| The relentless pursuit of hypersonic flight IA Leyva Physics Today 70 (11), 30-36, 2017 | 123 | 2017 |
| Laser-induced thermal acoustics (LITA) signals from finite beams EB Cummings, IA Leyva, HG Hornung Applied Optics 34 (18), 3290-3302, 1995 | 107 | 1995 |
| Experiments and numerical simulation of mixing under supercritical conditions T Schmitt, J Rodriguez, IA Leyva, S Candel Physics of Fluids 24 (5), 2012 | 84 | 2012 |
| Transition delay in hypervelocity boundary layers by means of CO2/acoustic instability interactions I Leyva, S Laurence, A Beierholm, H Hornung, R Wagnild, G Candler 47th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and …, 2009 | 77 | 2009 |
| Dark core analysis of coaxial injectors at sub-, near-, and supercritical conditions in a transverse acoustic field I Leyva, B Chehroudi, D Talley 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 5456, 2007 | 65 | 2007 |
| Carbon dioxide injection for hypervelocity boundary layer stability R Wagnild, G Candler, I Leyva, J Jewell, H Hornung 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and …, 2010 | 61 | 2010 |
| Experimental and computational study of high enthalpy double-wedge flows J Olejniczak, GV Candler, MJ Wright, I Leyva, HG Hornung Journal of Thermophysics and Heat Transfer 13 (4), 431-440, 1999 | 61 | 1999 |
| Transition within a hypervelocity boundary layer on a 5-degree half-angle cone in air/CO2 mixtures J Jewell, R Wagnild, I Leyva, G Candler, J Shepherd 51st AIAA Aerospace Sciences Meeting Including the New Horizons Forum and …, 2013 | 60 | 2013 |
| Effect of gas injection on transition in hypervelocity boundary layers JS Jewell, IA Leyva, NJ Parziale, JE Shepherd 28th International Symposium on Shock Waves: Vol 1, 735-740, 2012 | 47 | 2012 |
| Stability analysis of high-speed boundary-layer flow with gas injection AV Fedorov, V Soudakov, IA Leyva 7th AIAA Theoretical Fluid Mechanics Conference, 2498, 2014 | 45 | 2014 |
| Preliminary Results on Coaxial Jet Sprean Angles and the Effects of Variable Phase Transverse Acoustic Fields I Leyva, J Rodriguez, B Chehroudi, D Talley 46th AIAA Aerospace Sciences Meeting and Exhibit, 950, 2008 | 42 | 2008 |
| Investigation of unsteady flow field in a 2-stage PDE resonator I Leyva, V Tangirala, A Dean 41st Aerospace Sciences Meeting and Exhibit, 715, 2003 | 42 | 2003 |
| Effects of shock-tube cleanliness on hypersonic boundary layer transition at high enthalpy JS Jewell, NJ Parziale, IA Leyva, JE Shepherd AIAA journal 55 (1), 332-338, 2017 | 38 | 2017 |
| Method and apparatus for modulating airfoil lift SG Saddoughi, IA Leyva, AJ Dean, BF Robic, L Butler US Patent 6,629,674, 2003 | 38 | 2003 |
| On the impact of injection schemes on transition in hypersonic boundary layers I Leyva, J Jewell, S Laurence, H Hornung, J Shepherd 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and …, 2009 | 36 | 2009 |
| High enthalpy double-wedge experiments J Olejniczak, G Candler, M Wright, H Hornung, I Leyva Advanced Measurement and Ground Testing Conference, 2238, 1996 | 33 | 1996 |
| Turbulent spots in hypervelocity flow JS Jewell, IA Leyva, JE Shepherd Experiments in Fluids 58, 1-14, 2017 | 28 | 2017 |
| Shock detachment process on cones in hypervelocity flows IA Leyva California Institute of Technology, 1999 | 27 | 1999 |
| Two-stage pulse detonation system VE Tangirala, AJ Dean, IA Leyva US Patent 6,983,586, 2006 | 24 | 2006 |
| MEMS-based pulse detonation engine for small-scale propulsion applications K McManus, E Furlong, I Leyva AIAA, 2001 | 24 | 2001 |
