Question: Define Kutta-Joukowski theorem.
Options
A : Lift per unit span on the airfoil
B : Drag per unit span on the airfoil
C : Moment per unit span on the airfoil
D : Thrust per unit span on the airfoil
Click to view Correct Answer
Infinitesimal Fluid Element more questions
The relation between pressure and velocity in an inviscid, incompressible....
Which of the following is an application of incompressible flow....
Which of the following parameter can be measured using venturi?
Centre of pressure is defined as the point on the....
Is Kutta-Joukowski theorem is fundamental theorem of aerodynamics?
Is Kutta-Joukowski theorem relate to lift?
Reynold's number is the ratio of __
The aircraft fly in the atmosphere due to which of....
How the circulation around the airfoil?
Airfoil Characteristics more Online Exam Quiz
Finite Control Volume Approach