## Tarashankar Sharma

Title:
User
Status:
Trusted

Email:
t***********************@gmail.com
Location:
Mumbai
Twitter:
@TarashankarRS

Last seen:
1 month, 2 weeks ago
Joined:
8 months, 2 weeks ago

Hello,

I am Civil Engineer from Mumbai University and has a total of 2 years of experience in site engineering and valuation of immovable property.

Currently pursuing my Mtech from VJTI college in Project Management.

I am inter-college level chess champion.

Like to travel and explore new places.

Currently living in Mumbai with family.

Thanks for visiting my profile

#### Posts by Tarashankar Sharma

<prev • 262 results • page 2 of 27 • next >
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... **Sub sonic flow**: A flow is said sub sonic flow if Mach number is less than 1 i.e velocity of flow (V) is less than the velocity of the sound wave (C). **Sonic flow**: A flow is said sonic flow if Mach number is equal to 1 i.e velocity of flow is equal to the velocity of the sound wave. **Super ...
written 7 weeks ago by Tarashankar Sharma0
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... (5 Marks) Dec-2018 Subject **Fluid Mechanics 2** Topic **Compressible Flow** Difficulty **Medium** ...
written 7 weeks ago by Tarashankar Sharma0
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... An Aero-plane travels in air of pressure of 1 bar at 10 degree celsuis at a speed of 1800 km/hr. Find the Mach number and Mach angle. Take k=1.4 and R=287 J/Kg K. **(8 Marks)** Subject **Fluid Mechanics 2** Topic **Compressible Flow** Difficulty **Medium** ...
written 7 weeks ago by Tarashankar Sharma0 • updated 5 weeks ago by Yashbeer ♦♦ 150
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... **Mach number** defined as the square root of the ratio of the inertia force of a flowing fluid to the elastic force. $\therefore \text{Mach Number} = M = \sqrt \frac{ \text{Inertia force} }{ \text{Elastic force} } = \sqrt \frac{\rho AV^2}{KA}$ \$M = \sqrt \frac {V^2}{K/ \rho } = \frac{V} {\sqrt {k ...
written 7 weeks ago by Tarashankar Sharma0 • updated 6 weeks ago by Yashbeer ♦♦ 150
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... (5 Marks) Dec-2018 Subject **Fluid Mechanics 2** Topic **Compressible Flow** Difficulty **Medium** ...
written 7 weeks ago by Tarashankar Sharma0 • updated 6 weeks ago by Renu Banswani10
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... - The series of wave fronts form a disturbance envelope given by a straight line which is tangent to the family of circles. It will be seen that all the disturbance waves lie within a cone (shown in fig.) having a vertex/apex at the body at time considered. The locus of all the leading surfaces of t ...
written 7 weeks ago by Tarashankar Sharma0
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... Define Mach Cone, Mach Angle, Zone of Action and Zone of Silence. (5 Marks) May-2018 Subject **Fluid Mechanics 2** Topic **Compressible Flow** Difficulty **Medium** ...
written 7 weeks ago by Tarashankar Sharma0
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... ![1 of 1][1] [1]: https://i.imgur.com/gJnMm4T.jpg ...
written 7 weeks ago by Tarashankar Sharma0
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... A nozzle is fitted to a pipe 120mm in diameter and 250m long, with coefficient of friction as 0.01. If the available head at the nozzle is 100m. Find the diameter of the nozzle and the maximum power transmitted by a jet of water discharging freely out of a nozzle. (10 Marks) Dec-2018 Subject **Fl ...
written 8 weeks ago by Tarashankar Sharma0
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... Calculate the discharge in each pipe of the network shown in fig below by Hardy Cross method. Take n=2. Subject **Fluid Mechanics 2** Topic **Pipe Network and water hammer** Difficulty Medium ...
written 8 weeks ago by Tarashankar Sharma0

#### Latest awards to Tarashankar Sharma

Autobiographer 7 months ago, has more than 80 characters in the information field of the user's profile.
Centurion 7 months ago, created 100 posts.
Rising Star 7 months ago, created 50 posts within first three months of joining.