Comparison of Optimization Strategies for High-Lift Design-Reference-Cited by-同舟云学术

Comparison of Optimization Strategies for High-Lift Design

Published:2017-03 Issue:2 Volume:54 Page:642-658
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Iannelli Pierluigi¹,Moens Frédéric²,Minervino Mauro³,Ponza Rita⁴,Benini Ernesto⁴

Affiliation:

1. Centro Italiano Ricerche Aerospaziali, 81043 Capua, Italy

2. ONERA–The French Aerospace Lab, 92190 Meudon, France

3. Piaggio Aero Industries, 17038 Villanova d’Albenga, Italy

4. University of Padua, 35131 Padua, Italy

Funder

European Commission

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C033648

Reference25 articles.

1. The aerodynamic design of multi-element high-lift systems for transport airplanes

2. RudolphP. K. C. “High Lift Systems on Commercial Subsonic Airliners,” NASA CR 4746, Sept. 1996.

3. MeredithP. T. “Viscous Phenomena Affecting High-Lift Systems and Suggestions for Future CFD Development,” AGARD, CP 315, Neuilly sur Seine, France, 1993, pp. 19-1–19-8.

4. Transport Aircraft Three-Dimensional High-Lift Wing Numerical Transition Prediction

5. High-Lift Aerodynamics

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