NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Juncture flow control using leading-edge filletsFlow measurements have been made in the wake region of a simulated wing-fuselage juncture, with and without leading-edge fillets, in order to assess the effect of leading-edge modifications on the flow field around the juncture. Preliminary results indicate that there is some reduction in juncture drag at moderate angles of attack with the use of leading-edge fillets. There is also evidence of improvement in the flow characteristics on the surface downstream of the juncture when fillets are used. As the fillet size is increased, flow characteristics start deteriorating at some point, and an optimum fillet size may be required to achieve an overall improvement in the flow field.
Document ID
19860029716
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kubendran, L. R.
(NASA Langley Research Center Hampton, VA, United States)
Harvey, W. D.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
October 1, 1985
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 85-4097
Accession Number
86A14454
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available