Philippe Schultz

Design & costing of interconnect systems for high end applications (aeronautics, aerospace, defense, research, nuclear, medical). Management of development and industrialisation phases.

Preliminary Intercooler Weight Estimation in a Reeverse-Flow-Core Turbofan Concept Creation of a heat-exchanger design tool in Matlab. Test of different configurations in the context of the LEMCOTEC Project. Required time management, programming skills, thermal and aerodynamics engineering skills, Coordination with engine performance study project,

The Engine Systems Symposium is an event organised by students of the Thermal Power MSc. Class of Cranfield University. It is held twice a year and features lectures made by the students and some special guests such as teachers. http://www.essymposium.co.uk/index.html Roles : Co-Leader of Marketing Team Team Management Design of an advertising Brochure Collection of funds for the organisation of the symposium

Creation of wiring diagrams of the A350XWB’s cabin Full-Scale Mock-Up (5000 connections regrouped in 200 harnesses). Required searching for information through many different documents.

Preliminary Design of a Fighter Aircraft Management of a 4 students team 3D Design on CATIA; Estimation of Weight, Balancing of the Aircraft, Estimation of Aerodynamics Characteristics and Estimation of Aircraft Performance on Excel. Very challenging project, required management skills and creativity.

IPS'Action is a Student Association Organising Lectures on Aeronautics-Related Topics at IPSA. Missions: - Design a new Logo for the Association - Invite Students to Lectures Organised by the Association - Creation of Teasing Posters - Help with Preparation and Welcome of the Lecturers

In the military clients returned spare parts storage facility. Activity: taking delivery and shipping returned or repaired spare parts (ca. 50 parts a day), management of the stock.

Thesis : Preliminary Intercooler Weight Estimation for a Reverse Flow Core Engine Concept Topics studied :Gas Turbine Performance, Turbomachinery Design, Combustion, Blade Cooling, Material Selection

Year-End Project : Preliminary Design of a Jet Fighter Gas Turbines, Flight Mechanics, Fluid Dynamics, CAD, Thermal Transfert, Structure Mechanics, FEM, Avionics, Piston Engines,