Summary
Summary COMPRESSIBLE FLUID FLOW - OBLIQUE SHOCK AND EXPANSION WAVES
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Uploaded on
11-08-2023
Written in
2023/2024
This report elaborates on some applications of oblique shocks and expansion wave relations (shock expansion theory) to calculate the drag force on a diamond airfoil at different angles of attack and solve for the flow deflection angle at the tail of an infinitely thin plate. The report also shows a plot of flow deflection angle against shock angle using different supersonic Mach numbers. With the correct prediction of the shock patterns around a body, one can use these shock patterns to calculate for the flow properties such as static and total pressures at different sections of the body, and the first two examples employ a MATLAB code to demonstrate this ability. Lastly, the
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Written for
- Institution
- North Carolina A&T State University
- Module
- MEEN 668 - COMPRESSIBLE FLOW (MEEN668)
All documents for this subject (4)
Document information
- Uploaded on
- August 11, 2023
- Number of pages
- 33
- Written in
- 2023/2024
- Type
- Summary
Subjects
-
compressible flows
-
oblique shock
-
expansion waves
-
prandtl meyer
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COMPRESSIBLE FLOW - NOTES, EXAMPLES AND CODES
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