hoppala, Other Engineering

Assignment Help:
Please help me to compare the minimum cell cost method and Vogel''s approximation method to find initial basic solution. Generally the sources indicated that the Vogel''s method gives more optimal results but other approach is used and also rarely gives more optimal solution compared to Vogel''s. But I didn''t define the advantages of the min cost method and reasons why industrial engineers are using them. Save me.

Related Discussions:- hoppala

Various cementing materials, The various cementing materials are classified...

The various cementing materials are classified as follows. a) Argillaceous cementing materials b) Calcareous cementing materials c) Carbonaceous cementing materials Argillaceous Ma

Cro, derive the expression of deflection of beam in CRO

derive the expression of deflection of beam in CRO

Mr tiy, Hi, do u help with HYSYS assignment ?

Hi, do u help with HYSYS assignment ?

Software engineering, what is differnce between need and requirement?

what is differnce between need and requirement?

Dsp-bilinear transformation, Convert the analog filter the system function...

Convert the analog filter the system function Ha(s)=(s+0.1)/((s+0.1)(s+0.1)+16) with digital iir filter by bilinear transformation .the digital filter is to have the resonent freq

Material science and engineeing, cite advantages of forming metal by extrus...

cite advantages of forming metal by extrusion as opposed to rolling

Constant speeding propeller, Constant speeding propeller: The definitio...

Constant speeding propeller: The definition of a Constant Speeding propeller is 'A propeller, the pitch setting of which varies automatically to maintain a preselected constant

#Corporate Finance Homework, #As an investment advisor you have been approa...

#As an investment advisor you have been approached by a client called Ramesh, who wants some help in investment related matters. Ramesh is currently 45 years old and has Rs 6, 00,

Aircraft controls, The aerodynamic flight controls of a typical aeroplane ...

The aerodynamic flight controls of a typical aeroplane include ailerons (British: ξ ("Xi"); US: da or δa), elevator (British: η ("eta"); US de or δe), and rudder (British: ζ ("zeta

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