H. Naseh

Numerical and experimental investigation of vortex breaker effectiveness on the improvement in launch vehicle ballistic parameters

Mehran Mirshams, Hasan Karimi, Hasan Naseh, 2010 .

A Bayesian Networks Approach to Reliability Analysis of a Launch Vehicle Liquid Propellant Engine

H. Naseh, 2013 .

Developing a Multi-objective Multi-Disciplinary Robust Design Optimization Framework

F. Ommi, H. Naseh, M. Meibody, 2021, Scientia Iranica.

Multi-objective multidisciplinary design of Space Launch System using Holistic Concurrent Design

Mehran Mirshams, H. R. Fazeley, Hasan Naseh, 2014 .

A multi-objective, multidisciplinary design optimization methodology for the conceptual design of a spacecraft bi-propellant propulsion system

Mehran Mirshams, H. R. Fazeley, H. Naseh, 2016 .

An integrated methodology applied for reliability based multi-disciplinary design optimization in EPFE with LOX/kerosene

F. Ommi, H. Naseh, H. Alimohammadi, 2023, Reliab. Eng. Syst. Saf..