Static Longitudinal Aerodynamic Characteristics Of Close Coupled Wing Canard Configurations At Mach Numbers From 160 To286

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Static Longitudinal Aerodynamic Characteristics of Close-coupled Wing-canard Configurations at Mach Numbers from 1.60 to 2.86
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An experimental investigation was made in the Mach number range from 1.60 to 2.86 to determine the static longitudinal aerodynamic characteristics of close-coup
Static Longitudinal Aerodynamic Characteristics of Close-coupled Wing-canard Configurations at Mach Numbers from 1.60 To.2.86
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An experimental investigation has been made in the Mach number range from 1.60 to 2.86 to determine the static longitudinal aerodynamic characteristics of close
Longitudinal Aerodynamic Characteristics of a Fighter Model with a Close-coupled Canard at Mach Numbers from 0.40 to 1.20
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Longitudinal Aerodynamic Characteristics of a Fighter Model with a Close-coupled Canard at Mach Numbers from 0.40 to 1.20
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Static Stability and Control of Canard Configurations at Mach Numbers from 0.70 to 2.22 - Trangular Wing and Canard with Twin Vertical Tails
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