Barrett L Shrout

• Aerodynamic characteristics of a series of bodies with variations in nose camber
• Aerodynamic characteristics of a supersonic cruise airplane configuration at Mach numbers of 2.30, 2.96, and 3.30
• Effect of a simulated engine jet blowing above an arrow wing at mach 2.0
• Longitudinal aerodynamic characteristics of an elliptical body with a horizontal tail at mach numbers 2.3 to 4.63
• Surface pressure data for a supersonic-cruise airplane configuration at mach numbers of 2.30, 2.96, and 3.30