Wakelam, CT and Hynes, TP and Evans, SW and Hodson, HP and Chanez, P (2008) The effect of boundary layer trips on intake separation in crosswinds. In: UNSPECIFIED.Full text not available from this repository.
The flow typical of that occurring over the windward lip of an aero engine intake operating in a crosswind has been reproduced on a 2D lip. The uncontrolled boundary layer undergoes a laminar separation at the leading edge of the lip. It has been shown that a minimum size of boundary layer trip, positioned upstream of the separation location, is required to enable the flow to remain attached around the leading edge. A turbulent separation then occurs in the diffuser. Larger diameter trips promote earlier diffuser separation. Copyright © 2008 by the American Institute of Aeronautics and Astronautics, Inc.
|Item Type:||Conference or Workshop Item (UNSPECIFIED)|
|Divisions:||Div A > Turbomachinery|
|Depositing User:||Cron Job|
|Date Deposited:||09 Dec 2016 18:23|
|Last Modified:||23 Feb 2017 06:49|