NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Laminar Flow Control Leading Edge Systems in Simulated Airline ServiceAchieving laminar flow on the wings of a commercial transport involves difficult problems associated with the wing leading edge. The NASA Leading Edge Flight Test Program has made major progress toward the solution of these problems. The effectiveness and practicality of candidate laminar flow leading edge systems were proven under representative airline service conditions. This was accomplished in a series of simulated airline service flights by modifying a JetStar aircraft with laminar flow leading edge systems and operating it out of three commercial airports in the United States. The aircraft was operated as an airliner would under actual air traffic conditions, in bad weather, and in insect infested environments.
Document ID
20040161127
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Wagner, R. D.
(NASA Langley Research Center Hampton, VA, United States)
Maddalon, D. V.
(NASA Langley Research Center Hampton, VA, United States)
Fisher, D. F.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 1988
Subject Category
Aircraft Stability And Control
Meeting Information
Meeting: 16th Congress of the International Council of the Aeronautical Sciences
Location: Jerusalem
Country: Israel
Start Date: August 28, 1988
End Date: September 2, 1988
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available