Predicted aerodynamic characteristics of a NACA 0015 airfoil having a 25% integral-type trailing edge flap
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Predicted aerodynamic characteristics of a NACA 0015 airfoil having a 25% integral-type trailing edge flap

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Published by National Aeronautics and Space Administration, Langley Research Center, National Technical Information Service, distributor in Hampton, Va, [Springfield, Va .
Written in English

Subjects:

  • Noise reduction.,
  • Airfoils.,
  • Blade-vortex interaction.,
  • Navier-Stokes equation.,
  • Trailing edge flaps.,
  • Aerodynamic characteristics.,
  • Grid generation (Mathematics),
  • Computational grids.

Book details:

Edition Notes

StatementAhmed Hassan.
Series[NASA contractor report] -- NASA/CR-1999-209328., NASA contractor report -- NASA CR-209328.
ContributionsLangley Research Center.
The Physical Object
FormatMicroform
Pagination1 v.
ID Numbers
Open LibraryOL15552423M

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