Cfd analysis of slotted natural-laminar-flow concepts for ultra-efficient commercial aircraft

Douglas L. Stefanski, Ryan S. Glasby, J. Taylor Erwin, James G. Coder

Research output: Chapter in Book/Report/Conference proceedingConference contribution

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™-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.

Original languageEnglish (US)
Title of host publicationAIAA Scitech 2019 Forum
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624105784
DOIs
StatePublished - 2019
EventAIAA Scitech Forum, 2019 - San Diego, United States
Duration: Jan 7 2019Jan 11 2019

Publication series

NameAIAA Scitech 2019 Forum

Conference

ConferenceAIAA Scitech Forum, 2019
Country/TerritoryUnited States
CitySan Diego
Period1/7/191/11/19

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering

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