Aeroengines - fluent problems, Other Engineering

We are interested in the supersonic flow of air through a convergent-divergent nozzle having a circular cross-sectional area, A, that varies with axial distance from the throat, x, according to the formula

A = C1 + x2;  -0.5 < x < 0.5

where A is in m2 and x is in m C1 is a constant which is different for each where A is in m and x is in m.  C1 is a constant which is different for each student. The stagnation pressure po at the inlet is given. The stagnation temperature To at the inlet is 300 K. The static pressure p at the exit is also given given. 

We will calculate the Mach number, pressure and temperature distribution in the FLUENT the nozzle using FLUENT and compare the solution to quasi-1D nozzle flow results. The Reynolds number for this high-speed flow is large. Use an inviscid flow model. 

2151_fluent problem.png

Posted Date: 8/27/2012 2:34:28 AM | Location : United States







Related Discussions:- Aeroengines - fluent problems, Assignment Help, Ask Question on Aeroengines - fluent problems, Get Answer, Expert's Help, Aeroengines - fluent problems Discussions

Write discussion on Aeroengines - fluent problems
Your posts are moderated
Related Questions
tell me about where we download notes for electronics syllabus

factors affecting engine performance

Engine lubrication systems There are basically two types of lubrication system at present in use in gas turbine engines:- a) Recirculatory. In this system, oil is distribut

In the Aircraft Performance course, the aircraft was assumed to be in a steady-state (e.g. steady  cruise, climb, turn, glide), with the forces and moments balanced. The subject of

Company: British Sky Broadcasting Topic: You are a security analyst in a large investment house and must write a report on a real stock of your choice, giving a buy, hold or sell r

Turbine Blade Clearance. Creep is term used to describe the continuous and permanent stretching of turbine blades due to high temperatures and centrifugal forces acting on the

When we solved our simple problem we saw that the truncation error was O(x) We therefore expect that as the number of grid points is was O(x). We therefore expect that as the numbe

(a)  A section of road has a free flow speed of 55km/h and a jam density of 367 vehicles per kilometre. Assuming under a linear speed-density relationship, calculate the density at

Using this link and the information therein ( http://www.sec.gov/Archives/edgar/data/1110452/000119312507151600/d20f.htm#tx19738_13.) find Air France’s weighted average cost of ca

FIRE PROTECTION SYSTEMS A complete fire warning system consists of a detection system, an extinguisher system and a method of detecting that the fire is out. There are specifi