{alias:wedge}
\\
{panel}
{color:#ff0000}{*}Problem Specification{*}{color}\\
[1. Pre-Analysis & Start-up|FLUENT - Supersonic Flow Over a Wedge- Step 1]\\
[2. Geometry|FLUENT - Supersonic Flow Over a Wedge- Step 2]\\
[3. Mesh|FLUENT - Supersonic Flow Over a Wedge- Step 3]\\  [4. Setup (Physics)|SIMULATION:FLUENT - Supersonic Flow Over a Wedge - Step 4 *New]\\
[5. Solution|SIMULATION:FLUENT - Supersonic Flow Over a Wedge - Step 5 * New]\\
[6. Results|FLUENT - Supersonic Flow Over a Wedge- Step 6 *New]\\
[7. Verification & Validation|FLUENT - Supersonic Flow Over a Wedge- Step 7]
{panel}\\
\\
\\

h2. Problem Specification

!wedge2sm.jpg!

Consider a 15° angle wedge at zero angle of attack. The incoming flow conditions are: M{~}1~=3, p{~}1~=1 atm, T{~}1~=300 K. Use FLUENT to obtain the flowfield over the wedge. Compare the pressure coefficient on the wedge surface with the corresponding analytical result for an oblique shock.

Go to [Step 1: Pre-Analysis & Start-up|FLUENT - Supersonic Flow Over a Wedge- Step 1]

[See and rate the complete Learning Module|FLUENT - Supersonic Flow Over a Wedge]

Go to [all FLUENT Learning Modules|FLUENT Learning Modules]