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)