Andrew J. Neely

发表

LOW-TEMPERATURE ANALOGUE BURNER FACE PLATE TIME RESPONSE

Abd. Rahim Abu Talib, Peter T. Ireland, Andrew J. Neely, 2005 .

An immersed boundary method for fluid-structure interaction with compressible multiphase flows

Li Wang, John Young, Feng Han, 2017, J. Comput. Phys..

Numerical ans Experimental Research on Aerodynamics of a High-speed Passenger Vehicle within the HEXAFLY-INT Project

Johan Steelant, Marco Marini, Nina Voevodenko, 2016 .

Free Flight Testing in Hypersonic Flows: HEXAFLY-INT EFTV

David R. Buttsworth, Murat Tahtali, Andrew J. Neely, 2016 .

Analytical Models for Side Force Prediction of Fluidic Thrust Vectoring on High-Speed Vehicles

John Young, Andrew J. Neely, Hilbert van Pelt, 2015 .

Flight Testing Designs in HEXAFLY-INT for High-Speed Transportation

Dries Verstraete, Johan Steelant, Alexander Wagner, 2018 .

Computational study of the flow characteristics and separation efficiency in a mini-hydrocyclone

Andrew J. Neely, Jong-Leng Liow, Guofeng Zhu, 2012 .

Studies of ground effect automotive aerodynamics

Tracie Barber, Graham Doig, Andrew J. Neely, 2007, ATZautotechnology.

The Effect of Aircraft Integration Design on Gas Turbine Shaft Thermal Bow and the Newkirk Effect

Andrew J. Neely, E. O. Smith, 2014 .

Super-orbital re-entry in Australia: laboratory measurement, simulation and flight observation [Keynote lecture]

Neil Mudford, David R. Buttsworth, Andrew J. Neely, 2011 .

Robust Design Optimization of Two-Dimensional Scramjet Inlets

Tapabrata Ray, Neil Mudford, Matthew Brown, 2006 .

Thermal-structural modelling of TDLAS system for SCRAMSPACE hypersonic flight test

Andrew J. Neely, Rishabh Choudhury, Arnab Dasgupta, 2012 .

Turbine Blade Life Prediction Using Fluid-Thermal-Structural Interaction Modelling

Andrew J. Neely, I. A. Ubulom, Krishna Shankar, 2015 .

Permanent-Change Thermal Paints for Hypersonic Flight-Test

Robert Clark, Andrew J. Neely, Hans Riesen, 2010 .

Calibration of Thermal Paints for Hypersonic Flight Test

Andrew J. Neely, Wei C. Tjong, A. Neely, 2008 .

Flow establishment behind blunt bodies at hypersonic speeds in a shock tunnel

Gisu Park, Andrew J. Neely, Sudhir L. Gai, 2009, International Congress on High-Speed Imaging and Photonics.

Suppressing restricted shock separation in a subscale rocket nozzle using contour geometry

Graham Doig, Andrew J. Neely, K. Schomberg, 2016 .

Compact Low-Temperature Analogue of Aero Engine Fire-Certification Burner

Peter T. Ireland, Andrew J. Neely, Andrew J. Mullender, 2001 .

Performance Studies of Shock Vector Control Fluidic Thrust Vectoring

Andrew J. Neely, John Young, Fernando Gesto, 2007 .

COMPUTATIONAL STUDY ON CONDUCTION HEAT TRANSFER THROUGH A THIN FILM GAUGE

Abd. Rahim Abu Talib, Peter T. Ireland, Andrew J. Neely, 2005 .

Numerical Simulation of Low Velocity Impact on Plastic Laminates

Andrew J. Neely, Krishnakumar Shankar, Karthik Ram Ramakrishnan, 2010 .

High-Cycle Fatigue of Fan Blades Accounting for Fluid-Structure Interaction

John Young, Andrew J. Neely, Krishnakumar Shankar, 2012 .

Measurement of Vehicle Stability Coefficients in Hypersonic Wind Tunnels

David R. Buttsworth, Andrew J. Neely, Chris Kennell, 2015 .

The Effect of Compressor Shaft Geometry on Shaft Thermal Bow due to Natural Convection

Andrew J. Neely, E. O. Smith, 2015 .

Development of a Blade Parametric Modeling Methodology for Design and Analysis of Computer Experiments

Andrew J. Neely, Zafer Leylek, 2015 .

A Novel Liquid Crystal Image Processing Technique Using Multiple Gas Temperature Steps to Determine Heat Transfer Coefficient Distribution and Adiabatic Wall Temperature

Peter T. Ireland, Andrew J. Neely, Abd Rahim Abu Talib, 2004 .

CFD Analysis of Nosecone Geometries and a Generic 2D Scramjet

Russell R. Boyce, Andrew J. Neely, Andrew J. Neely, 2005 .

Suppressing Restricted Shock Separation in Thrust-Optimized Rocket Nozzles Using Contour Geometry

Graham Doig, Andrew J. Neely, K. Schomberg, 2015 .

The effect of boundary layer transition on jet interactions

Russell R. Boyce, N. R. Deepak, Neil Mudford, 2009 .

Detailed Investigation of Heat Flux Measurements Made in a Standard Propane-Air Fire-Certification Burner Compared to Levels Derived From a Low-Temperature Analog Burner

Abd. Rahim Abu Talib, Peter T. Ireland, Andrew J. Neely, 2005 .

Hypersonic Fluid–Structure Interaction on a Cantilevered Plate with Shock Impingement

David R. Buttsworth, Andrew J. Neely, Gaetano M. D. Currao, 2019, AIAA Journal.

In-flight Mapping of Heating on a Hypersonic Nose Cone

Andrew J. Neely, Judy Odam, Hans Riesen, 2009 .

Hypersonic Wind-Tunnel Free-Flying Experiments with Onboard Instrumentation

Neil Mudford, David R. Buttsworth, Andrew J. Neely, 2015 .

Detailed Investigation of Heat Flux Measurements Made in a Standard Propane-Air Fire-Certification Burner Compared to Levels Derived From a Low-Temperature Analogue Burner

Peter T. Ireland, Andrew J. Neely, Abd Rahim Abu Talib, 2003 .

Turbulent heat transfer measurements using liquid crystals

Peter T. Ireland, Andrew J. Neely, David R. H. Gillespie, 1999 .

CFD analysis of an ethylene-fueled intake-injection shock-induced-combustion scramjet configuration

Russell R. Boyce, Andrew J. Neely, A. Neely, 2005 .

FLOW STUDIES ON A HYDROGEN-FUELED CAVITY FLAME-HOLDER SCRAMJET

Russell R. Boyce, Neil Mudford, Andrew J. Neely, 2005 .

THE USE OF THERMOCHROMIC LIQUID CRYSTALS TO INVESTIGATE FLOW FIELD INTERACTIONS WITH THE GROUND AROUND A SUPERSONIC LAND SPEED RECORD VEHICLE

Tracie Barber, Eddie Leonardi, Andrew J. Neely, 2006 .

Transient Response of Thermal Paints for Use on Short- Duration Hypersonic Flight Tests

Andrew J. Neely, Philip J. Tracy, 2006 .

Extended surface convective cooling studies of engine components using the transient liquid crystal technique

Peter T. Ireland, Andrew J. Neely, A. Neely, 1997 .

OH PLIF Imaging of Supersonic Combustion using Cavity Injection

Russell R. Boyce, Neil Mudford, Andrew J. Neely, 2005 .

Calibration of Thermal Paints for Surface Temperature Measurement of HIFiRE-0 Flight

Andrew J. Neely, Rishabh Choudhury, 2012 .

Measurement of heating rates for earth entry at 13 kms-1

Richard G. Morgan, Andrew J. Neely, 1994 .