Organizational Unit:
Aerospace Systems Design Laboratory (ASDL)
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Probabilistic Matching of Turbofan Engine Performance Models to Test Data
A Work Transfer Perspective of Propulsion System Performance
Estimation of Turbofan Engine Performance Model Accuracy and Confidence Bounds
Performance Characterization of Turboshaft Engines Via Availability and Second Law Analysis
Implementation of Engine Loss Analysis Methods in the Numerical Propulsion System Simulation
Work Transfer Analysis of Turbojet and Turbofan Engines
The Role of Thermodynamic Work Potential in Aerospace Vehicle Design
Lost Thrust Methodology for Gas Turbine Engine Performance Analysis
Assessment of Uncertainty in Aerospace Propulsion System Design and Simulation
A Method for Thermodynamic Work Potential Analysis of Aircraft Engines