An eddy-viscosity limited algebraic stress model for shock-boundary- layer interaction
Effects of compressibility and roughness for turbulence modelling of hypersonic ramp flow
Effects of Compressibility and Roughness for Turbulence Modelling of Hypersonic Ramp Flow
Managing Reaction Wheel Microvibration on a High Resolution EO Small Spacecraft
Managing Micro-Vibration on the SSTL300-S1 a 400 Kg 1 M Resolution Earth Imaging Spacecraft
Towards Topology-Free Optimization: An Application to Turbine Internal Cooling Geometries
Towards Topology-Free Optimization: An Application to Turbine Internal Cooling Geometries
Dilute Gas/Droplet Flow Past a Frontward Facing Step
Dilute Gas / Droplet Flow Past a Frontward Facing Step
Energy dissipation in spacecraft structures incorporating bolted joints with viscoelastic layers
Energy dissipation in spacecraft structures incorporating bolted joints with viscoelastic layers
Orbit Transfer of Small Spacecraft with a Vortex Flow Hybrid Rocket
Transitioning DARPA Science and Technology Results into Space Capabilities II
Extending Satellite Lifetimes in Geosynchronous Orbit with Servicing
Development of an Electrical Data Exchange Interface based on STEP AP212
ON-ORBIT SERVICING OF DEPARTMENT OF DEFENSE AND NATIONAL SECURITY SPACE ASSETS
Large Eddy Simulation of a Harrier Aircraft at Touch Down
Particle acceleration, magnetic field generation, and emission in relativistic shocks
Particle acceleration, magnetic field generation, and emission in relativistic shocks
Development of an electrical data exchange interface based on STEP AP212
NigeriaSat-2 AOCS: Results from the First 90 Days in Orbit (AAS 12-093)
Enhancing NSS System Engineering Analysis through Value-Centric Design Methodology
Enhancing NSS System Performance by Including Value-Centric Analysis (VCA)
Small satellite computer-aided design and manufacturing
A General Methodology for Analysis of Structure-Borne Micro-Vibration
Low Cost Propulsion Developments for Small Spacecraft at the Surrey Space Centre
Energy Dissipation in Spacecraft Structures Incorporating Bolted Joints Operating in Macroslip
AN INVESTIGATION OF A LOW COST HTP/KEROSENE 40 N THRUSTER FOR SMALL SATELLITES