A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92
By: Richard J. Re and William K. Abeyounis.
Contributors: Abeyounis, William Kelly.; Langley Research Center.
Series: NASA technical memorandum -- 110300.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1996
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Wind tunnel tests.; Pressure distribution.; Static pressure.; Engine inlets.; Aircraft engines.; Mach number.; Angle of attack.; Subsonic flow.
Notes: Shipping list no.: 98-0790-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 2 microfiches.
Table of contents: class: section