@inproceedings{2a35433d0dec4cc18f237922afda9726,
title = "Simulation of boundary layer transition on elliptic cones in hypersonic flow",
abstract = "Results are presented from DNS computations on a 4:1 elliptic cone in hypersonic flow. Solutions are obtained on large grids using a high order, low dissipation scheme to capture the very small scales in the flow. This allows for the study of disturbance growth occurring in both the centerline and crossflow boundary layers. The simulations are based on flow visualization experiments due to Huntley.3 Acoustic noise is added into the computational freestream to fully model the experimental conditions. In the work presented here four Reynolds numbers were simulated and found to have good agreement with experiment.",
author = "Bartkowicz, {Matthew D.} and Subbareddy, {Pramod K.} and Candler, {Graham V}",
year = "2010",
doi = "10.2514/6.2010-1064",
language = "English (US)",
isbn = "9781600867392",
series = "48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition",
publisher = "American Institute of Aeronautics and Astronautics Inc.",
booktitle = "48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition",
}