@inproceedings{7feda7db7a594de38c5308e2c6fa65d4,
title = "Numerical simulation of jet-wake vortex interaction",
abstract = "The interaction of aircraft exhaust jet and wake vortex is numerically studied. Following the preceding numerical study of wake vortex evolution from roll-up until vortex decay, we aim to simulate the jet-vortex interaction from the early phase until the complete roll-up. For numerical simulation we employ an unstructured mesh Reynolds-averaged Navier-Stokes solver for a flow around an aircraft model, while a Cartesian mesh large-eddy simulation solver implemented on the framework of the Building-Cube Method (BCM) is used for the mid- to far-field wake. Here we investigate a coupling approach of the above solvers to simulate the roll-up of exhaust jet and aircraft wake. The results show that a multi-level Cartesian mesh of the BCM is effective to capture the evolution of aircraft wake including exhaust jet.",
author = "Takashi Misaka and Shigeru Obayashi and Anton Stephan and Frank Holz{\"a}pfel and Thomas Gerz and Kazuhiro Nakahashi",
year = "2014",
doi = "10.2514/6.2014-0926",
language = "English",
isbn = "9781624102561",
series = "52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014",
publisher = "American Institute of Aeronautics and Astronautics Inc.",
booktitle = "52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014",
note = "52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014 ; Conference date: 13-01-2014 Through 17-01-2014",
}