@inproceedings{b3efbb792a004f039812e665d81786bb,
title = "Computational assessment of the hvab rotor in hover using laminar-turbulent transition modeling",
abstract = "Hover predictions of the Hover Validation and Acoustic Baseline (HVAB) rotor are made using a computational fluid dynamics approach. Solutions are generated using the NASA OVERFLOW 2.2n solver with both hybrid RANS/LES and laminar-turbulent transition modeling enabled. Solutions are based on a hover tip Mach number of 0.675 for a pre-deformed rotor with prescribed collective pitch, lag, and coning angles. Grid generation and computational methods are described. The rotor flowfield is analyzed and the effect of the transition model is assessed through comparison to predictions made using a fully-turbulent modeling approach.",
author = "Carnes, {Jared A.} and Coder, {James G.}",
note = "Publisher Copyright: {\textcopyright} 2019 by Timothy K. Minton. Published by the American Institute of Aeronautics and Astronautics, Inc.; AIAA Scitech Forum, 2019 ; Conference date: 07-01-2019 Through 11-01-2019",
year = "2019",
doi = "10.2514/6.2019-0288",
language = "English (US)",
isbn = "9781624105784",
series = "AIAA Scitech 2019 Forum",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "AIAA Scitech 2019 Forum",
}