Aerodynamic Characteristics Of Several Jet Spoiler Controls On A 45 Degree Sweptback Wing At Mach Numbers Of 161 And 201
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Aerodynamic Characteristics of Several Jet-spoiler Controls on a 45 Degree Sweptback Wing at Mach Numbers of 1.61 and 2.01
| Author | : Douglas R. Lord |
| Publisher | : |
| Total Pages | : 93 |
| Release | : 1958 |
| Genre | : Aerodynamics |
| ISBN | : |
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An investigation has been made in the Langley 4- by 4-foot supersonic pressure tunnel at Mach numbers of 1.61 and 2.01 to determine the aerodynamic characteristics of several jet-spoiler controls on a wing having a 45 degree sweepback of the quarter-chord line, an aspect ratio of 3.5, a taper ratio of 0.3, and an NACA 65A005 airfoil section.
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