Collection efficiency and ice accretion calculations for a sphere, a swept MS(1)-317 wing, a swept NACA-0012 wing tip, an axisymmetric inlet, and a Boeing 737-300 inlet
By: Colin S. Bidwell and Stanley R. Mohler.
Contributors: Mohler, Stanley R.; United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 106831.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1995
Place of publication: [Washington, DC]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Accumulations.; Aircraft icing.; Engine inlets.; Spheres.; Swept wings.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 95-0410-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 1 microfiche.