This set of Aerodynamics Multiple Choice Questions & Answers (MCQs) focuses on “Vortex Flow”.
1. The free vortex flow forms _________
a) straight lines
b) concentric circles
c) parabola
d) hyperbola
View Answer
Explanation: The free vortex flow is a circulatory flow of the fluid such that its stream lines are concentric circles. The velocity components for a free vortex flow are Ur and Uθ and is equal to Ur=0 and Uθ=circulation/ 2*pi*r.
2. The following figure is an example of ____________
a) source flow
b) sink flow
c) doublet
d) free vortex flow
View Answer
Explanation: The above figure shows the concentric circles along with streamlines. Here, the stream function is a function of radius and it is constant value and hence the streamlines are concentric.
3. Except at the origin where r=0, the vortex flow is ___________
a) rotational
b) laminar
c) irrotational
d) turbulent
View Answer
Explanation: Vortex flow is irrotational everywhere except at the point r=0, where the vorticity is infinite. Therefore, the origin, r=0, is a singular point in the flow field. Here, the origin point represents the singularity point.
4. The strength of the vortex flow can be given by ______________
a) Γ=2*pi*C
b) Γ=2*pi
c) Γ=-2*pi*C
d) Γ=0
View Answer
Explanation: The circulation for vortex flow can be given by –
Γ=2*pi*C where, C – constant and Γ is the strength of the vortex flow.
When Γ is positive, it means that vortex of positive strength rotates in the clockwise direction and vice versa.
5. The combination of uniform flow and source flow gives ___________
a) flow past a cylinder
b) flow past a half body
c) flow past a full body
d) flow past a wedge
View Answer
Explanation: When a uniform of velocity U combines with a source flow of strength q, the resultant flow is a flow over a half body.
6. The circles with their centre on the X axis _____________
a) eccentric circles
b) concentric circles
c) potential lines
d) equal circles
View Answer
Explanation: Potential lines are eccentric non-intersecting circles with their centres on x-axis. The potential lines for source pair will be eccentric non-intersecting circles.
7. Centre of pressure can be calculated using __________
a) Principle of moments
b) Principle of energy
c) Mass conservation
d) Rayleigh’s principle
View Answer
Explanation: The centre of pressure can be calculated using a principle of moments which states that the moment of the resultant force about an axis is equal to the sum of moments of the components about the same axis.
8. A body floats on the surface when ____________
a) metacenter is above gravity
b) metacenter is below gravity
c) metacenter is equal to gravity
d) gravity is above metacenter
View Answer
Explanation: In case of a floating object, the metacenter should always be above gravity. Metacentre is the point about which a body starts oscillating when the body is tilted by a small angle. In the case of a floating body, the weight of an object is equal to the amount of fluid displaced.
Sanfoundry Global Education & Learning Series – Aerodynamics.
To practice all areas of Aerodynamics, here is complete set of 1000+ Multiple Choice Questions and Answers.
If you find a mistake in question / option / answer, kindly take a screenshot and email to [email protected]
- Practice Aerospace Engineering MCQs
- Check Aerodynamics Books
- Apply for Aerospace Engineering Internship
- Check Aerospace Engineering Books
- Check Aeronautical Engineering Books
