Aerial Deployed Unfolding Autonomous Glider System (AIAA 2015-0374)
Advanced Vehicle Concepts in the Next Generation Air Transportation System
Feasibility of In-Flight Quadrotor Individual Motor Thrust Measurements (AIAA 2016-1760)
Vapour aluminide coating of internal cooling channels, in turbine blades and vanes
Impact of Using Reliever Airports to Absorb Additional Demand in the Potomac TRACON
Eye-Tracking Analysis of Near-Term Terminal Automation for Arrival Coordination
Assessing the Impact of FAME and Diesel Fuel Composition on Stability and Vehicle Filter Blocking
Fundamentals of Supercritical Mixing and Combustion of Cryogenic Propellants
Design Methodology and Analysis of Composite Blades for a Low Weight Rotor
Experimental and Numerical Investigation of Airfoil Performance in Cylinder Wake (AIAA 2018-3232)
Integrated Hole and Countersink Inspection of Aircraft Components
Design and Fabrication of a Tri-C30 Multichip Module Building Block
The DTI FSU Nuclear Legacy Programme: Spent Nuclear Fuel Management at Andreeva Bay
The Effect of Future Vehicles on Controller and Pilot Workload
The wheel/rail interface - some recent accidents
Application of Space Station Freedom (SSF) DMS Technology to Fault Tolerant Avionics Systems
Electromechanical Clutch Actuator: Design, Analysis and Experiments
GT2011-46537 Prognostics and Health Management of Aircraft Engine EMA Systems
Development of a Small-Scale Collins-Type 10K Cryocooler for Space Applications
Comparison of AFR Calculation Methods Using Gas Analysis and Mass Flow Measurement
DATIDS - The University of Minnesota Distributed Air-Traffic Information Display Simulator
Managing Irregular Operations in a Free Flight Environment
The Cockpit Cognitive Walkthrough
The Dissemination of Knowledge in the Aviation System: A Case Study on Pre-flight Planning
Controller Design Methodology for a Circulation Controlled Vertical Axis Wind Turbine
Spacecraft and Constellation Design for a Continuous Responsive Imaging System in Space
Development of a Medium-Scale Collins-Type 10 K Cryocooler
HIGH THROUGHPUT 600 WATT HALL EFFECT THRUSTER FOR SPACE EXPLORATION (AIAA 2016-4830)
2010-9067 Cranfield Graduate Aircraft Design Education
Individual Cylinder Fuel Control with a Switching Oxygen Sensor