AREA: AERODYNAMICS/SUBSONIC

Example 1 | Twisted finite wing: lifting line analysis |

Example 2 | Bound circulation spanwise distribution and trailed vortex sheet strength |

Example 3 | Induced drag coefficient at a given section of a finite wing |

Example 4 | Glauert planform factor |

Example 5 | |

Example 6 | Absolute angle of attack, L/D and midspan circulation |

Example 7 | Vorticity, stream function, Euler equation and pressure coefficient |

Example 8 | Using the definition of vorticity to find velocity components |

Example 9 | Stagnation pressure and irrotationality |

Example 10 | Physical explanation of the terms in the integral conservation equations |

Example 11 | Terms corresponding to physical quantities |

Example 12 | |

Example 13 | Definitions: perfect fluid, streamline, superposition |

Example 14 | Circulation and vorticity |

Example 15 | Stream function physical definition |

Example 16 | Conditions for stream function to exist |

Example 17 | Bernoulli equation and pressure coefficient |

Example 18 | Elliptic and symmetric loadings of a finite wing |

Example 19 | Root section circulation and geometric angle of attack of a finite wing |

Example 20 | Does a velocity potential exist for this flow field? |

Example 21 | Does a stream function and/or a velocity potential exist for this flow? |

Example 22 | Finding circulation around a given path in a flowfield |

Example 23 | Pitot tube on an airplane |

Example 24 | Stagnation and static pressure in a wind tunnel test section |

Example 25 | Closed circuit wind tunnel |

Example 26 | Velocity components and flow speed ina potential flow |

Example 27 | Calculating streamlines around a cylinder in a potential flow |

Example 28 | Speed and pressure coefficient distribution around a cylinder in potential flow |

Example 29 | |

Example 30 |

** **