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:
Advanced Aircraft Analysis (DAR Corporation)
TORNADO
XLFR5
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