## Aerodynamic influence coefficient method using singularity splines, Volume 2423 |

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### Contents

SUMMARY | 1 |

I REQUIREMENTS FOR NUMERICAL SCHEME | 8 |

Figures Pa cje 1 Edge Conditions for Supersonic Plantoros | 11 |

21 other sections not shown

### Common terms and phrases

Aerodynamic Influence Coefficient analysis angle of attack antisymmetric bound vorticity boundary conditions chord chordwise computed configurations constant pressure panel coordinate cylinder differential equation discontinuities doublet downstream downwash singularities Eguation elementary horseshoe vortex Equation 25 evaluated expression formulation free stream Gaussian quadrature geometric paneling interference shell intersection kernel function Kutta condition least square error left edge lifting surface schemes logarithmic singularity Mach line paneling Mean Square Downwash method nondimensional number of control numerical scheme numerical stability order problem parameter perturbation velocity planar planform breaks potential flow pressure distribution pressure panel scheme QUADRATIC ADDITION region requirement rms error root chord root function Root Mean Square segment shows sideslip special Mach lines spline function Square Downwash Error stability derivatives strength subdivisions subsonic and supersonic subsonic flow supersonic flow symmetric technique tip function trailing edge value and slope velocity kernel vortex spline vortex spline scheme vorticity distribution xLE(n