The effect of incoming boundary layer characteristics on the performance of a distributed propulsion system /

Bibliographic Details

Main Authors:	Upadhyay, Puja (Author), Zaman, K. B. M. Q. (Khairul B. M. Q.) (Author)
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, March 2019.
Series:	NASA technical memorandum ; 2019-220068.
Subjects:	American Institute of Aeronautics and Astronautics. Boundary layer ingestion propulsion. Flow distribution. Subsonic speed. Aircraft models. Velocity measureement.
Online Access:	https://purl.fdlp.gov/GPO/gpo121300