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    CFD 2030 Grand Challenge: CFD-in-the-Loop Monte Carlo Flight Simulation for Space Vehicle Design

    Schuster, David M. | AIAA | 2021

    CFD 2030 GRAND CHALLENGE: CFD-IN-THE-LOOP MONTE CARLO FLIGHT SIMULATION FOR SPACE VFHICLE DESIGN

    Schuster, David M. | TIBKAT | 2021

    Future of NASA's Aerosciences Capability

    Schuster, David M. / D'Agostino, Mark G. | NTRS | 2017

    Remote Imaging of Exploration Flight Test-1 (EFT-1) Entry Heating Risk Reduction

    Schuster, David M. / Horvath, Thomas J. / Schwartz, Richard J. | NTRS | 2016

    Investigation of Unsteady Pressure-Sensitive Paint (uPSP) and a Dynamic Loads Balance to Predict Launch Vehicle Buffet Environments

    Schuster, David M. / Panda, Jayanta / Ross, James C. et al. | NTRS | 2016

    Infrared Observations of the Orion Capsule During EFT-1 Hypersonic Reentry

    Horvath, Thomas J. / Rufer, Shann J. / Schuster, David M. et al. | NTRS | 2016

    Plans and Example Results for the 2nd AIAA Aeroelastic Prediction Workshop

    Heeg, Jennifer / Chwalowski, Pawel / Schuster, David M. et al. | NTRS | 2015

    Time-Accurate Unsteady Pressure Loads Simulated for the Space Launch System at Wind Tunnel Conditions

    Alter, Stephen J. / Brauckmann, Greg J. / Kleb, William L. et al. | AIAA | 2015

      Time-Accurate Unsteady Pressure Loads Simulated for the Space Launch System at Wind Tunnel Conditions

      Alter, Stephen J. / Brauckmann, Gregory J. / Kleb, William L. et al. | NTRS | 2015

    Plans and Example Results for the 2^n^d AIAA Aeroelastic Prediction Workshop (AIAA 2015-0437)

    Heeg, Jennifer / Chwalowski, Pawel / Raveh, Daniella E. et al. | British Library Conference Proceedings | 2015

    Time-Accurate Unsteady Pressure Loads Simulated for the Space Launch System at Wind Tunnel Conditions (AIAA 2015-3149)

    Alter, Stephen J. / Brauckmann, Greg J. / Kleb, William L. et al. | British Library Conference Proceedings | 2015

    Time Accurate Unsteady Pressure Loads Simulated for the Space Launch System at a Wind Tunnel Condition

    Alter, Stephen J. / Brauckmann, Gregory J. / Kleb, Bil et al. | NTRS | 2015

    Orion Multi-Purpose Crew Vehicle (MPCV) Capsule Parachute Assembly System (CPAS) Wake Deficit Wind Tunnel Testing

    Ross, James C. / Schuster, David M. | NTRS | 2014

    Overview of the Aeroelastic Prediction Workshop

    Heeg, Jennifer / Chwalowski, Pawel / Schuster, David M. et al. | NTRS | 2013

      Overview of the Aeroelastic Prediction Workshop

      Heeg, Jennifer / Chwalowski, Pawel / Florance, Jennifer P. et al. | NTRS | 2013

    Analysis of Test Case Computations and Experiments for the First Aeroelastic Prediction Workshop

    Schuster, David M. / Heeg, Jennifer / Wieseman, Carol D. et al. | NTRS | 2013

    Lessons Learned in the Selection and Development of Test Cases for the Aeroelastic Prediction Workshop: Rectangular Supercritical Wing

    Heeg, Jennifer / Chwalowski, Pawel / Wieseman, Carol D. et al. | NTRS | 2013

    Modeling, Analysis and Simulation Approaches Used in Development of the National Aeronautics and Space Administration Max Launch Abort System

    Yuchnovicz, Daniel E. / Dennehy, Cornelius J. / Schuster, David M. | NTRS | 2011

    Grid Fin Stabilization of the Orion Launch Abort Vehicle

    Pruzan, Daniel A. / Mendenhall, Michael R. / Rose, William C. et al. | NTRS | 2011

    Multi-functional annular fairing for coupling launch abort motor to space vehicle

    Camarda, Charles J. / Scotti, Stephen J. / Buning, Pieter G. et al. | NTRS | 2011

    Design and Analysis of Outer Mold Line Close-outs for the Max Launch Abort System (MLAS) Flight Experiment

    Woods-Vedeler, Jessica A. / Knutson, Jeffrey R. / Schuster, David M. et al. | NTRS | 2010

    Air Data Boom System Development for the Max Launch Abort System (MLAS) Flight Experiment

    Woods-Vedeler, Jessica A. / Cox, Jeff / Bondurant, Robert et al. | NTRS | 2010

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