Bianca T. Anderson

• Effects of wing sweep on boundary-layer transition for a smooth F-14A wing at Mach numbers from 0.700 to 0.825
• Effects of wing sweep on in-flight boundary-layer transition for a laminar flow wing at Mach numbers from 0.60 to 0.79
• Overview of supersonic laminar flow control research on the F-16XL ships 1 and 2
• Techniques used in the F-14 variable-sweep transition flight experiment