Investigation to optimize the passive shock wave/boundary layer control for supercritical airfoil drag reduction
Subtitle: semi-annual report for the period March 16, 1983 to September 14, 1983
By: by H.T. Nagamatsu, R. Ficarra, R. Orozco.
Contributors: Ficarra, R.; Orozco, R.; Langley Research Center.
Series: [NASA-CR] -- 173276.; NASA contractor report -- NASA CR-173276.
Publisher: NASA Langley Research Center
Published: 1983
Place of publication: [Hampton, Va.?]
Language: eng
Format: Microform
Subjects: Aerofoils.; Boundary layer control.; Boundary layer control.; Drag reduction.; Shock waves.; Supercritical wings.
Notes: Also available via Internet from the NTRS web site. Address as of 10/03/07: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19840008067%5F1984008067.pdf  ; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration], 1984. 1 microfiche.