IT KING

Not Rated (0)

$25/per page/Negotiable

About IT KING

Levels Tought:
Elementary,Middle School,High School,College,University,PHD

Expertise:
Computer Science,Engineering See all
Computer Science,Engineering,Environmental science,Essay writing,Information Systems,Programming Hide all
Teaching Since: Apr 2017
Last Sign in: 453 Weeks Ago, 3 Days Ago
Questions Answered: 402
Tutorials Posted: 401

Education

  • MSC,MBA(IT)
    Standford
    Jun-1997 - Sep-2000

Experience

  • IT Manager
    Honeywell
    Aug-2001 - Present

Category > Applied Sciences Posted 06 May 2017 My Price 8.00

A single-stage axial flow

A single-stage axial flow turbine is to be designed for zero reaction without any
absolute swirl at rotor exit. At nozzle inlet the stagnation pressure and temperature of the gas are
424kPa and 1100K. The static pressure at the mean radius between the nozzle row and rotor
entry is 217 kPa and the nozzle exit flow angle is 70°.
Sketch an appropriate Mollier diagram (or a T - s diagram) for this stage allowing for the
effects of losses and sketch the corresponding velocity diagram. Hence, using Soderberg’s correlation
to calculate blade row losses, determine for the mean radius,
(i) the nozzle exit velocity,
(ii) the blade speed,
(iii) the total-to-static efficiency.

Answers

IT KING
Not Rated (0)
Status NEW Posted 06 May 2017 10:05 AM My Price 8.00

Hel-----------lo -----------Sir-----------/Ma-----------dam----------- T-----------han-----------k Y-----------ou -----------for----------- us-----------ing----------- ou-----------r w-----------ebs-----------ite----------- an-----------d a-----------cqu-----------isi-----------tio-----------n o-----------f m-----------y p-----------ost-----------ed -----------sol-----------uti-----------on.----------- Pl-----------eas-----------e p-----------ing----------- me----------- on----------- ch-----------at -----------I a-----------m o-----------nli-----------ne -----------or -----------inb-----------ox -----------me -----------a m-----------ess-----------age----------- I -----------wil-----------l

Not Rated(0)