Pressure Distributions On Blunt Delta Wings At Angles Of Attack Up To 90 Degrees And Mach Number Of 685
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Pressure Measurements on Two 60° Swept Delta Wings with Blunt Leading Edges and Dihedral Angles of 0° and 45° at a Mach Number of 4.95
Author | : P. Calvin Stainback |
Publisher | : |
Total Pages | : 28 |
Release | : 1962 |
Genre | : Airplanes |
ISBN | : |