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Author: Rajesh Bhaskaran, Cornell

University

Problem Specification
1. Create Geometry in GAMBIT
2. Mesh Geometry in GAMBIT
3. Specify Boundary Types in GAMBIT
4. Set Up Problem in FLUENT
5. Solve!
6. Analyze Results
7. Verify Results

Problem Specification

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Consider a 15° angle wedge at zero angle of attack. The incoming flow conditions are: M₁=3, p₁=1 atm, T₁=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.

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{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]

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

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

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Problem Specification