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Write a matlab code for streamline flow around a cylinder.
Write a matlab code to plot streamline flow around a cylinder.
Matlab

Worldtech Asked on 6th November 2019 in Aerodynamics.
- 1K views
- 1 answers
- 0 votes
Write a matlab solution to Rankine nose problem.
Write a matlab solution to Rankine nose problem.
Matlab

techAir Asked on 5th November 2019 in Aerodynamics.
- 1K views
- 1 answers
- 0 votes
A typical World War I biplane fighter (such as the French SPAD shown in Figure 3.50) has a number of vertical interwing struts and diagonal bracing wires. Assume for a given airplane that the total length for the vertical struts (summed together) is 25ft, and that the struts are cylindrical with a diameter of 2 in. Calculate the drag (in pounds) contributed by the struts and bracing wires when the airplane is flying at \(120 \;mi/h\) at standard sea level.
Assume for a given airplane that the total length for the vertical struts (summed together) is \(25\; ft\), and that …
incompressible flow

Worldtech Asked on 5th November 2019 in Aerodynamics.
- 1K views
- 1 answers
- 0 votes
The lift on a spinning circular cylinder in a freestream with a velocity of \(30 \;m/s\) and at standard sea level conditions is \(6\; N/m\) of span. Calculate the circulation around the cylinder.
The lift on a spinning circular cylinder in a freestream with a velocity of \(30 \;m/s\) and at standard sea …
incompressible flow

techAir Asked on 5th November 2019 in Aerodynamics.
- 2K views
- 1 answers
- 0 votes
Consider the lifting flow over a circular cylinder of a given radius and with a given circulation. If \(V_{\infty}\) is doubled, keeping the circulation the same, does the shape of the streamlines change? Explain.
Consider the lifting flow over a circular cylinder of a given radius and with a given circulation. If \(V_{\infty}\) is …
incompressible flow

techAir Asked on 4th November 2019 in Aerodynamics.
- 2K views
- 1 answers
- 0 votes
Consider the nonlifting flow over a circular cylinder of a given radius, where \(V_{\infty} = 20\; ft/s\). If \(V_{\infty}\) is doubled, that is, \(V_{\infty} = 40 ft/s\), does the shape of the streamlines change? Explain.
Consider the nonlifting flow over a circular cylinder of a given radius, where \(V_{\infty} = 20 ft/s\). If \(V_{\infty}\) is …
incompressible flow

Worldtech Asked on 4th November 2019 in Aerodynamics.
- 4K views
- 1 answers
- 0 votes
Consider the nonlifting flow over a circular cylinder. Derive an expression for the pressure coefficient at an arbitrary point \((r, θ)\) in this flow, and show that it reduces to Equation \(Cp = 1 − 4 sin^{2} θ\) on the surface of the cylinder.
Consider the nonlifting flow over a circular cylinder. Derive an expression for the pressure coefficient at an arbitrary point \((r, …
incompressible flow

techAir Asked on 4th November 2019 in Aerodynamics.
- 4K views
- 1 answers
- 0 votes
Derive the velocity potential for a doublet.
Derive the velocity potential for a doublet.
incompressible flow

Worldtech Asked on 4th November 2019 in Aerodynamics.
- 3K views
- 1 answers
- 0 votes
Prove that the velocity potential and the stream function for a source flow, satisfy Laplace’s equation.
Prove that the velocity potential and the stream function for a source flow, satisfy Laplace’s equation.
incompressible flow

techAir Asked on 3rd November 2019 in Aerodynamics.
- 2K views
- 1 answers
- 0 votes
Prove that the velocity potential and the stream function for a uniform flow , satisfy Laplace’s equation.
Prove that the velocity potential and the stream function for a uniform flow , satisfy Laplace’s equation.
incompressible flow

Worldtech Asked on 3rd November 2019 in Aerodynamics.
- 2K views
- 1 answers
- 0 votes

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