AREA: AERODYNAMICS/COMPREHENSIVE

Example 1 | Pressure gradient and rotation |

Example 2 | Two parallel streams mixing |

Example 3 | Terms in the integral conservation equations: physical meaning |

Example 4 | Air jets impinging on plate and cascade of vanes |

Example 5 | Flow through a pipe tee and elbow: continuity and momentum equations applied |

Example 6 | Turboprop engine: change in stagnation enthalpy by 1-D energy equation |

Example 7 | Substantial derivative |

Example 8 | Airfoil drag coefficient from wake momentum deficit |

Example 9 | Reaction force due to flow turning |

Example 10 | Pressure force on the nose of a body in a flow |

Example 11 | Acceleration terms through a quasi 1-D contraction |

Example 12 | Reaction force on a jet engine test stand |

Example 13 | Horizontal axis wind turbine quasi 1-D flow and forces |

Example 14 | Turbine horsepower |

Example 15 | Airplane Pitot and static pressures: Bernoulli equation |

Example 16 | Wind tunnel stagnation and static pressures: Bernoulli equation |

Example 17 | Closed circuit wind tunnel |

Example 18 | Static enthalpy of different gases |

Example 19 | Speed of sound in helium vs. air |

Example 20 | Isentropic relations connecting stagnation and static properties in a wind tunnel |

Example 21 | Experimental determination of the speed of sound in air |

Example 22 | Mach number and Mach angle |

Example 23 | Stagnation and static temperature in supersonic flight |

Example 24 | Pressure coefficient on an airplane wing |

Example 25 | Error in pressure calculation if compressibility were neglected |

Example 26 | Highest speed achieved when air blows out of a reservoir |

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