@conference{37c8456eb61d47b29ac16774d4187535,
title = "Effects of transition modeling on the simulation of helicopter rotor hubs",
author = "Coder, {James G.}",
note = "Funding Information: This research was partially funded by the US Army{\textquoteright}s National Rotorcraft Technology Center program, effort sponsored by the US Government under Other Transaction number Fig. 17: Integrated streamwise-momentum SPOD modal energies for low-drag hub AFT solution. Funding Information: W15QKN-10-9-0003 between Vertical Lift Consortium, Inc. and the Government, and by the Government under Agreement No. W911W6-17-2-0003. The US Government is authorized to reproduce and distribute reprints for Governmental purposes notwithstanding any copyright notation thereon. The views and conclusions contained herein are those of the authors and should not be interpreted as necessarily representing the official policies or endorsements, either expressed or implied, of the US Government.; Vertical Flight Society's 75th Annual Forum and Technology Display ; Conference date: 13-05-2019 Through 16-05-2019",
year = "2019",
language = "English (US)",
}