Research Catalog

Lewis Icing Research Tunnel test of the aerodynamics effects of aircraft ground deicing/anti-icing fluid

Title
Lewis Icing Research Tunnel test of the aerodynamics effects of aircraft ground deicing/anti-icing fluid [microform] / L. James Runyan ... [et al.].
Publication
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1992.

Details

Additional Authors
  • Runyan, L. James.
  • United States. National Aeronautics and Space Administration. Scientific and Technical Information Program.
Description
1 v.
Series Statement
NASA technical paper ; 3238
Subject
  • Aerodynamic characteristics
  • Boeing aircraft
  • Deicing
  • Ice formation
  • Newtonian fluids
  • Rheology
  • Wind tunnel tests
Note
  • Shipping list no.: 93-0009-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.15:3238
OCLC
marcive39636236
Title
Lewis Icing Research Tunnel test of the aerodynamics effects of aircraft ground deicing/anti-icing fluid [microform] / L. James Runyan ... [et al.].
Imprint
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1992.
Series
NASA technical paper ; 3238
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1992] 2 microfiches.
Added Author
Runyan, L. James.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Program.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:3238
Research Call Number
READEX Microfiche NAS 1.15:3238
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