| Uncertainty quantification of CFD data generated for a model scramjet isolator flowfield RA Baurle, EL Axdahl JANNAF Joint Subcommittee Meeting, 2017 | 15 | 2017 |
| The Enhanced Injection and MIxing Project at NASA Langley KF Cabell, TG Drozda, EL Axdahl, PM Danehy JANNAF CS/APS/EPSS/PSHS Joint Subcommittee Meeting, 2014 | 14 | 2014 |
| Study of Forebody Injection and Mixing with Application to Hypervelocity Airbreathing Propulsion E Axdahl, A Kumar, A Wilhite 48th Joint Propulsion Conference and Exhibit, 2012 | 13 | 2012 |
| Reusable lunar transportation architecture utilizing orbital propellant depots J Gaebler, R Lugo, E Axdahl, P Chai, M Grimes, M Long, R Rowland, ... AIAA SPACE 2009 Conference & Exposition, 6711, 2009 | 11 | 2009 |
| Flight Dynamics of an Aeroshell Using an Attached Inflatable Aerodynamic Decelerator E Axdahl, JR Cruz, M Schoenenberger, A Wilhite 20th Aerodynamic Decelerator Systems Technology Conference and Seminar, 2009 | 5 | 2009 |
| Numerical investigation and optimization of a flushwall injector for scramjet applications at hypervelocity flow conditions TG Drozda, R Shenoy, EL Axdahl, RA Baurle AIAA Propulsion and Energy 2019 Forum, 4196, 2019 | 4 | 2019 |
| Uninstalled performance predictions of a magnesium-fueled ramjet cycle in carbon dioxide atmospheres EL Axdahl, L Li 2018 Joint Propulsion Conference, 4448, 2018 | 4 | 2018 |
| Pre-Test CFD for the Design and Execution of the Enhanced Injection and Mixing Project at NASA Langley Research Center TG Drozda, EL Axdahl, KF Cabell JANNAF CS/APS/EPSS/PSHS Joint Subcommittee Meeting, 2014 | 4 | 2014 |
| Study of Unsteady, Sphere-Driven, Shock-Induced Combustion for Application to Hypervelocity Airbreathing Propulsion E Axdahl, A Kumar, A Wilhite 47th Joint Propulsion Conference and Exhibit, 2011 | 4 | 2011 |
| Comparison of several global mixing performance metrics for high-speed fuel injectors CR Ground, TG Drozda, KF Cabell, EL Axdahl 22nd AIAA international space planes and hypersonics systems and …, 2018 | 3 | 2018 |
| Mitigation of Autoignition Due to Premixing in a Hypervelocity Flow Using Active Wall Cooling E Axdahl, A Kumar, A Wilhite 49th Joint Propulsion Conference and Exhibit, 2013 | 3 | 2013 |
| An Automated DAKOTA and VULCAN-CFD Framework with Application to Supersonic Facility Nozzle Flowpath Optimization EL Axdahl NASA, 2015 | 2 | 2015 |
| A Study of Premixed, Shock-Induced Combustion with Application to Hypervelocity Flight EL Axdahl Georgia Institute of Technology, 2013 | 2 | 2013 |
| A 2nd Order Uncertainty Quantification Framework Applied to a Turbulence Model Validation Effort RA Baurle, EL Axdahl DATAworks 2019, 2019 | | 2019 |
| Shifting Data Collection from a Fixed to an Adaptive Sampling Paradigm EL Axdahl MODSIM World 2018, 2018 | | 2018 |
| Hypervelocity Mixing Experiments at NASA Langley M DePiro, T Drozda, E Axdahl, K Cabell, P Danehy NASA Fundamental Aeronautics Program 2012 Technical Conference, 2012 | | 2012 |
| Flight Dynamics of an Aeroshell Using an Attached Inflatable Aerodynamic Decelerator JR Cruz, M Schoenenberger, E Axdahl, A Wilhite 20th AIAA Aerodynamic Decelerator Systems Technology Conference, 2009 | | 2009 |
Tomasz DrozdaNASABestätigte E-Mail-Adresse bei nasa.gov
