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Influence of Surface Properties and Impact Conditions on Insect Residue AdhesionAirflow over airfoils used on current commercial aircraft transitions from laminar to turbulent at relatively low chord positions. As a result, drag increases, requiring more thrust to maintain flight. An airfoil with increased laminar flow would experience reduced drag and a lower fuel burn rate. One of the objectives of NASA's Environmentally Responsible Aviation project is to identify and demonstrate technologies that will enable more environmentally friendly commercial aircraft. While more aerodynamically efficient airfoil shapes can be designed, surface contamination from ice, dirt, pollen, runway debris, and insect residue can degrade performance.
Document ID
20150009474
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Wohl, Christopher J.
(NASA Langley Research Center Hampton, VA, United States)
Doss, Jereme R.
(National Inst. of Aerospace Hampton, VA, United States)
Shanahan, Michelle H.
(National Inst. of Aerospace Hampton, VA, United States)
Smith, Joseph G., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Penner, Ronald K.
(Science and Technology Corp. Hampton, VA, United States)
Connell, John W.
(NASA Langley Research Center Hampton, VA, United States)
Siochi, Emilie J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
June 3, 2015
Publication Date
February 20, 2015
Subject Category
Aerodynamics
Nonmetallic Materials
Report/Patent Number
NF1676L-20493
Report Number: NF1676L-20493
Meeting Information
Meeting: Annual Meeting of the Adhesion Society
Location: Savannah, GA
Country: United States
Start Date: February 20, 2015
End Date: February 25, 2015
Sponsors: Adhesion Society, Inc.
Funding Number(s)
WBS: WBS 699959.02.20.07.03.02
Distribution Limits
Public
Copyright
Public Use Permitted.
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