A Viscous/potential Flow Interaction Analysis Method for Multi-element Infinite Swept Wings, Volume 1

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1974 - 91 pages

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Contents

LIST OF SYMBOLS
8
BOUNDARY LAYER CALCULATION METHODS
22
Boundary Layer Transition
30

5 other sections not shown

Common terms and phrases

1+ky aerodynamic agreement airfoil analysis angle approach boundary layer calculation boundary layer development calculation chord Comparison COMPARISON OF MEASURED component configuration considerable convergence coordinate cross flow Cumpsty and Head curvature described determined dimensional direction drag eddy viscosity effects element equations exact experiment field Figure flap upper surface function geometry give given infinite swept wing influence coefficient initial integral inviscid iteration known lift lower surfaces matrix MEASURED AND PREDICTED method momentum thickness multi-element normal normal velocity obtained OVERLAY panel parameter potential flow predicted present pressure distribution pressure gradient problem procedure region represent Reynolds number separation shape factor shown in Figure skin friction coefficient slat slotted flaps solution source distribution streamline streamwise three-dimensional trailing edge transition turbulent boundary layer velocity profiles vortex distribution vortex strengths ди

Bibliographic information

TitleA Viscous/potential Flow Interaction Analysis Method for Multi-element Infinite Swept Wings, Volume 1
ContributorF. A. Dvorak
Published1974
Original fromNational Aeronautics and Space Administration (NASA)
DigitizedMay 20, 2010
Length91 pages
  
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