AIRCRAFT DESIGN LAB

Main Activities:

- Introductory tools concerning the aircraft preliminary design.

- Description of the different steps of an aircraft design

- Mission profile and design of the preliminary aircraft

-Preliminary analysis of wing loading and installed thrust on the basis of:

Take-off/landing analysis TOP

Airfoil and finite wing choice

Low speed polar analysis

Climb requirements.


Tools

- Classical  iterative approaches as developed by Torenbeck or Roskam to evaluate the main preliminary  characteristics of an aircraft with reference to the prescribed mission.


Software:

Coordinator L. Marino

Via Eudossiana, 18 Building A
Dip. di Ingegneria Meccanica e Aerospaziale 
tel: +39 06 44585229

For further information please contact:  luca.marino@uniroma1.it