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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]
[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]
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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]

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