| Preliminary design of a 2D supersonic inlet to maximize total pressure recovery H Ran, D Mavris AIAA 5th ATIO and16th Lighter-Than-Air Sys Tech. and Balloon Systems …, 2005 | 87 | 2005 |
| A comprehensive global model of broadband direct solar radiation for solar cell simulation H Ran, R Thomas, D Mavris 45th AIAA aerospace sciences meeting and exhibit, 33, 2007 | 58 | 2007 |
| Multidisciplinary design optimization of a truss braced wing aircraft with upgraded aerodynamic analyses G Seber, H Ran, T Nam, J Schetz, D Mavris 29th AIAA Applied Aerodynamics Conference, 3179, 2011 | 19 | 2011 |
| Rapid-prototyping method for modeling a circulation-control wing at low speeds H Ran, DN Mavris, M Kirby Journal of aircraft 49 (5), 1480-1484, 2012 | 11 | 2012 |
| Investigation of a health monitoring methodology for future natural laminar flow transport aircraft DN Mavris, WS Saric, H Ran, MJ Belisle, MJ Woodruff, HL Reed ICAS_2010_193, 27th International Congress of the Aeronautical Sciences, 2010 | 7 | 2010 |
| Extension of a modern lifting-line method to transonic speeds and application to multiple-lifting-surface configurations R Jacobs, H Ran, M Kirby, D Mavris 30th AIAA Applied Aerodynamics Conference, 2889, 2012 | 6 | 2012 |
| A framework for determination of the weak Pareto frontier design solutions under probabilistic constraints H Ran, D Mavris 11th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, 6960, 2006 | 5 | 2006 |
| A generic airfoil design method based on a naturally bounded PARSEC approach S Ghosh, H Ran, DN Mavris 32nd AIAA Applied Aerodynamics Conference, 2010, 2014 | 4 | 2014 |
| Advanced vehicles modeling for the next generation air transportation system (nextgen vehicle integration nra) M Kirby, H Ran, S Dufresne, W Sung, D Mavris, G Burdette 9th AIAA Aviation Technology, Integration, and Operations Conference (ATIO …, 2009 | 4 | 2009 |
| A framework for the determination of weak Pareto frontier solutions under probabilistic constraints H Ran Aerospace Engineering, Georgia Institute of Technology, 2007 | 4 | 2007 |
| Time Marching Aeroelasticity Modeling and Validation Study for Plates with and without Hole H Ran, T Wray, S Yang, HQ Yang AIAA Scitech 2020 Forum, 2289, 2020 | 3 | 2020 |
| A mean value based sizing and simulation model of a hydrogen fueled spark-ignition internal combustion engine H Ran, R Thomas, DN Mavris SAE Technical Paper, 2007 | 2 | 2007 |
| Determination of the Terminal Shock in Two-Dimensional Supersonic Inlets H Ran, R Deany, DN Mavris Journal of aircraft 49 (5), 1532-1535, 2012 | 1 | 2012 |
