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

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

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Bibliographic Details
Main Author: Hassan, Ahmed
Corporate Author: Langley Research Center
Format: Government Document Book
Language:English
Published: Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], [1999]
Series:NASA contractor report ; NASA CR-209328.
Subjects:
Noise reduction.
Airfoils.
Blade-vortex interaction.
Navier-Stokes equation.
Trailing edge flaps.
Aerodynamic characteristics.
Grid generation (Mathematics)
Computational grids.
Description
Item Description:Shipping list no.: 99-0933-M.
Physical Description:1 volume.

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