A Viscous/potential Flow Interaction Analysis Method for Multi-element Infinite Swept Wings, Volume 11974 - 91 pages |
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Contents
LIST OF SYMBOLS | 8 |
BOUNDARY LAYER CALCULATION METHODS | 22 |
Boundary Layer Transition | 30 |
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Common terms and phrases
1+ky boundary condition boundary layer calculation boundary layer development boundary layer method calculated pressure calculation procedure COMPARISON OF MEASURED cross flow Cumpsty and Head determined difference boundary layer dimensional displacement thickness double slotted flap eddy viscosity effects equations factor H finite difference boundary finite difference method flap surface flap upper surface geometry H₁ incompressible flow infinite swept wing initial iteration Kutta condition laminar boundary layer laminar flow leading edge leading edge slot lift coefficient Lockheed program lower surfaces matrix multiplication MEASURED AND PREDICTED NACA 23012 AIRFOIL NASA normal chord normal velocity OVERLAY panel parameter pitching moment potential core PREDICTED PRESSURE DISTRIBUTIONS pressure coefficients pressure gradient Reynolds number shape factor shear stress shown in Figure skin friction coefficient slat source distribution source strength spanwise stagnation line three-dimensional trailing edge transition turbulent boundary layer velocity profiles viscous/potential flow interaction vortex distribution vortices X/C FIG ӘР ди ду