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
2. Differentiate between stream oriented and data gram oriented socket in java?

what is the basic operation of gas turbine engine?

tubular joint root fatigue criteria and creteria about tubular joint fatigue for inersid weld toe welded from both side

Consider 1:1 stoichiometric polymerisation of 1,4-diaminobutane with sebacoyl chloride. (a) Write down a balanced chemical equation for the polymerization (b) Name the polymer fo


Integrated circuits: Integrated circuits, or IC's, have changed the entire electronics industry. Before IC's were developed, all electronic circuits consisted of individual (d

PROPELLER BALANCE There are two types of balance of importance when working with propellers: • Static Balance • Dynamic Balance Static balance is checked and corrected

I have a 30'' simple span beam, braced at the supports only. Uniform load is 1200 plf. I need deflection limited to L/400. What size steel beam do I need?


represent the numbers 387 and 25 as floating numbers and illustrate the calculation of 387+25 using rounding.What is the calculated sum.