| Numerical and experimental investigation of vortex breaker effectiveness on the improvement in launch vehicle ballistic parameters MN Mahyari, H Karimi, H Naseh, M Mirshams Journal of Mechanical Science and Technology 24, 1997-2006, 2010 | 30 | 2010 |
| A multi-objective, multidisciplinary design optimization methodology for the conceptual design of a spacecraft bi-propellant propulsion system HR Fazeley, H Taei, H Naseh, M Mirshams Structural and Multidisciplinary Optimization 53, 145-160, 2016 | 26 | 2016 |
| Multi-objective multidisciplinary design of space launch system using holistic concurrent design M Mirshams, H Naseh, HR Fazeley Aerospace Science and Technology 33 (1), 40-54, 2014 | 23 | 2014 |
| Multi-Stage Liquid Propellant Launch Vehicle Conceptual Design (LVCD) Software, Based on Multi-Parameter Optimization Idea M Mirshams, H Karimi, H Naseh Journal of Space Science and Technology 1 (2), 2008 | 17 | 2008 |
| Design of Physical Configuration of a 10N Monopropellant Hydrazine Thruster H Karimaei, MR Salimi, H Naseh, E Jokari Space Science and Technology 12 (1), 13-22, 2019 | 15 | 2019 |
| Multi-Stage Liquid Propellant Launch Vehicle Conceptual Design, Based on Combinatorial Optimization of Major Design Parameters M Mirshams, H Karimi, H Naseh Space Science and Technology 1 (1), 21-36, 2008 | 14 | 2008 |
| Progressive Latin Hypercube sampling-based robust design optimisation (PLHS-RDO) MNP Meibody, H Naseh, F Ommi Australian Journal of Mechanical Engineering 20 (3), 660-667, 2022 | 12 | 2022 |
| Liquid propellant engine conceptual design by using a fuzzy-multi-objective genetic algorithm (MOGA) optimization method M Mirshams, H Naseh, H Taei, HR Fazeley Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2014 | 12 | 2014 |
| A bayesian networks approach to reliability analysis of a launch vehicle liquid propellant engine AM Akhlaghi, H Naseh, M MirShams, S Irani Journal of Aerospace Science and Technology (JAST) 8 (2), 107-117, 2011 | 10 | 2011 |
| A novel framework for liquid propellant engine’s cooling system design by sensitivity analysis based on RSM and multi-objective optimization using PSO HR Alimohammadi, H Naseh, F Ommi Advances in Space Research 67 (5), 1682-1700, 2021 | 9 | 2021 |
| A kriging based multi objective gray wolf optimization for hydrazine catalyst bed M Meibody, H Naseh, F Ommi Engineering Solid Mechanics 7 (3), 179-192, 2019 | 9 | 2019 |
| A Bayesian networks approach to reliability analysis of a space vehicle separation sub-system H Naseh, M Mirshams 2013 6th International Conference on Recent Advances in Space Technologies …, 2013 | 8 | 2013 |
| An Analytic Hierarchy Process based reliability allocation method (ARAM) H Naseh, AM Akhlaghi, M Mirshams, S Irani International Symposium on the Analytic Hierarchy Process. Sorrento, Italy, 2011 | 7 | 2011 |
| Developing a multi-objective multi-disciplinary robust design optimization framework MNP Meibody, H Naseh, F Ommi Scientia Iranica 28 (4), 2150-2163, 2021 | 6 | 2021 |
| Expendable launch vehicle reliability modeling by using stochastic method AM Akhlaghi, M Mirshams, H Naseh Proceedings of The 1st Conference of Aerospace System Reliability, 24-26, 2009 | 6 | 2009 |
| Propellant management device (PMD) design optimization of hydrazine fuel tank H Naseh, A Alipour Modares Mechanical Engineering 17 (7), 152-160, 2017 | 5 | 2017 |
| A new synthetic metamodel methodology for liquid‐propellant engine's cooling system optimization HR Alimohammadi, H Naseh, F Ommi Heat Transfer 50 (1), 907-941, 2021 | 4 | 2021 |
| Numerical-parametrical analysis on the hydrogen peroxide catalyst bed for space monopropellant thruster applications H Naseh, AH Hosseini, F OMMI APPLIED RESEARCH IN CHEMICAL POLYMER ENGINEERING 1 (22), 15-24, 2018 | 4 | 2018 |
| Propellant Management Device (PMD) System Design Methodology in Zero Gravity Condition A Alipour Modares Mechanical Engineering 18 (2), 84-94, 2018 | 3 | 2018 |
| Adaptive surrogate modelling algorithm for meta-model-based design optimisation MNP Meibody, H Naseh, F Ommi International Journal of Industrial and Systems Engineering 39 (3), 394-410, 2021 | 2 | 2021 |
