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Record 3 of 3
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Author
Runyan, L. James, author.
Title
Lewis Icing Research Tunnel test of the aerodynamic effects of aircraft ground deicing/anti-icing fluids / L. James Runyan [and three others].
Publication Info.
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, August 1992.
Connect to
Connect to https://ntrs.nasa.gov/citations/19920021152
Copies
Location
Call No.
OPAC Message
Status
Axe Federal Documents Online
NAS 1.60:3238
---
Available
Description
1 online resource (iii, 129 pages) : illustrations.
text txt rdacontent
computer c rdamedia
online resource cr rdacarrier
Series
NASA technical paper ; 3238
NASA technical paper ; 3238.
Note
"August 1992"--Report documentation page.
"Performing organization: National Aeronautics and Space Administration Lewis Research Center"--Report documentation page.
Type Of Report
Technical paper.
Funding
Sponsored by National Aeronautics and Space Administration WU-505-68-11 E-5808
Note
Online resource; title from PDF title page (NASA, viewed June 21, 2017).
Subject
Aerodynamic characteristics.
Boeing aircraft.
Deicing.
Ice formation.
Newtonian fluids.
Rheology.
Wind tunnel tests.
Genre/Form
Online resources.
Added Author
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Program, issuing body.
Other Form:
Print version: Lewis icing research tunnel test of the aerodynamic effects of aircraft ground deicing/anti-icing fluids (OCoLC)664373995
Microfiche version: Lewis Icing Research Tunnel test of the aerodynamics effects of aircraft ground deicing/anti-icing fluid (OCoLC)39636236
Gpo Item No.
0830-H-15 (online)
Sudoc No.
NAS 1.60:3238
Available items only
