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Worldtech
Considering a non-lifting flow over a circular cylinder derive an expression for the pressure coefficient.
on 29th December 2018 in
Aerodynamics.
1K
1
0
Worldtech
Calculate locations on the surface of a cylinder where surface pressure equals to free-stream pressure considering a non-lifting flow.
on 29th December 2018 in
Aerodynamics.
1K
1
0
techAir
Find the circulation around spinning cylinder.
on 28th December 2018 in
Aerodynamics.
1K
1
0
Worldtech
In an inviscid, incompressible flow of air along a streamline, the air density is 0.002377 slug/ft^3. Find the pressure at a point.
incompressible flow
on 28th December 2018 in
Fluid dynamics.
2K
1
0
Worldtech
Consider an airfoil in a flow at standard sea level conditions with a free stream velocity of 70 m/s.
incompressible flow
on 28th December 2018 in
Aerodynamics.
2K
1
0
Worldtech
The temperature and pressure at the stagnation point of a high speed missile are 934 R and 7.8 atm. Calculate the density at this point.
on 26th December 2018 in
Aeronautics.
2K
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