{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]\\ [5. Solution|SIMULATION:FLUENT - Supersonic Flow Over a Wedge - Step 5 * New]\\ [6. Results|FLUENT - Supersonic Flow Over a Wedge- Step 6]\\ [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: Create Geometry in GAMBIT|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] |