Kisan Kumar, Author at Aerospace answers

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Kisan Kumar
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233
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68

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24

How to do Isro chandrayaan 3 launch registration?
How to do Isro chandrayaan 3 launch registration , ISRO launch registration, ISRO launch slot registration, ISRO mission registration?
Kisan Kumar Asked on 21st June 2023 in Others.
- 626 views
- 1 answers
- 0 votes
Why is critical Mach number of a sphere higher than a cylinder?
Why is critical Mach number of a sphere higher than a cylinder?
Airplane design

airspeed

Mach number

Kisan Kumar Asked on 13th January 2022 in Aerodynamics.
- 958 views
- 1 answers
- 0 votes
What is AWACS?
What is AWACS?
aircraft instrument

Airplane design

Kisan Kumar Asked on 13th December 2021 in Technology.
- 943 views
- 1 answers
- 0 votes
What is a Jet lag?
What is a Jet lag?
earth

Kisan Kumar Asked on 8th September 2021 in Others.
- 1K views
- 1 answers
- 0 votes
A circular cylinder and a sphere are in a free stream flow with their axis perpendicular to the flow. At the top of the sphere there is a pressure tap which is connected by a tube to one side of a manometer. There is a pressure tap on the surface of the cylinder which is connected to the other side of the manometer. Find the location of this tap on cylindrical surface such that there is no deflection of fluid in the manometer.
A circular cylinder and a sphere are in a free stream flow with their axis perpendicular to the flow. At …
fluids

incompressible flow

Kisan Kumar Asked on 1st September 2021 in Aerodynamics.
- 1K views
- 1 answers
- 0 votes
A NACA 4421 airfoil having a chord length of \(2\,m\) is flying at an velocity of \(70\,m/s\) at an altitude of \(2\,km\). Find the lift per unit span and the circulation at an angle of attack of \(4^{\circ}\), for this airfoil.
A NACA 4421 airfoil having a chord length of \(2\,m\) is flying at an velocity of \(70\,m/s\) at an altitude …
airfoil

airspeed

Circulation

lift coefficient

Kisan Kumar Asked on 22nd July 2021 in Aerodynamics.
- 1K views
- 1 answers
- 0 votes
Can an airfoil fly upside-down ?
A positively cambered airfoil has a zero-lift angle of \(-3.5^{\circ}\). The lift slope for this airfoil is \(0.12\) per degree. …
airfoil

lift

lift and drag

lift coefficient

lift force

Kisan Kumar Asked on 13th July 2021 in Aerodynamics.
- 2K views
- 1 answers
- 0 votes
Find the velocity of air in the test section of a low speed open circuit subsonic wind tunnel which has an inlet -to-throat area ratio of \(10\). The U-tube mercury manometer read as a height difference of \(10.5\,cm\) for the pressure difference between the inlet and the test section of the wind tunnel.
Find the velocity of air in the test section of a low speed open circuit subsonic wind tunnel which has …
airspeed

incompressible flow

Kisan Kumar Asked on 15th June 2021 in Aeronautics.
- 1K views
- 1 answers
- 0 votes
Find the acceleration of a fluid particle in the \(x\) direction at \((x,y) = (3,1)\) for a velocity field, which is given by\(\vec{V} = 3y\hat{i}+4x\hat{j}\). \(x\) and \(y\) are in meters.
Find the acceleration of a fluid particle in the \(x\) direction at \((x,y) = (3,1)\) for a velocity field, which …
fluids

Kisan Kumar Asked on 5th May 2021 in Fluid mechanics.
- 1K views
- 1 answers
- 0 votes
A velocity field is given by \(u=\frac{y}{x^{3}+y}\) and \(v=\frac{-x}{x^{3}+y}\). Find the equation of the streamline which is passing through the point \(\left ( 2,6 \right )\).
A velocity field is given by \(u=\frac{y}{x^{3}+y}\) and \(v=\frac{-x}{x^{3}+y}\). Find the equation of the streamline which is passing through the …
streamlines

Kisan Kumar Asked on 15th April 2021 in Fluid dynamics.
- 1K views
- 1 answers
- 0 votes

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