Jawaharlal Nehru Technological University Hyderabad
Jawaharlal Nehru Technological University Hyderabad B.Tech II AERODYNAMICS - I Previous Question Paper (August/September - 2022 - R18)
Answer any five questions. All questions carry equal marks.
Main
What are the properties of fluids? Explain any three with units.
Answer
Fluid properties are physical characteristics that define the state and behavior of a fluid. Three primary properties are:
- Density (ρ): Defined as the mass per unit volume of a fluid. It represents the degree of compactness of the fluid particles. The SI unit is kg/m3.
- Viscosity (μ): A measure of a fluid's resistance to gradual deformation by shear stress or tensile stress. It is essentially the internal friction of the fluid. The SI unit is N·s/m2 or Pa·s.
- Specific Weight (γ): Defined as the weight per unit volume of a fluid, calculated as the product of density and acceleration due to gravity (γ = ρg). The SI unit is N/m3.
Derive the equations for pressure coefficient and discuss the importance.
Answer
The pressure coefficient (Cp) is a dimensionless number used in aerodynamics and fluid mechanics to describe the relative pressures throughout a flow field. It is derived from Bernoulli's equation for incompressible, steady, irrotational flow:
Rearranging this to isolate the pressure difference gives:
Dividing both sides by the dynamic pressure (q∞ = 1/2ρV∞2) yields the definition of the pressure coefficient:
The importance of Cp includes:
- It allows for the comparison of pressure distributions over geometrically similar bodies regardless of the flow velocity or fluid density.
- It is essential for calculating the lift and drag forces on an airfoil by integrating the pressure distribution over the surface.
- It helps identify regions of high pressure (stagnation points where Cp = 1) and low pressure (suction peaks), which are critical for analyzing flow separation and aerodynamic performance.
Derive the energy equation for a viscous incompressible flow from the first principle and discuss its applications.
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What is Laplace equation? What is the condition for a flow to be incompressible and irrotational? Explain Magnus effect.
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Discuss on non-lifting flow over a cylinder with the resulting stream function and derive the corresponding equation.
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Explain the vortex panel method with an example and also explain its applicability.
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Explain the following terms related aerodynamics:
Circulation
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Biot- Savart’s law
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Rankine’s vortex.
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What is the effect of propeller on wings and tail unit? Explain them and discuss its impact on the performance.
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Show the conformal transformation of a circle to a symmetric airfoil by drawing the suitable diagram.
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