Parametric study on laminar flow for finite wings at supersonic speeds
By: Joseph Avila Garcia.
Contributors: United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 108852.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1994
Place of publication: [Washington, DC]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Boundary layer control.; Boundary layer stability.; Laminar boundary layer.; Laminar flow.; Supersonic speed.; Wings.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 95-0410-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 2 microfiches.