The zero-lift drag coefficient (CD0) of the Airbus A319-100 is typically around 0.022 to 0.025. This coefficient represents the drag experienced by the aircraft when it is not generating any lift, primarily due to factors like skin friction and pressure drag. Variations in this value can occur based on specific configurations and modifications of the aircraft.
coefficient of drag in 0 lift
0.032
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.
The zero lift drag coefficient (C_D0) of the Airbus A350-1000 is approximately 0.021. The span efficiency factor (e) for the A350-1000 is around 0.85, indicating its aerodynamic efficiency in converting lift into usable flight. These values contribute to the aircraft's overall performance, including fuel efficiency and range.
The 2012 Nissan GT-R has a drag coefficient of 0.26 Cd.
For cylinders coefficient of lift is approximately half of coefficient of drag while they are equal for Aerofoils.
drag coefficient of the 2017 Kia Forte sedan
to reduce drag
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.
The 2009 Scion xD has a drag coefficient of .32 Cd.