The Benefits of a Rotating Rig for Research into Advanced Turbine Cooling Systems
Rockets for use in upper atmosphere research
Design and operation of X-15 hypersonic research airplane
Smart Flow Control in Aircraft Engine Components & Component Interactions
Fuel/Oil System Thermal Management in Aircraft Turbine Engines
Cycle-Match Engine Models used in Functional Engine Design - An Overview
Fault Tolerant Design Methodology in Software for Safety Related Systems
Theory for the Use of Foreign Gas in Simulating Film Cooling
The Gas Turbine Engine Conceptual Design Process - An Integrated Approach
Gas turbine engine test cell instrumentation : STO-TR-AVT-180 ; final report of task group AVT-180
The Introduction of Reinforced TMC Materials into Rotating Machinery - The Safe Approach
Designing for Reliability - The Rolls-Royce Approach
A Mixed Flow Turbofan Afterburner Simulation for the Definition of Reheat Fuel Control Laws
Design of a New Fighter Engine - The Dream in an Engine Man's Life
Simultaneous Active Source Control of Blade Row Interaction Generated Discrete Tones
La fiabilite des roulements aeronautiques et le comportement en fatigue
Keynote Address "Design Principles and Methods for Military Turbojet Engines"
Improved Gas Turbine Response using LQR Control
Design of an Active Stall Avoidance System for a Subsonic Axial Compressor
A One Dimensional, Time Dependent Inlet/Engine Numerical Simulation for Aircraft Propulsion Systems
Actuation System for Variable Exhaust Nozzle and Inlet Guide Vanes on an Advanced Gas Turbine Engine
F/A-18 E/F Aircraft Engine (F414-GE-400) Design and Development Methodology
Scramjet Performance Analysis in function of Combustion Process Parameters
Advanced Computational Fluid Dynamics in the Design of Military Turbines
Noise issues associated with the operation of gas turbine powered military vehicles
The F-15 Active Aircraft "The Next Step"
Acquisition et demonstration des technologies pour futurs moteurs militaires - Le programme AMET
Advanced CFD Tools for Multi-Stage Turbine Analysis
Microchannel Heat Pipe Cooling of Modules
Lightweight Electronic Enclosures Using Composite Materials
Developing Affordable Gas Turbine Engines
Distributed Architectures for Advanced Engine Control Systems
Combined-Cycle Engines for Hypersonic Applications
Neural Adaptive Control of an Engine Exhaust Nozzle
Computer Modeling of Heat Generation in Vapor Lubricated Bearings for Gas Turbines
NATO reference mobility modelling
Monitoring and Control of Helicopter Engines at Abnormal Operating Conditions
Advanced Standard Electronic Modules Format-E (SEM-E) Processes for Rapid Prototyping
Turbomachinery Blade Design Using a Navier-Stokes Solver and Artificial Neural Network
Three-Dimensional Inverse Design Method for Turbine and Compressor Blades