Experimental and computational investigation of lift-enhancing tabs on a multi-element airfoil
By: Dale Ashby.
Contributors: United States. National Aeronautics and Space Administration.
Series: JIAA TR -- 116.; [NASA contractor report] -- NASA-CR-201482.; NASA contractor report -- NASA CR-201482.
Publisher: Joint Institute for Aeronautics and Acoustics, National Aeronautics and Space Administration, Ames Research Center; Joint Institute for Aeronautics and Acoustics, Stanford University; National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1996
Place of publication: [Stanford, Calif.]; [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Aerodynamic coefficients.; Boundary layer separation.; Incompressible flow.; Separated flow.; Tabs (control surfaces); Airfoils.; Potential flow.; Pressure distribution.; Flaps (Control surfaces); Lift augmentation.
Notes: Shipping list no.: 98-0846-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 3 microfiches.