Aeroengines - comparison with analytical solution, Other Engineering

Assignment Help:

The figure below compares the discrete solution with the exact analytical solution The error is largest at the right boundary where it is equal to solution. The error is largest at the right boundary where it is equal to approximately 15% : In a real CFD solution the number of unknowns is typically thousands to millions. A lot of work goes into solving these matrices efficiency matrices efficiency. Usually an iterative procedure is d used. 

1161_comparsion with analytical process.png


Related Discussions:- Aeroengines - comparison with analytical solution

Zero-coupon bond, Zero-Coupon Bond is a type of bond gives no periodic inte...

Zero-Coupon Bond is a type of bond gives no periodic interest payments, instead is sold at a steep discount from its face value. Due to these bonds these do not pay interest until

Final project, can u give idea about project in agriculture

can u give idea about project in agriculture

Biomechanics, i have homework in my biomechanics class

i have homework in my biomechanics class

Oil pumps, what is the function and location of the components?

what is the function and location of the components?

Phase detector, Phase detector Phase detector (PD) consists of a multip...

Phase detector Phase detector (PD) consists of a multiplier and a low pass filter. The output of the PD has a magnitude proportional to V s cos 2 φ  where φ is the phase shif

Case study, M/s XYZ Ltd manufactures a product “PLVS” at its plant at Meeru...

M/s XYZ Ltd manufactures a product “PLVS” at its plant at Meerut, the maximum capacity of which is 200 units per month. Details of raw materials which go into the making of 1 units

Aviation legislation design and type certificate, Design, Construction and ...

Design, Construction and Type Certificate The following chapter covers the initial design, construction, registration and test flying of the first prototype of a new aircraft.

Ideal intake conditions - aircraft engine, Ideal intake conditions: For...

Ideal intake conditions: For air to flow smoothly through a compressor, its velocity should be about 0.5 mach at the compressor inlet; this includes aircraft flying faster than

Write Your Message!

Captcha
Free Assignment Quote

Assured A++ Grade

Get guaranteed satisfaction & time on delivery in every assignment order you paid with us! We ensure premium quality solution document along with free turntin report!

All rights reserved! Copyrights ©2019-2020 ExpertsMind IT Educational Pvt Ltd