Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport
By: Milton Lamb and William K. Abeyounis.
Contributors: Abeyounis, William Kelly.; Langley Research Center.
Series: NASA technical memorandum -- 87627.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service
Published: 1986
Place of publication: Washington, D.C; Springfield, Va
Language: eng
Format: Microform
Subjects: Airplanes -- Nacelles.; Transonic planes -- Wings -- Testing.; Aerodynamic drag.; Nacelles.; Pylons.; Skin friction.; System effectiveness.; Wind tunnel tests.
Notes: Prepared at Langley Research Center.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration], 1986. 1 microfiche.