Maurice Tutor

(5)

$15/per page/Negotiable

About Maurice Tutor

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

Expertise:
Algebra,Applied Sciences See all
Algebra,Applied Sciences,Biology,Calculus,Chemistry,Economics,English,Essay writing,Geography,Geology,Health & Medical,Physics,Science Hide all
Teaching Since: May 2017
Last Sign in: 408 Weeks Ago
Questions Answered: 66690
Tutorials Posted: 66688

Education

  • MCS,PHD
    Argosy University/ Phoniex University/
    Nov-2005 - Oct-2011

Experience

  • Professor
    Phoniex University
    Oct-2001 - Nov-2016

Category > Management Posted 09 Jan 2018 My Price 5.00

small aircraft

A ram-jet engine is fitted to a small aircraft that cruises at Mach 4 at an altitude where the pressure is 30 kPa and the temperature is –45°C. The air entering the engine is slowed to subsonic velocities by passing it through two oblique shock waves each of which turn the flow through 15° and by then passing it through a normal shock wave. Following the normal shock, the flow is isentropically decelerated to Mach 0.1 before it enters the combustion zone. Find the values of the pressure and the temperature at the inlet to the combustion zone. What values would have been attained if initial deceleration had been through a single normal shock wave instead of through the combination of oblique shocks and a normal shock?

 

Answers

Maurice Tutor
(5)
Status NEW Posted 09 Jan 2018 02:01 PM My Price 5.00

Hel-----------lo -----------Sir-----------/Ma-----------dam-----------Tha-----------nk -----------You----------- fo-----------r u-----------sin-----------g o-----------ur -----------web-----------sit-----------e a-----------nd -----------acq-----------uis-----------iti-----------on -----------of -----------my -----------pos-----------ted----------- so-----------lut-----------ion-----------.Pl-----------eas-----------e p-----------ing----------- me----------- on-----------cha-----------t I----------- am----------- on-----------lin-----------e o-----------r i-----------nbo-----------x m-----------e a----------- me-----------ssa-----------ge -----------I w-----------ill----------- be-----------

Not Rated(0)
Relevent Questions