Investigation to optimize the passive shock wave/boundary layer control for supercritical airfoil drag reduction
Subtitle: final report
By: by H.T. Nagamatsu and R. Dyer.
Contributors: Dyer, R.; Langley Research Center.
Series: [NASA-CR] -- 175788.; NASA contractor report -- NASA CR-175788.
Publisher: National Aeronautics and Space Administration, Langley Research Center
Published: 1984
Place of publication: [Hampton, Va.?
Language: eng
Format: Microform
Subjects: Aerofoils.; Boundary layer control.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration, 1985] 1 microfiche.