Current Research
Robust Operation and Performance Limiting Mechanisms in Kilowatt-Scale High-Speed Gas Turbine Engine
Bi-Directional Turbomachinery for use in pumped thermal energy storage - J. Chiapperi
Novel Propulsion Architectures for Unmanned Aerial Vehicles - M. Shorter
A Reduced Order Model Framework for Operability Assessment of Damaged Blades - K. Wong
Conceive, Design, Build, and Demonstrate a Rocket Engine Turbopump and Test Bed - K. Ruecker
Demonstration of a 1MW Class Integrated Motor-generator - Y.K. Chen, A. Dowdle, M. Qasim
Off-design Compressor Performance Estimation of Axial Multi-stage Compressors - A. Joerger, Y. Wan
Modular Hybrid Propulsion System - A. Kunycky and D. Pham
Forced Response System Identification of Cavitation Instabilities - M. Campbell
An Integrated Boundary-Layer Ingesting Propulsion System for Electric Aircraft
Assessment of Installed Turbofan Performance & Stability of Advanced Aircraft
Novel Propulsion Architectures for Unmanned Aerial Vehicles - M. Shorter