and Angles of Roll from 0 Deg to 25 Deg at a 90 Deg Angle of Attack

Pressure Distributions on a Flat-plate Delta Wing Swept 65 Deg at a Mach Number of 5.97 at Angles of Attack from 65 Deg to 115 Deg and Angles of Roll from 0 Deg to 25 Deg at a 90 Deg Angle of Attack
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Total Pages: 32
Release: 1962
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