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.

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Call Number:	NAS 1.15:4018
NAS 1.15:4018	Available