@inproceedings{4ef31d09dc474c16b72d366d012b5c27,
title = "Cfd analysis of slotted natural-laminar-flow concepts for ultra-efficient commercial aircraft",
abstract = "Slotted natural-laminar-flow airfoils are an enabling technology for development of ultra-efficient commercial aircraft. Design and analysis of vehicles using these airfoils requires tools for predicting flows with transitioning boundary layers. A prototype version of the HPCMP CREATE{\texttrademark}-AV Kestrel finite-element CFD solver COFFE which contains a laminar-turbulent transition prediction capability via the amplification factor transport model is exercised on several baseline SNLF airfoil geometries, and preliminary results are presented.",
author = "Stefanski, {Douglas L.} and Glasby, {Ryan S.} and Erwin, {J. Taylor} and Coder, {James G.}",
note = "Funding Information: This material is based in part upon work supported by the National Aeronautics and Space Administration (NASA) under cooperative agreement award number NNX17AJ95A. The work was performed under the University Leadership Initiative (ULI) at the University of Tennessee, Knoxville for the “Advanced Aerodynamic Design Center for Ultra-Efficient Commercial Vehicles.” Material presented in this paper is a product of the HPCMP CREATE{\texttrademark}-AV element of the Computational Research and Engineering for Acquisition Tools and Environments (CREATE) Program, sponsored by the U.S. Department of Defense HPC Modernization Program Office. Publisher Copyright: {\textcopyright} 2019, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.; AIAA Scitech Forum, 2019 ; Conference date: 07-01-2019 Through 11-01-2019",
year = "2019",
doi = "10.2514/6.2019-0293",
language = "English (US)",
isbn = "9781624105784",
series = "AIAA Scitech 2019 Forum",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "AIAA Scitech 2019 Forum",
}