Publication Date:
2013-08-31
Description:
The main objectives of the NASA sponsored Aerothermal Modeling Program, Phase 2, Element C, are to collect benchmark quality data to quantify the fuel spray interaction with the turbulent swirling flows and to validate current and advanced two phase flow models. The technical tasks involved in this effort are discussed.
Keywords:
FLUID MECHANICS AND HEAT TRANSFER
Type:
Turbine Engine Hot Section Technology, 1987; p 101-110
Format:
application/pdf