Integration effects of D-shaped, underwing, aft-mounted, separate-flow, flow-through nacelles on a high-wing transport /

Integration effects of D-shaped, underwing, aft-mounted, separate-flow, flow-through nacelles on a high-wing transport / Milton Lamb, John R. Carlson, and Odis C. Pendergraft.

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Bibliographic Details
Online Access: Online Access
Main Authors: Lamb, Milton (Author), Carlson, John R. (Author), Pendergraft, Odis C. (Author)
Corporate Authors: Langley Research Center, United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Format: Government Document eBook
Language:English
Published: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division, November 1987.
Series:NASA technical memorandum ; 4018.
Subjects:
Angle of attack.
Nacelles.
Separated flow.
Supersonic flow.
Transonic wind tunnels.
Description
Item Description:"November 1987."
"Performing organization: NASA Langley Research Center"Report documentation page.
Physical Description:1 online resource (21 pages) : illustrations.
Bibliography:Includes bibliographical references (page 3)

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