Aerodynamic Characteristics of Several Jet-spoiler Controls on a 45 Degree Sweptback Wing at Mach Numbers of 1.61 and 2.01
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Publications and source records attributed to Lord, Douglas R.
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An investigation has been made at Mach numbers of 1.61 and 2.01 and Reynolds numbers from 1.7 X 10 to 7.6 X 10 to determine the pressure distributions over a 60 deg. delta wing having 20 different control configurations. Measurements were made at angles of attack from O deg to 15 deg for control deflections from -30 deg to 30 deg. This report presents the complete tabulated pressure data for the range of test conditions.
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