Chapter 6: Oblique Shock Waves

This chapter contains 23 unsolved problems.

# | Short Problem Description | Manual solution Inactive links |
Computer solution Inactive links |
---|---|---|---|

1 | Properties behind oblique shock wave |
q01.pdf | q01.py |

2 | Stagnation pressure ratio |
q02.pdf | q02.py |

3 | Wedge at an angle of attack |
q03.pdf | q03.py |

4 | Mach line and wall turn angle |
q04.pdf | q04.py |

5 | Turning angle of corner |
q05.pdf | q05.py |

6 | Flow pattern and attached shock limit |
q06.pdf | q06.py |

7 | Largest wall corner angle |
q07.pdf | q07.py |

8 | Minimum Mach number limit |
q08.pdf | q08.py |

9 | Optical method for Mach number calculation |
q09.pdf | q09.py |

10 | 2D Shock reflection |
q10.pdf | q10.py |

11 | Properties behind reflected shock |
q11.pdf | q11.py |

12 | Mach reflection range |
q12.pdf | q12.py |

13 | Two Oblique shock reflections |
q13.pdf | q13.py |

14 | Pressure after reflection |
q14.pdf | q14.py |

15 | Shock reflection with deflected wall |
q15.pdf | q15.py |

16 | Shock reflection with deflected wall |
q16.pdf | q16.py |

17 | Shock-shock intersection |
q17.pdf | q17.py |

18 | Pressure calculation (Shock intersection) |
q18.pdf | q18.py |

19 | Pressure calculation (Shock intersection) |
q19.pdf | q19.py |

20 | Flow pattern after shock intersection |
q20.pdf | q20.py |

21 | Turbo jet engine - normal vs oblique shock |
q21.pdf | q21.py |

22 | Ram-jet engine calculation with shocks |
q22.pdf | q22.py |

23 | Oblique shocks for flow Mach estimation |
q23.pdf | q23.py |

For further details, please contact me at:

mail.spbhat@gmail.com

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If you observe any error or want to provide me with feedback, please don't hesitate to contact me.

Thanks,

Sourabh Bhat

Thanks,

Sourabh Bhat