Pressure distributions from subsonic tests of a NACA 0012 semispan wing model
By: Zachary T. Applin.
Contributors: Langley Research Center.
Series: NASA technical memorandum -- 110148.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1995
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Aerodynamic configurations.; Airfoil profiles.; Dynamic pressure.; Free flow.; Pressure distribution.; Semispan models.; Subsonic speed.; Unswept wings.; Wind tunnel tests.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 96-0336-M.

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