A NEW APPROACH FOR THE DESIGN OF AN AEROSPACE SYSTEM

Testing and evaluation program of lab. scale hybrid propulsion system

SELECTION AND PERFORMANCE OF HYBRID PROPELLANT PROPULSION SYSTEM

AIRCRAFT PROPULSION SYSTEMS : A DIESEL HYBRID ENGINE

ADVANCED PROPELLING SOLUTIONS COMPLING WITH FUTURE DEMANDS (FCS)

Preliminary Design of Heavy Duty Industrial Gas Turbine

Optimization of Gas Generator Liquid Rocket Engine using an Advanced Mass Model

Automation of Design Tool for an Axial Flow Gas Turbine Stage Used in Small Gas Turbine Engine

Modeling and Systematic Investigation of a Small-Scale Propeller Selection

DEVELOPMENT OF AN ORIGINAL PROCESS FOR THE PRELIMINARY DESIGN OF AN UAV SYSTEM BASED ON MULTIPLE MODULES