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A flight test of laminar flow control leading-edge systemsNASA's program for development of a laminar flow technology base for application to commercial transports has made significant progress since its inception in 1976. Current efforts are focused on development of practical reliable systems for the leading-edge region where the most difficult problems in applying laminar flow exist. Practical solutions to these problems will remove many concerns about the ultimate practicality of laminar flow. To address these issues, two contractors performed studies, conducted development tests, and designed and fabricated fully functional leading-edge test articles for installation on the NASA JetStar aircraft. Systems evaluation and performance testing will be conducted to thoroughly evaluate all system capabilities and characteristics. A simulated airline service flight test program will be performed to obtain the operational sensitivity, maintenance, and reliability data needed to establish that practical solutions exist for the difficult leading-edge area of a future commercial transport employing laminar flow control.
Document ID
19830067138
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Fischer, M. C.
(NASA Langley Research Center Hampton, VA, United States)
Wright, A. S., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Wagner, R. D.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 11, 2013
Publication Date
October 1, 1983
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 83-2508
Report Number: AIAA PAPER 83-2508
Accession Number
83A48356
Distribution Limits
Public
Copyright
Other

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