Results for the hybrid laminar flow control experiment conducted in the NASA Langley 3-FT transonic pressure tunnel on a 7-ft chord model
By: Percy J. Bobbitt ... [et al.].
Contributors: Bobbitt, Percy J.; Langley Research Center.
Series: NASA technical memorandum -- 107582.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1992
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Aerofoils.; Laminar flow.; Transonic wind tunnels.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 94-0809-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1994] 1 microfiche.