SHELBY COBRA

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SHELBY COBRA AERODYNAMIC IMPROVEMENT AND
HARDTOP DESIGN
Eric Jacobs Professor Anderson MER 197 Fall 2004
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Progress to Date

• Baseline wind tunnel testing on 118 model
• Pressure taps (20, 40, 60Hz)
• PIV (30, 50Hz)
• Lift Drag (25, 30, 35, 40, 45Hz, had to repair
  model)

• Other Achievements
• 2D CFD of Cobra (50 m/s 30Hz)
• Foam/Body filler debacle of 110 model
• Design/construction of FFR Spec Series
  windscreen and air dam

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Lift Drag
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CDF vs PIV (_at_ 30Hz)
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