Wing pressure distributions from subsonic tests of a high-wing transport model
By: Zachary T. Applin and Carl L. Gentry, Jr., M.A. Takallu.
Contributors: Gentry, Carl L.; Takallu, Mohammad Ali, 1948-; Langley Research Center.
Series: NASA technical memorandum -- 4583.
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: Angle of attack.; Leading edge flaps.; Mach number.; Pressure distribution.; Reynolds number.; Sideslip.; Subsonic flow.; Trailing edge flaps.; Transport aircraft.; Wind tunnel tests.; Wings.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 95-0478-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 5 microfiches.