NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Investigation of powered nacelles on a high aspect ratio NASA supercritical wing, phase 2A modified wing with the long core separate flow nacelle and several E(3) nacelles was utilized. The effects of nacelle and pylon cant angles and nacelle longitudinal and vertical location were investigated over a Mach number range from 0.70 to 0.83. The results at the cruise condition 0.82 Mach number and 0.55 lift coefficient are presented.
Document ID
19810010482
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Flechner, S. G. (NASA Langley Research Center Hampton, VA, United States)
Patterson, J. C., Jr. (NASA Langley Research Center Hampton, VA, United States)
Fournier, P. G. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 11, 2013
Publication Date
February 1, 1981
Publication Information
Publication: Advan. Aerodyn. and Active Controls
Subject Category
Aircraft Design, Testing And Performance
Accession Number
81N19008
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitle19810010475Collected WorksAdvanced aerodynamics and active controls. Selected NASA research
No Preview Available