AREA: AERODYNAMICS/SUBSONIC

Example 1 | Transformation to Laplace equation |

Example 2 | Shape and tangency boundary condition |

Example 3 | Derive relation cl=cl0/Beta |

Example 4 | Lift curve slope vs. Mach number |

Example 5 | Cp and static pressure at high subsonic Mach number |

Example 6 | Airfoil thickness and pressure coefficient vs Mach number |

Example 7 | Linearized potential equation error (this is supersonic!) |

Example 8 | Calculating stagnation pressure |

Example 9 | Velocity component at a point on a surface |

Example 10 | Variation of Cp with Mach number |

Example 11 | Wing parameter transformation with Mach number |

Example 12 | Ellipsoid of revolution |

Example 13 | Wing lift curve slope change with Mach number |

Example 14 | Wing lift curve slope change with Mach number |

Example 15 | Delta wing sweep for corresponding wings |

Example 16 | Slender body theory derivation |

Example 17 | |

Example 18 | |

Example 19 |

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