A distributed toolbox for multidisciplinary preliminary aircraft design

2011 ◽  
Vol 2 (1-4) ◽  
pp. 57-68 ◽  
Author(s):  
Carsten M. Liersch ◽  
Martin Hepperle
Keyword(s):  
Aircraft Design ◽  
Preliminary Aircraft Design

Method for Estimation of Electrical Wiring Interconnection Systems in Preliminary Aircraft Design

2019 ◽  
Vol 56 (3) ◽  
pp. 1259-1263 ◽  
Author(s):  
Francesca Tomasella ◽  
Marco Fioriti ◽  
Luca Boggero ◽  
Sabrina Corpino
Keyword(s):  
Aircraft Design ◽  
Preliminary Aircraft Design ◽  
Electrical Wiring

Genetic Optimization Applied in Conceptual and Preliminary Aircraft Design

2008 ◽  
Author(s):  
R. Oliveira ◽  
A. Cortellazzi ◽  
P. Nakamura ◽  
R. Neto ◽  
E. Belo ◽  
...  
Keyword(s):  
Aircraft Design ◽  
Genetic Optimization ◽  
Preliminary Aircraft Design

EPISTLE: High lift system design for low-noise applied to a supersonic aircraft

2006 ◽  
Vol 110 (1107) ◽  
pp. 327-331 ◽  
Author(s):  
U. Herrmann
Keyword(s):  
System Design ◽  
Aircraft Design ◽  
Reynolds Numbers ◽  
Low Noise ◽  
High Lift ◽  
New Approach ◽  
Low Speed ◽  
Supersonic Aircraft ◽  
Preliminary Aircraft Design ◽  
High Reynolds

Abstract A new approach for low-drag high-lift system design based on the application of viscous flow solvers was developed in the EC research project EPISTLE. Two high-lift systems for a supersonic commercial transport aircraft (SCT) wing were designed, manufactured and wind-tunnel tested. The predicted large drag reductions were fully confirmed by tests at high Reynolds numbers. These drag reductions significantly reduce the low-speed noise of future SCT configurations. This was estimated by preliminary aircraft design tools. Low-speed noise reduction by aerodynamic means is obtained, as effective high-lift systems enable these aircraft to climb faster.

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