Zero Lift Drag Coefficient Given By Thrust Calculator

The zero lift drag coefficient, CD0, quantifies an aircraft’s drag when it produces no lift at zero angle of attack. It’s a dimensionless parameter determined by the body’s shape, surface characteristics, and other non-lift generating factors. Lower CD0 values signify reduced drag during level flight, enhancing fuel efficiency and overall aerodynamic performance. The formula to calculate Zero lift drag coefficient as follows:

Where:

  • is the zero lift drag coefficient.
  • is the thrust in N.
  • is the dynamic pressure in Pa.
  • is the reference area m2.
  • is the induced drag coefficient.

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