REVIEW OF NASA COMBUSTOR AND TURBINE HEAT TRANSFER RESEARCH.

This report presents a summary of the mainstream effort in combustor and turbine heat transfer research being conducted and sponsored by the NASA Lewis Research Center (LeRC). The report focuses on the breadth of the heat transfer problems associated with the design and development of gas turbine engine hot sections and on the research, both currently underway and planned, that is producing the technological approaches to understand and solve these problems.