M. Wright

发表

Mars Science Laboratory Entry Capsule Aerothermodynamics and Thermal Protection System

K. Edquist, B. Hollis, B. Laub, 2007, 2007 IEEE Aerospace Conference.

Data-parallel lower-upper relaxation method for reacting flows

J. Mcdonald, G. Candler, M. Wright, 1994 .

Data-Parallel Line Relaxation Method for the Navier -Stokes Equations

G. Candler, M. Wright, D. Bose, 1998 .

A data-parallel LU relaxation method for the Navier-Stokes equations

G. Candler, M. Wright, M. Prampolini, 1995 .

Thermal protection system development, testing, and qualification for atmospheric probes and sample return missions: Examples for Saturn, Titan and Stardust-type sample return

B. Laub, E. Venkatapathy, J. Arnold, 2009 .

M. Wright, D. Bose, G. Palmer, 2005 .

M. Wright, D. Schwenke, Helen H. Hwang, 2007 .

Boundary Layer Stability Analysis of Mars Science Laboratory Aeroshell

G. Candler, M. Wright, H. Johnson, 2006 .

Numerical study of inviscid shock interactions on double-wedge geometries

G. Candler, M. Wright, J. Olejniczak, 1997, Journal of Fluid Mechanics.

Sizing and Margins Assessment of the Mars Science Laboratory Aeroshell Thermal Protection System

Karl T. Edquist, David M. Driver, Eric Slimko, 2009 .

Data-parallel lower-upper relaxation method for the navier-stokes equations

Graham V. Candler, Marco Prampolini, Michael J. Wright, 1996 .

Collision Integrals for Ion-Neutral Interactions of Nitrogen and Oxygen

M. Wright, E. Levin, 2004 .

A Review of Aerothermal Modeling for Mars Entry Missions

Karl T. Edquist, Brian R. Hollis, Michael J. Wright, 2010 .

Validation of Afterbody Aeroheating Predictions for Planetary Probes: Status and Future Work

James L. Brown, G. Candler, M. Wright, 2005 .

Viking Afterbody Heating Computations and Comparisons to Flight Data

Karl T. Edquist, Michael J. Wright, Gary A. Allen, 2006 .

Kinetic Rates for Gas-Phase Chemistry of Phenolic-Based Carbon Ablator in Atmospheric Air

I. Boyd, M. Wright, Alexandre Martin, 2015 .

Impact of Flowfield-Radiation Coupling on Aeroheating for Titan Aerocapture

Deepak Bose, Michael J. Wright, M. Wright, 2005 .

Uncertainty Analysis of Laminar Aeroheating Predictions for Mars Entries

Deepak Bose, Grant Palmer, Michael J. Wright, 2005 .

Comment on "X-33 Computational Aeroheating Predictions and Comparisons with Experimental Data"

James L. Brown, E. Venkatapathy, M. Wright, 2003 .

Implicit Surface Boundary Conditions for Blowing, Equilibrium Composition, and Diffusion-limited Oxidation

M. Wright, M. Maclean, M. Barnhardt, 2010 .

Preliminary Convective-Radiative Heating Environments for a Neptune Aerocapture Mission

Dinesh K. Prabhu, Brian R. Hollis, Naruhisa Takashima, 2004 .

Chemistry model for ablating carbon-phenolic material during atmospheric re-entry

I. Boyd, M. Wright, Alexandre Martin, 2010 .

A Code Calibration Study for Huygens Entry Aeroheating

Michael J. Wright, Brian R. Hollis, Joseph Olejniczak, 2006 .

Photon drag radiation monitors for use with pulsed CO2 lasers

M. Kimmitt, M. Wright, D. C. Tyte, 1972 .

The Use of Probabilistic Modeling for Reentry Thermal Protection System Design

N. Mansour, M. Wright, D. Bose, 2008 .

An Approach to Shock Envelope Grid Tailoring and Its Effect on Reentry Vehicle Solutions

David Saunders, Michael J. Wright, Michael J. Wright, 2007 .

Paper Session I-B - Conceptual Design of a Cargo Lander for the First Lunar Outpost

Michael J. Wright, M. Wright, 1993 .

POST-FLIGHT AEROTHERMAL ANALYSIS OF HUYGENS PROBE

B. Hollis, M. Wright, D. Bose, 2006 .

Shock Layer Radiation Measurements and Analysis for Mars Entry

M. Wright, D. Bose, D. Bogdanoff, 2009 .

FIRE II calculations for hypersonic nonequilibrium aerothermodynamics code verification: DPLR, LAURA, and US3D

Graham V. Candler, Peter A. Gnoffo, Dinesh K. Prabhu, 2007 .

Development of the Mars Science Laboratory Heatshield Thermal Protection System

Karl T. Edquist, David M. Driver, Michael J. Wright, 2014 .

Development of the Mars Science Laboratory Heatshield Thermal Protection System

Karl T. Edquist, David M. Driver, Eric Slimko, 2009 .

Numerical Simulations of Protruding Gapfillers on the Mars Science Laboratory Heatshield

Karl T. Edquist, Alan Cassell, Michael J. Wright, 2009 .

Uncertainty and Sensitivity Analysis of Thermochemical Modeling for Titan Atmospheric Entry

Deepak Bose, Michael J. Wright, Tahir Gokcen, 2004 .

Computational Fluid Dynamics for Winged Re-entry Vehicles at Hypersonic Conditions

Dinesh K. Prabhu, James Reuther, David Saunders, 2004 .

Aerothermal analysis of the Project Fire II afterbody flow

Mark Loomis, Michael J. Wright, Periklis Papadopoulos, 2001 .

Experimental and computational study of high enthalpy double-wedge flows

Hans G. Hornung, Graham V. Candler, Michael J. Wright, 1999 .

Numerical/Experimental Investigation of 3-D Swept Fin Shock Interactions

S. Berry, G. Candler, M. Wright, 1998 .

High enthalpy double-wedge experiments

Hans G. Hornung, Graham V. Candler, Michael J. Wright, 1996 .

Numerical study of shock interactions on double-wedge geometries

G. Candler, M. Wright, J. Olejniczak, 1996 .

Effects of continuum breakdown on hypersonic aerothermodynamics

Iain D. Boyd, Andrew J. Lofthouse, Michael J. Wright, 2006 .

Aerothermodynamic Environments Definition for the Mars Science Laboratory Entry Capsule

Karl T. Edquist, Artem A. Dyakonov, Michael J. Wright, 2007 .

Augmented inertial navigation using cold atom sensing

Michael J. Wright, Jason F. Ralph, Simon Maskell, 2020 .

Commencing Scene Segmentation by Luminance Peak and Valley Detection

M. J. Wright, A. H. Ρinnington, M. Yazdanfar, 1991 .

A Comparison of Methods to Compute High-Temperature Gas Thermal Conductivity

Grant Palmer, Michael J. Wright, M. Wright, 2003 .

Shuttle Orbiter Contingency Abort Aerodynamics: Real-Gas Effects and High Angles of Attack

Paul Wercinski, Dinesh K. Prabhu, Ethiraj Venkatapathy, 2003 .

Numerical simulations of Atlas II rocket motor plumes

G. Candler, D. Levin, M. Wright, 2001 .

Modeling issues in the computation of plume radiation signatures

Graham V. Candler, Deborah A. Levin, Michael J. Wright, 1998 .

Scaling and simulation issues in ram accelerator projectile design

G. Candler, M. Wright, V. Weirs, 1997 .

Comparison of methods to compute high-temperature gas viscosity

Grant Palmer, Michael J. Wright, M. Wright, 2002 .

A Risk-Based Approach for Aerothermal/TPS Analysis and Testing

Michael J. Wright, Jay H. Grinstead, Deepak Bose, 2007 .

An Overview of Technology Investments in the NASA Entry Systems Modeling Project

Anthony M. Calomino, Michael Barnhardt, Monica Hughes, 2015 .

Computational Modeling of T5 Laminar and Turbulent Heating Data on Blunt Cones, Part 1 : Titan Applications

Hans G. Hornung, Karl T. Edquist, Michael J. Wright, 2005 .

Transition Onset and Turbulent Heating Measurements for the Mars Science Laboratory Entry Vehicle

Brian R. Hollis, Derek S. Liechty, Timothy Wadhams, 2005 .

Surface Heating from Remote Sensing of the Hypervelocity Entry of the NASA GENESIS Sample Return Capsule

Paul Wercinski, Dean Kontinos, George S. Rossano, 2006 .

Aerothermodynamic Design of the Mars Science Laboratory Backshell and Parachute Cone

Karl T. Edquist, Artem A. Dyakonov, Michael J. Wright, 2009 .

Collision Integrals for Ion-Neutral Interactions of Air and Argon

M. Wright, E. Levin, 2005 .

Validation Process for Blowing and Transpiration-Cooling in DPLR

D. Hash, S. Ruffin, M. Wright, 2007 .

Ground-to-Flight Traceability Analysis of Arcjet Testing for the Crew Exploration Vehicle

Michael J. Wright, Deepak Bose, James Reuther, 2009 .

Afterbody Aeroheating Flight Data for Planetary Probe Thermal Protection System Design

Michael J. Wright, Frank S. Milos, M. Wright, 2006 .

Status of aerothermal modeling for current and future Mars exploration missions

J. Olejniczak, E. Venkatapathy, K. Edquist, 2006, 2006 IEEE Aerospace Conference.

Survey of Afterbody Aeroheating Flight Data for Planetary Probe Thermal Protection System Design

Michael J. Wright, Philippe Tran, Frank S. Milos, 2005 .

Aeroheating Analysis for the Afterbody of a Titan Probe

Dinesh K. Prabhu, Deepak Bose, Michael J. Wright, 2004 .

Space Technology Mission Directorate Game Changing Development Program

Michael J. Wright, M. Wright, 2018 .

Overview of Entry Descent and landing investments in the NASA Exploration Technology Development Program

Charles H. Campbell, Karl T. Edquist, Michael J. Wright, 2011, 2011 Aerospace Conference.

Aeroheating Predictions for Phoenix Entry Vehicle

Ryan McDaniel, Michael J. Wright, M. Wright, 2008 .

Modeling of shock tunnel aeroheating data on the Mars Science Laboratory aeroshell

Hans G. Hornung, Karl T. Edquist, Michael J. Wright, 2006 .

Sizing and Margins Assessment of Mars Science Laboratory Aeroshell Thermal Protection System

Karl T. Edquist, David M. Driver, William Willcockson, 2014 .

Introduction: Atmospheric Entry of the Stardust Sample Return Capsule

Dean Kontinos, Michael J. Wright, M. Wright, 2010 .

Defining Ablative Thermal Protection System Margins for Planetary Entry Vehicles

Lockheed Martin, William Willcockson, Michael J. Wright, 2011 .

Probabilistic Modeling of Aerothermal and Thermal Protection Material Response Uncertainties

Deepak Bose, Michael J. Wright, Yih-Kanq Chen, 2007 .

Prediction of the Aerothermodynamic Environment of the Huygens Probe

Deepak Bose, Brian R. Hollis, Naruhisa Takashima, 2005 .

Base Flow Investigation of the Apollo AS-202 Command Module. Chapter 6

Michael J. Wright, Louis Walpot, Peter Noeding, 2011 .

Modeling of Stardust Entry at High Altitude, Part 1: Flowfield Analysis

Iain D. Boyd, Kerry A. Trumble, Michael J. Wright, 2010 .

Nonequilibrium Particle and Continuum Analyses of Stardust Entry for Near{Continuum Conditions

Iain D. Boyd, Kerry A. Trumble, Michael J. Wright, 2007 .

Analysis of the Forebody Aeroheating Environment during Genesis Sample Return Capsule Reentry

Michael Wright, M. Wright, Chun Tang, 2007 .

Uncertainty Analysis of Aeroheating Predictions for Titan Entries

Grant Palmer, Michael J. Wright, Joseph Olejniczak, 2006 .

Data Parallel Line Relaxation (DPLR) Code User Manual: Acadia - Version 4.01.1

Todd White, Michael J. Wright, Nancy L. Mangini, 2009 .

Analysis of Afterbody Heating Rates on the Apollo Command Modulels, Part I: AS-202

Dinesh K. Prabhu, Michael J. Wright, Edward R. Martinez, 2004 .

Analysis of Apollo Command Module Afterbody Heating Part I: AS-202

Dinesh K. Prabhu, Michael J. Wright, Edward R. Martinez, 2006 .

X-33 aerothermal design environment predictions - Verification and validation

James Brown, Michael J. Wright, Dinesh K. Prabhu, 2000 .

X-33 aerothermal design environment predictions - Review of acreage and local computations

Dean Kontinos, Michael J. Wright, Dinesh K. Prabhu, 2000 .

Experimental measurements of the permeability of fibrous carbon at high-temperature

Francesco Panerai, Nagi N. Mansour, Michael J. Wright, 2016, 1603.04844.