An Analysis of the Impact of Extreme Attitude Operation on a Turbofan Engine in a Regional Jet Aircraft

Abstract

Verbatim from NASA NTRS. Not paraphrased, not summarized.

The objective of this work is to characterize the variability in engine performance at extreme attitudes, resulting from the use of different standard control variables, evaluated at different points in the engine’s lifecycle. This paper describes the procedure used to create a dynamic model of an aft-mounted jet engine on a T-tail regional jet aircraft. This model enables simulation of engine operation at extreme attitudes. The model was subsequently evaluated at various altitudes, Mach numbers, and power settings over a range of angles of attack and sideslip, and deterioration levels. Each case was simulated using both fan speed and engine pressure ratio as the engine control variable. The results show that the wing has a very large impact on the engine operation, overwhelming other sources of variation.

Authors

• Jonathan S Litt Glenn Research Center
• T Shane Sowers HX5, LLC
• Daniel A Trowbridge ZIN Technologies ( United States)

Keywords

• loss of control - inflight
• LOC-I
• Sensitivity study
• Gas Turbine Engine
• T-Tail