Aerodinamika
Aerodynamics Quiz
Test your knowledge on the fascinating principles of aerodynamics with this engaging quiz! Challenge yourself with questions covering Bernoulli’s principle, thermodynamics, viscosity, and more.
Whether you're a student, teacher, or aviation enthusiast, this quiz is designed to enhance your understanding of aerodynamics and its applications.
- Multiple choice questions
- Thought-provoking scenarios
- Browser-friendly interface
Bernoulli’s principle is derived from which of the following?
Conservation of energy
Conservation of momentum
Newton’s law of motion
Stagnation pressure or the total pressure is the sum of
Kinetic and potential energy
Kinetic energy +potential energy +gravity
Static and dynamic pressure
Conservation of energy is based on which law of thermodynamics
Zeroth
First
Second
Third
In a thermodynamic system, the measurement of heat is called as
Enthaply
Entropy
Internal energy
Heat trensfer
Which of the following has more viscosity
Water
Honey
Oil
Juice
The nature of the boundary layer depends on
Re
M
Gh
T
How lift and drag ratio can be expressed in a relation?
Dividing the lift coefficient by the drag coefficient
Dividing the lift coefficient by the moment coefficient
Dividing the drag coefficient by the lift coefficient
Dividing the drag coefficient by the moment coefficient
Is lift to drag ratio, maximum at zero degrees angle of attack?
False
True
The flow in which the parameters do not change with respect to time is called as
Unsteady flow
Transient flow
Steady uniform flow
Continuous flow
Consider a flow over a flat plate of uniform cross section area, the flow moves at a constant speed. Due to a certain disturbance, there is a disturbance in the flow. In the given scenario, which of the following statement is true?
The flow remains uniform even after the disturbance
The flow remains uniform throughout
The flow is the first uniform and after disturbance undergoes non-uniformity
The disturbance will change the cross section area
The randomness of the molecules gives us ________ pressure.
Static
Dynamic
Absolute
Minimal gorund clearance
0,003m
0.3cm
30cm
0.03m
3cm
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