All Stories

  1. Assessing General Propulsion Architectures for Fast Transit Times to Mars for Crewed Missions

    Article • July 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Scott M Martin, Vivek Bhatt

  2. Mitigating Engine Unstart in Scramjets With Porous Bleeders

    Article • January 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Scott M Martin

  3. Non-Adiabatic SCRAMJET Turbulent Combustion Modelling With the Tabulated Conditional Moment Closure Model

    Article • January 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Scott M Martin

  4. Turbulent Combustion Model for Hydrogen Jet in a Supersonic Crossflow

    Article • January 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Scott M Martin

  5. Emissions and Flame Characteristics of a High-Pressure Reacting Jet-in-Crossflow

    Article • January 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Scott M Martin

  6. Numerical Simulation of an Axial Reacting Jet-in-Crossflow at Elevated Pressure

    Article • January 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Scott M Martin

  7. Effects of Dilution on Reacting Jet in Crossflow Flame Characteristics at High Pressure

    Article • January 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Scott M Martin

  8. Experimental and Numerical Investigation of a High-Pressure Reacting Jet-in-Crossflow

    Article • August 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Scott M Martin

  9. Premixed Reacting Jet Flow Behavior in an Axially Staged Model Combustor at Elevated Pressure

    Article • August 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Scott M Martin

  10. NOx Emission of an Axial-Staged Combustor at High-Pressure

    Article • August 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Scott M Martin

  11. Turbulence-Kinetics Interaction Effects on Liquid Fuel Scramjet Kinetic Mechanisms

    Article • March 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Scott M Martin

  12. Exploration of a Reacting Jet-in-Crossflow in a High-Pressure Axial Stage Combustor

    Article • August 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Scott M Martin

  13. Characteristics of a Premixed Reacting Jet-in-Crossflow at Elevated Pressures

    Article • August 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Scott M Martin

  14. Large Eddy Simulation Of Turbulent Reacting Flow Using Premixed Conditional Moment Closure Method

    Article • January 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Scott M Martin

  15. A Counter-flow Diffusion Flame study for the Supercritical CO2 Combustion

    Article • January 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Scott M Martin

  16. Reacting Unsteady Reynolds-Averaged Navier–Stokes with the Tabulated Premixed Conditional Moment Closure Method

    Article • Journal of Propulsion and Power, May 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Scott M Martin

  17. Analytical Forms of the Range Performance of Hybrid and Electric Turboprop Aircraft, for Design Optimization Studies

    Article • January 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Scott M Martin

  18. Large Eddy Simulation of an Enclosed Turbulent Reacting Methane Jet With the Tabulated Premixed Conditional Moment Closure Method

    Article • Journal of Engineering for Gas Turbines and Power, April 2016, ASME International

    Dr Scott M Martin

  19. LES Simulation of an Enclosed Turbulent Reacting Methane Jet With the Tabulated Premixed CMC Method

    Article • June 2015, ASME International

    Dr Scott M Martin

  20. Unsteady Rans Simulation of an Enclosed, Turbulent Reacting Methane Jet with the Premixed CMC Method

    Article • January 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Scott M Martin

  21. Application of Flamelet Generated Manifolds Approach with Heat Loss Inclusion to a Turbulent High-Pressure Premixed Confined Jet Flame

    Article • January 2015, Springer Science + Business Media

    Dr Scott M Martin

  22. Modeling an Enclosed, Turbulent Reacting Methane Jet With the Premixed Conditional Moment Closure Method

    Article • June 2013, ASME International

    Dr Scott M Martin

  23. Numerical Simulations of a Premixed Turbulent Confined Jet Flame Using the Flamelet Generated Manifold Approach With Heat Loss Inclusion

    Article • June 2013, ASME International

    Dr Scott M Martin

  24. Self-induced unstable behaviors of CH4 and H2/CH4 flames in a model combustor with a low-swirl injector

    Article • Combustion and Flame, February 2013, Elsevier

    Dr Scott M Martin

  25. High pressure jet flame numerical analysis of CO emissions by means of the flamelet generated manifolds technique

    Article • January 2013, American Institute of Physics

    Dr Scott M Martin

  26. Large Eddy Simulation/Eulerian Probability Density Function Approach for Simulating Hydrogen-Enriched Gas Turbine Combustors

    Article • June 2012, ASME International

    Dr Scott M Martin

  27. Measurement of Flame Characteristics of a Low Swirl Burner at High Pressures and Velocities

    Article • January 2011, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Scott M Martin

  28. Effect of Combustor Inlet Geometry on Acoustic Signature and Flow Field Behavior of the Low Swirl Injector

    Article • January 2010, ASME International

    Dr Scott M Martin

  29. The Premixed Conditional Moment Closure Method Applied to Idealized Lean Premixed Gas Turbine Combustors

    Article • Journal of Engineering for Gas Turbines and Power, January 2003, ASME International

    Dr Scott M Martin

  30. The Premixed Conditional Moment Closure Method Applied to Idealized Lean Premixed Gas Turbine Combustors

    Article • January 2002, ASME International

    Dr Scott M Martin

  31. Chemical reactor modeling applied to the production of pollutant emission in LP combustors

    Article • July 1997, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Scott M Martin

  32. Effects of Incomplete Premixing on NO x Formation at Temperature and Pressure Conditions of LP Combustion Turbines

    Article • June 1997, ASME International

    Dr Scott M Martin