AviationTire
›
Principles Of Flight - Aeroplane
›
Subsonic Aerodynamics
›
The total drag
Q 2 / 5
▾
All topics
Subsonic Aerodynamics
Transonic Aerodynamics
Supersonic Aerodynamics
Stability
Control
Limitations
Propellers
Flight Mechanics
All subtopics
Basics, laws and definitions
The two-dimensional airflow about an aerofoil
The coefficients
The three-dimensional airflow about an aeroplane
The total drag
The ground effect
The relation between the lift coefficient and the speed for constant lift
The stall
CLmax augmentation
Means to decrease the CL - CD ratio, increasing drag
The boundary layer
Special circumstances
Subscribe
Topics
Subjects
Log in
Minimum total drag of an aircraft occurs:
when induced drag is minimum.
at the stalling speed.
when profile drag equals induced drag.
at the best rate of climb speed.
← Previous
Next →