For no lift, The induced drag will be zero. However, there will still be drag due to viscous forces and pressure forces.
coefficient of drag in 0 lift
The zero lift drag coefficient of a Boeing 747 is approximately 0.022. This value represents the drag force experienced by the aircraft when it is not generating lift.
0.032
For cylinders coefficient of lift is approximately half of coefficient of drag while they are equal for Aerofoils.
The zero lift drag coefficient (C_D0) for the Airbus A340 is typically around 0.025 to 0.030. This value represents the drag experienced by the aircraft when it is not generating lift, primarily due to factors such as skin friction and form drag. Exact values can vary based on specific configurations and conditions, but this range is commonly referenced in aerodynamic studies for the A340.
17.4
The 2012 Nissan GT-R has a drag coefficient of 0.26 Cd.
LIft = coefficient times density times velocity squared times wing area divided by 2 drag= coefficient times density times velocity squared over 2 times reference area
drag coefficient of the 2017 Kia Forte sedan
The 2007 Volkswagen Jetta has a drag coefficient of 0.31 Cd.
The 2007 Lexus IS-250 has a drag coefficient of 0.28 Cd.
The 2006 Chevrolet Corvette has a drag coefficient of .28 Cd.