Numerical study of the aerodynamic characteristics of high-lift droop nose with the deflection of fowler flap and spoiler
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference18 articles.
1. P.T. Meredith, Viscous phenomena affecting high-lift systems and suggestions for future CFD development, AGARD-CP-315, 1993.
2. The aerodynamic design of multi-element high-lift systems for transport airplanes;van Dam;Prog. Aerosp. Sci.,2002
3. Aerodynamic design of the high-lift-wing for a megaliner aircraft;Reckzeh;Aerosp. Sci. Technol.,2003
4. Model and full scale high-lift wing wind tunnel experiments dedicated to airframe noise reduction;Dobrzynski;Aerosp. Sci. Technol.,2001
5. Design of a high-lift system with droop nose device;Jirasek;J. Aircr.,2009
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