Assessment of dual-point drag reduction for an executive-jet modified airfoil section
By: Dennis O. Allison and Raymond E. Mineck.
Contributors: Mineck, Raymond E.; Langley Research Center.
Series: NASA techical paper -- 3579; NASA technical paper -- 3579.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1996
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Airfoil profiles.; Angle of attack.; Boundary layer transition.; Drag reduction.; Force distribution.; Pitching moments.; Reynolds number.; Trailing edges.; Transonic wind tunnels.; Aerodynamic characteristics.
Other titles: Assessment of dual point drag reduction for an executive-jet modified airfoil section
Notes: Shipping list no.: 98-0733-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 2 microfiches.