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Author: Rajesh Bhaskaran, Cornell University

{color:#ff0000}{*}Problem Specification{*}{color}
[1. Create Geometry in GAMBIT[Problem Specification|FLUENT - Supersonic Flow Over a Wedge - StepProblem 1Specification]\\
[21. MeshPre-Analysis Geometry in GAMBIT& Start-up|FLUENT - Supersonic Flow Over a Wedge- Step 21]\\
[32. Specify Boundary Types in GAMBITGeometry|FLUENT - Supersonic Flow Over a Wedge- Step 32]\\
[43. Set Up Problem in FLUENT|SIMULATION:Mesh|FLUENT - Supersonic Flow Over a Wedge - Step 3]\\  {color:#ff0000}{*}4. *New]Setup(Physics)*{color}\\
[5. Solve\!Solution|SIMULATION:FLUENT - Supersonic Flow Over a Wedge - Step 5 (FLUENT 6.3.26)]* New]\\
[6. Analyze Results|FLUENT - Supersonic Flow Over a Wedge- Step 6]\\
[7. VerifyVerification & ResultsValidation|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]

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

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