{alias:wedge} {panel} Author: Rajesh Bhaskaran, Cornell University {color:#ff0000}{*}Problem Specification{*}{color} [1. Create Geometry in GAMBIT|FLUENT - Supersonic Flow Over a Wedge- Step 1] [2. Mesh Geometry in GAMBIT|FLUENT - Supersonic Flow Over a Wedge- Step 2] [3. Specify Boundary Types in GAMBIT|FLUENT - Supersonic Flow Over a Wedge- Step 3] [4. Set Up Problem in FLUENT|FLUENT - Supersonic Flow Over a Wedge- Step 4 (FLUENT 6.3.26)] [5. Solve\!|FLUENT - Supersonic Flow Over a Wedge- Step 5] [6. Analyze Results|FLUENT - Supersonic Flow Over a Wedge- Step 6] [7. Verify Results|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] |