Predicted aerodynamic characteristics of a NACA 0015 airfoil having a 25% integral-type trailing edge flap
By: Ahmed Hassan.
Contributors: Langley Research Center.
Series: [NASA contractor report] -- NASA/CR-1999-209328.; NASA contractor report -- NASA CR-209328.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1999
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Noise reduction.; Airfoils.; Blade-vortex interaction.; Navier-Stokes equation.; Trailing edge flaps.; Aerodynamic characteristics.; Grid generation (Mathematics); Computational grids.
Notes: Shipping list no.: 99-0933-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1999] 2 microfiches.