D. J. Mee

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All published works
Action Title Year Authors
+ Heat Transfer Measurements of the BOLT II Flight Experiment Model within the T4 Reflected Shock Tunnel 2023 Will O. Landsberg
Jacob Sandral
D. J. Mee
Ananthanarayanan Veeraragavan
+ Heat Transfer Measurements in an Expansion Tube Using Infrared Thermography 2021 Ranjini Garani Ramesh
Richard G. Morgan
D. J. Mee
+ A Calibration Procedure for Performing Infrared Thermography in Expansion Tubes 2021 Ranjini Garani Ramesh
Richard G. Morgan
D. J. Mee
+ Transition-Length Predictions for Hypersonic Flows with an Adverse Pressure Gradient 2020 Isaac Convery-Brien
Sreekanth Raghunath
D. J. Mee
+ Magnetohydrodynamic drag force measurements in an expansion tunnel using a stress wave force balance 2020 Daniel R. Smith
David Gildfind
D. J. Mee
Christopher M. James
Barry V. Allsop
+ Infrared Thermography in Expansion Tubes for Martian Entry Flows 2020 Ranjini Garani Ramesh
Richard G. Morgan
Ranjith Ravichandran
D. J. Mee
+ Magnetohydrodynamic drag force measurements in expansion tunnels using an accelerometer-based force balance 2019 Daniel R. Smith
David Gildfind
Timothy J. McIntyre
D. J. Mee
Christopher M. James
Andreas Andrianatos
+ Shock Layer Radiation Measurements at a Mars Entry Condition for Infrared Thermography 2019 Ranjini Garani Ramesh
Rory Kelly
Timothy G. Cullen
Richard G. Morgan
D. J. Mee
+ Estimating Turbulent Spot Initiation Rates from Transition Lengths in Hypersonic Boundary Layers 2017 Sreekanth Raghunath
D. J. Mee
Roddam Narasimha
+ Performance comparison of distributed injection methods for hypersonic film-cooling 2016 Kevin Basore
Markus Selzer
Vincent Wheatley
Russell Boyce
D. J. Mee
Bianca R. Capra
Markus Kuhn
Stefan Brieschenk
+ Force Measurement in Impulse Hypersonic Facilities 2016 D. J. Mee
+ Boundary layer transition in hypersonic flows 2016 D. J. Mee
Sreekanth Raghunath
+ Free Piston Shock Tunnels HEG, HIEST, T4 and T5 2015 Klaus Hannemann
Katsuhiro Itoh
D. J. Mee
H. G. Hornung
+ Experimental Testing of an Airframe-Integrated Three-Dimensional Scramjet at Mach 10 2015 Luke J. Doherty
Michael K. Smart
D. J. Mee
+ Measurement of Three-Components of Force on an Airframe Integrated Scramjet at Mach 10 2015 Luke J. Doherty
Michael K. Smart
D. J. Mee
+ Experimental Testing of an Airframe Integrated 3-D Scramjet at True Mach 10 Flight Conditions 2014 Luke J. Doherty
Michael K. Smart
D. J. Mee
+ Nozzle design study for a quasi-axisymmetric scramjet-powered vehicle at Mach 7.9 flight conditions 2013 Katsuyoshi Tanimizu
D. J. Mee
Raymond J. Stalker
Peter A. Jacobs
+ Design of an Airframe Integrated 3D Scramjet and Experimental Results at a Mach 10 Flight Condition 2012 Luke J. Doherty
Michael K. Smart
D. J. Mee
+ Supersonic Skin-Friction Drag with Tangential Wall Slot Fuel Injection and Combustion 2012 Rainer Kirchhartz
D. J. Mee
Raymond J. Stalker
+ Suitability of the <i>k</i>–<i>ω</i> turbulence model for scramjet flowfield simulations 2011 W. Y. K. Chan
Peter A. Jacobs
D. J. Mee
+ Thrust Nozzle Design Study for a Quasi-Axisymmetric Scramjet-Powered Vehicle 2010 Katsuyoshi Tanimizu
D. J. Mee
Raymond J. Stalker
Peter A. Jacobs
+ Drag force on quasi-axisymmetric scramjets at various flight Mach numbers: theory and experiment 2009 Katsuyoshi Tanimizu
D. J. Mee
Raymond J. Stalker
Peter A. Jacobs
+ Boundary Layers on a Flat Plate at Sub- and Superorbital Speeds 2007 M. J. Hayne
D. J. Mee
S. L. Gai
Timothy J. McIntyre
+ Background oriented schlieren for flow visualisation in hypersonic impulse facilities 2007 Dwishen Ramanah
Sreekanth Raghunath
D. J. Mee
Thomas RĂśsgen
Peter A. Jacobs
+ Comparison of drag measurements of two axisymmetric scramjet models at Mach 6 2007 K. Tanimizu
D. J. Mee
R. J. Stalker
+ Numerical Simulation of a Ludwieg-tube Fuel Delivery System for Scramjet Experiments in Shock Tunnels 2007 Crown Plaza
Dhananjay Y. Gangurde
D. J. Mee
Peter A. Jacobs
+ Supersonic combustion experiments in the T4 Shock Tunnel 2007 D. J. Mee
+ Measurement and Prediction of the Force of an Unfuelled Axisymmetric Scramjet Model 2006 Katsuyoshi Tanimizu
D. J. Mee
Raymond J. Stalker
+ Scramjet Flow Visualization Using Background Oriented Schlieren in Hypersonic Impulse Facilities 2006 Dwishen Ramanah
D. J. Mee
+ Scramjet Lift, Thrust and Pitching-Moment Characteristics Measured in a Shock Tunnel 2006 Matthew J. Robinson
D. J. Mee
A. Paull
+ Scramjets and shock tunnels—The Queensland experience 2005 R. J. Stalker
A. Paull
D. J. Mee
Richard G. Morgan
Peter A. Jacobs
+ Skin Friction Reduction in Hypersonic Turbulent Flow by Boundary Layer Combustion 2005 Milinda Suraweera
D. J. Mee
Raymond J. Stalker
+ Compressible, Turbulent Flow with Boundary-Layer Heat Addition 2005 Andrew Denman
Peter A. Jacobs
D. J. Mee
+ Performance measurements in a shock tunnel of a fuelled scramjet vehicle generating lift, thrust and pitching moment 2005 Matthew J. Robinson
D. J. Mee
+ Flow establishment over rearward-facing steps in high enthalpy flows 2005 M. J. Hayne
D. J. Mee
S. L. Gai
B. S. Stewart
Richard G. Morgan
+ Real gas effects on flows over rearward-facing steps in high enthalpy flows 2005 M. J. Hayne
S. L. Gai
D. J. Mee
Richard G. Morgan
+ Rarefied, superorbital flows in an expansion tube 2004 Vincent Wheatley
Han-Chieh Chiu
Peter A. Jacobs
M. N. Macrossan
D. J. Mee
Richard G. Morgan
+ Visualization Of Supersonic Flows In Shock Tunnels, Using The Background Oriented Schlieren Technique 2004 Sreekanth Raghunath
D. J. Mee
T. Roesgen
Peter A. Jacobs
+ Heat transfer and flow behind a step in high enthalpy superorbital flow 2003 M. J. Hayne
D. J. Mee
Richard G. Morgan
S. L. Gai
T. J. Mclntyre
+ Measurement of the aerodynamic performance of a scramjet-powered vehicle in a shock tunnel 2003 Matthew J. Robinson
D. J. Mee
A. Paull
+ Developing a stress wave thrust balance for a hypersonic shock tunnel 2002 S. L. Tuttle
J. M. Simmons
D. J. Mee
+ Sonic line location in reacting flows 2002 Richard G. Morgan
Madhat Abdel‐jawad
D. J. Mee
+ Dynamic calibration of force balances 2002 D. J. Mee
+ Heat transfer and flow behind a rearward facing step in a super-orbital expansion tube 2002 M. J. Hayne
S. L. Gai
R. Hillier
Richard G. Morgan
D. J. Mee
T. J. McIntyre
+ Design, modelling and analysis of a six component force balance for hypervelocity wind tunnel testing 2001 A. L. Smith
D. J. Mee
W.J.T. Daniel
Takayuki Shimoda
+ Heat transfer behind a step in high enthalpy super-orbital flow 2001 S. L. Gai
M. J. Hayne
A. Gardener
Richard G. Morgan
D. J. Mee
+ Boundary layer transition measurements in hypervelocity flows in a shock tunnel 2001 D. J. Mee
+ Hyshot scramjet testing in the T4 shock tunnel 2000 M. Frost
A. Paull
Hans Alesi
D. J. Mee
+ Comparison of force measurements in the HEG and T4 shock tunnels 1999 M.K.H. Weiland
D. J. Mee
A. Paull
W.H. Beck
+ Three-Component Force Measurements on a Scramjet in a Reflected-Shock Tunnel 1998 Ching‐Yi Tsai
R. J. Bakos
D. J. Mee
+ Turbulent spots in boundary layers in a free-piston shock-tunnel flow 1996 D. J. Mee
Christopher P. Goyne
+ Turbulent spots in boundary layers in a free-piston shock-tunnel flow 1996 D. J. Mee
Christopher P. Goyne
+ Drag measurements in a hypervelocity expansion tube 1996 A. L. Smith
D. J. Mee
+ Drag measurements in a hypervelocity expansion tube 1996 A. L. Smith
D. J. Mee
+ Drag measurements at Mach 5 using a stress wave force balance 1995 S. L. Tuttle
D. J. Mee
J. M. Simmons
+ Experiments on supersonic combustion ramjet propulsion in a shock tunnel 1995 A. Paull
R. J. Stalker
D. J. Mee
+ Scramjet thrust measurement in a shock tunnel 1995 A. Paull
R. J. Stalker
D. J. Mee
+ Shock Tunnel Studies of Scramjet Phenomena 1993 1995 R. J. Stalker
R. J. Bakos
Richard G. Morgan
L.M.L. Porter
D. J. Mee
A. Paull
Sarah Tuttle
J. M. Simmons
M. Wendt
K. A. Skinner
+ Use of Argon-Helium Driver-Gas Mixtures in the T4 Shock Tunnel 1995 Peter A. Jacobs
Richard G. Morgan
R. J. Stalker
D. J. Mee
+ New Techniques for Force and Pressure Measurement in Hypervelocity Impulse Facilities 1995 JM Simmons
D. J. Mee
S. L. Tuttle
W Cook Daniel
SC Overton
AL Smith
+ Supersonic combustion ramjet propulsion experiments in a shock tunnel 1995 A. Paull
R. J. Stalker
D. J. Mee
+ Shock tunnel measurements of hypervelocity blunted cone drag 1994 L.M.L. Porter
A. Paull
D. J. Mee
J. M. Simmons
+ Measurement of scramjet thrust in shock tunnels 1994 R. J. Stalker
J. M. Simmons
A. Paull
D. J. Mee
+ Drag measurements on blunted cones and a scramjet vehicle in hypervelocity flow 1993 L.M.L. Porter
D. J. Mee
A. Paull
+ Investigation of swept shock wave boundary layer interactions 1987 D. J. Mee
Common Coauthors
Commonly Cited References
Action Title Year Authors # of times referenced
+ Experiments on supersonic combustion ramjet propulsion in a shock tunnel 1995 A. Paull
R. J. Stalker
D. J. Mee
13
+ Drag measurements at Mach 5 using a stress wave force balance 1995 S. L. Tuttle
D. J. Mee
J. M. Simmons
7
+ Hypersonic and high temperature gas dynamics 2013 J. D. Anderson
7
+ Millisecond aerodynamic force measurement with side-jet model in theISL shock tunnel 1993 K. W. Naumann
H. van den Ende
G. Mathieu
A. George
6
+ Measurements of heat transfer to a flat plate in a dissociated high-enthalpy laminar air flow 1980 R. A. East
R. J. Stalker
J. P. Baird
6
+ Scramjets and shock tunnels—The Queensland experience 2005 R. J. Stalker
A. Paull
D. J. Mee
Richard G. Morgan
Peter A. Jacobs
6
+ Control of Hypersonic Turbulent Skin Friction by Boundary- Layer Combustion of Hydrogen 2005 R. J. Stalker
6
+ Generalized reference enthalpy formulations and simulation of viscous effects in hypersonic flow 1998 G. Simeonides
5
+ Mass spectrometric measurements of driver gas arrival in the T4 free-piston shock-tunnel 2005 Russell Boyce
M. Takahashi
R. J. Stalker
5
+ Scramjet Lift, Thrust and Pitching-Moment Characteristics Measured in a Shock Tunnel 2006 Matthew J. Robinson
D. J. Mee
A. Paull
5
+ PDF Chat Design of Three-Dimensional Hypersonic Inlets with Rectangular-to-Elliptical Shape Transition 1999 Michael K. Smart
5
+ Hypersonic Airbreathing Propulsion 1994 William H. Heiser
David T. Pratt
Daniel H. Daley
Unmeel B. Mehta
5
+ Drag force on quasi-axisymmetric scramjets at various flight Mach numbers: theory and experiment 2009 Katsuyoshi Tanimizu
D. J. Mee
Raymond J. Stalker
Peter A. Jacobs
5
+ Scramjet thrust measurement in a shock tunnel 1995 A. Paull
R. J. Stalker
D. J. Mee
4
+ An evaluation of theories for predicting turbulent skin friction andheat transfer on flat plates at supersonic and hypersonic Mach numbers 1971 Edward J. Hopkins
M. Inouye
4
+ PDF Chat A pseudo-temporal multi-grid relaxation scheme for solving the parabolized Navier-Stokes equations 1999 J. A. White
Joseph Morrison
4
+ A review of reaction rates and thermodynamic and transport properties for the 11-species air model for chemical and thermal nonequilibrium calculations to 30000 K 1989 Roop N. Gupta
Jerrold M. Yos
Richard A. Thompson
4
+ Measurement of Flow Properties and Thrust on Scramjet Nozzle Using Pressure-Sensitive Paint 2009 Christian Hirschen
Ali GĂźlhan
Walter Beck
Ulrich Henne
4
+ Shock-Tunnel Experiments with a Mach 12 Rectangular-to-Elliptical Shape-Transition Scramjet at Offdesign Conditions 2009 Milinda Suraweera
Michael K. Smart
4
+ Measurements of heat transfer in separated highenthalpy dissociated laminar hypersonic flow behind a step 1989 S. L. Gai
N. T. Reynolds
C. Ross
J. P. Baird
4
+ PDF Chat Comparative Surface Heat Transfer Measurements in Hypervelocity Flow 2011 William Flaherty
Joanna M. Austin
4
+ High-Enthalpy Aerothermodynamics of a Mars Entry Vehicle Part 1: Experimental Results 1997 Brian R. Hollis
John Perkins
4
+ Shock tunnel measurements of hypervelocity blunted cone drag 1994 L.M.L. Porter
A. Paull
D. J. Mee
J. M. Simmons
4
+ Heat transfer and transition to turbulence in the shock-induced boundary layer on a semi-infinite flat plate 1969 William R. Davies
L. Bernstein
4
+ Heat-transfer measurements in short-duration hypersonic facilities 1973 D. L. Schultz
T. V. Jones
4
+ Measurement of heat transfer in superorbital flows 2000 R. Palmer
4
+ The Superorbital Expansion Tube concept, experiment and analysis 1994 Andrew Neely
Richard G. Morgan
4
+ Supersonic hydrogen combustion with a short thrust nozzle 1984 R. J. Stalker
Richard G. Morgan
4
+ An experimental investigation of an airframe integrated three-dimensional scramjet engine at a Mach 10 flight condition 2014 Luke J. Doherty
4
+ Skin Friction Reduction in Hypersonic Turbulent Flow by Boundary Layer Combustion 2005 Milinda Suraweera
D. J. Mee
Raymond J. Stalker
4
+ Experiments on cruise propulsion with a hydrogen scramjet 1998 R. J. Stalker
A. Paull
4
+ Simultaneous Lift, Moment and Thrust Measurements on a Scramjet in Hypervelocity Flow 2003 Matthew Robinson
4
+ About the formulation, verification and validation of the hypersonic flow solver Eilmer 2013 Rowan Gollan
Peter A. Jacobs
3
+ Heat Transfer Measurements on the Afterbody of Spheres in Hypersonic Free-Flight in Air and Carbon Dioxide 2015 Michael C. Wilder
David W. Bogdanoff
David Saunders
3
+ Review of Problems in Application of Supersonic Combustion 1964 Antonio Ferri
3
+ Skin-friction measurements in high-enthalpy hypersonic boundary layers 2003 Christopher P. Goyne
R. J. Stalker
A. Paull
3
+ Drag measurements in a hypervelocity expansion tube 1996 A. L. Smith
D. J. Mee
3
+ Hypersonic ignition and thrust production in a scramjet 1993 A. Paull
3
+ A Simplex Method for Function Minimization 1965 J. A. Nelder
R. Mead
3
+ Free-Flight Measurements of Convective Heat Transfer in Hypersonic Ballistic-Range Environments 2007 Michael C. Wilder
Daniel C. Reda
David W. Bogdanoff
Dinesh Prabhu
3
+ Skin-Friction Measurements in a Supersonic Combustor with Crossflow Fuel Injection 2001 Hideyuki Tanno
A. Paull
R. J. Stalker
3
+ Simulation and Optimization of Heated, Inviscid Flows in Scramjet Ducts 1999 Peter A. Jacobs
Chris S. Craddock
3
+ Quasi-one-dimensional modeling of a free-piston shock tunnel 1994 Peter A. Jacobs
3
+ Turbulent spots in boundary layers in a free-piston shock-tunnel flow 1996 D. J. Mee
Christopher P. Goyne
3
+ Mass spectrometry in shock tunnel experiments of hypersonic combustion 1994 K. A. Skinner
3
+ Design of an Airbreathing Second Stage for a Rocket-Scramjet-Rocket Launch Vehicle 2013 Thomas Jazra
Dawid Preller
Michael K. Smart
3
+ Silane as an ignition aid in scramjets 1987 Norman Morris
Richard G. Morgan
A. Paull
R. J. Stalker
3
+ Waves and Thermodynamics in High Mach Number Propulsive Ducts 1991 R. J. Stalker
3
+ The interaction of a shock wave with a laminar boundary layer at a compression corner in high-enthalpy flows including real gas effects 1997 S. G. Mallinson
S. L. Gai
N. R. Mudford
3
+ Flight Data Analysis of the HyShot 2 Scramjet Flight Experiment 2006 Michael K. Smart
Neal Hass
Allan Paull
3