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.

Author/creator Lamb, Milton author.
Format Electronic
PublicationWashington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division, November 1987.
Description1 online resource (21 pages) : illustrations.
Supplemental Contenthttps://purl.fdlp.gov/GPO/gpo76181

Other author/creatorCarlson, John R., author.
Other author/creatorPendergraft, Odis C., author.
Other author/creatorLangley Research Center.
Other author/creatorUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
SeriesNASA technical memorandum ; 4018
NASA technical memorandum 4018. ^A467613
General note"November 1987."
General note"Performing organization: NASA Langley Research Center"Report documentation page.
General noteCRDP Program record.
Bibliography noteIncludes bibliographical references (page 3).
Report noteTechnical memorandum.
Funding informationSponsored by the National Aeronautics and Space Administration 505-68-91-06
Funding informationL-16342
Source of descriptionDescription based on online resource; title from PDF title page (NASA, viewed Jan. 11, 2017).
Issued in other formPrint version: Lamb, Milton. Integration effects of D-shaped, underwing, aft-mounted, separate-flow, flow-through nacelles on a high-wing transport
Issued in other formMicrofiche version: Lamb, Milton. Integration effects of D-shaped, underwing, aft-mounted, separate- flow, flow-through nacelles on a high-wing transport
GPO item number0830-D (online)
Govt. docs number NAS 1.15:4018