High-Lift Aerodynamics Design for Large Civil Aircraft in Fudan University

Gang Sun; Kang Le Xu; Ying Chun Chen

doi:10.4028/www.scientific.net/AMM.52-54.1382

Paper Titles

Reliability Analysis of Uncertain Input Variables for Cracked Structures
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Study on Fillet Stresses Distribution of Crankshaft of High-Duty Diesel Engine
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A CAE Approach for Pretest Analysis of Vehicle Body Frame Vibration Test
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Electromechanical Coupling Modeling in Permanent Magnet AC Servo-Driven Precision Gear Transmission System
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High-Lift Aerodynamics Design for Large Civil Aircraft in Fudan University
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Noise Prediction for Multi-Element Airfoil Based on FW-H Equation
p.1388

Stress and Probabilistic Study of the Lumbar Vertebra under Compression Loading
p.1394

Simulations of Bearing Capacity of Foundation on Unsaturated Granular Soils
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CCT Curves and Dynamic Phase Diagrams of Steel
p.1406

HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 52-54High-Lift Aerodynamics Design for Large Civil...

High-Lift Aerodynamics Design for Large Civil Aircraft in Fudan University

Abstract:

Part of work on CFD simulations by the high-lift system design team in Fudan university for large civil aircraft is presented. The research on CFD simulation of the high-lift systems and some concepts and experience in three-dimensional geometry modeling are also presented, which are done on the self-developed platform of high-lift device aerodynamic calculation software and programs. For which, the design efficiency is substantially improved.

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Periodical:

Applied Mechanics and Materials (Volumes 52-54)

Pages:

1382-1387

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.52-54.1382

Citation:

Cite this paper

Online since:

March 2011

Authors:

Gang Sun, Kang Le Xu, Ying Chun Chen

Keywords:

Aerodynamics Design, High-Lift System, Large Civil Aircraft

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