Research Catalog

Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport

Title
Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport [microform] / Milton Lamb and William K. Abeyounis.
Author
Lamb, Milton.
Publication
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986.

Details

Additional Authors
  • Abeyounis, William Kelly.
  • Langley Research Center.
Description
1 v.
Series Statement
NASA technical memorandum ; 87627
Subject
  • Airplanes > Nacelles
  • Transonic planes > Wings > Testing
  • Aerodynamic drag
  • Nacelles
  • Pylons
  • Skin friction
  • System effectiveness
  • Wind tunnel tests
Note
  • Prepared at Langley Research Center.
Reproduction (note)
  • Microfiche.
Call Number
GPO Microfiche NAS 1.15:87627
OCLC
marcive166422470
Author
Lamb, Milton.
Title
Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport [microform] / Milton Lamb and William K. Abeyounis.
Imprint
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986.
Series
NASA technical memorandum ; 87627
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration], 1986. 1 microfiche.
Added Author
Abeyounis, William Kelly.
Langley Research Center.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:87627
Research Call Number
GPO Microfiche NAS 1.15:87627
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