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A Study of Hybrid Airfoil Design Method Read chapter Read first chapter

2019 | OriginalPaper | Chapter

An Engineering Correction Method of Static Aeroelasticity and Reynolds Number Effect on Wind Tunnel Pressure Distribution

Authors : Kun Mao, Fei Xue, Feng Bai, Dongyun Zhang, Meihong Zhang

Published in: The Proceedings of the 2018 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2018)

Publisher: Springer Singapore

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Abstract

Effects of static aeroelasticity and Reynolds number on transonic pressure distribution are described. An engineering correction method of static aeroelasticity and Reynolds number effect on wind tunnel pressure distribution is constructed based on high-fidelity Fluid-Structure Interaction Simulation Method. And the fidelity of our engineering correction method has been verified with CRM tunnel pressure distribution from ETW tunnel.

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Literature
1.
Keye S, Rudnik R (2015) Validation of wing deformation simulation for the NASA CRM model using fluid-structure interaction computations. In: 53rd AIAA Aerospace Sciences Meeting, AIAA 2015
2.
Haines AB, Young AD (1994) Scale effects on aircraft and weapon aerodynamics. AGARD-AG-323
3.
Bushnell DM (2006) Scaling: wind tunnel to flight. Annu Rev Fluid Mesh 38:111–128CrossRef
4.
Fiahwe DF et al (1998) Reynolds number effects at high angles of attack. NASA TP-1998-20655
5.
Amsallem D, Farhat C, Lieu T (2007) Aeroelastic analysis of F-16 and F-18/A configurations using adapted CFD-based reduced-order models. In: The 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Honolulu, Hawaii, AIAA Paper 2007-2364, pp 23–26
6.
Burner AW, Goad WK, Massey EA et al (2008) Wing deformation measurements of the DLR-F6 transport configuration in the national transonic facility. In: 26th AIAA Applied Aerodynamics Conference, Honolulu, Hawaii, AIAA Paper 2008-6921, pp 18–21
7.
Vrchota P, Prachar A (2015) Improvement of CFD results of NASA CRM by on-line mesh deformation using modal analysis of a wing. In: 33rd AIAA Applied Aerodynamics Conference, Dallas, TX, AIAA Aviation 2015-3153
8.
Vassberg JC, DeHaan MA, Rivers MB, Wahls MS (2015) Development of a common research model using fluid-structure interaction computations, AIAA Paper 2015-0619
9.
10.
11.
Menter F, Rumsey C (1994) Assessment of two-equation turbulence models for transonic flows, AIAA 94-2343
12.
Anderson JD (2010) Fundamentals of aerodynamics. McGraw-Hill Companies, pp 207–508
Metadata
Title
An Engineering Correction Method of Static Aeroelasticity and Reynolds Number Effect on Wind Tunnel Pressure Distribution
Authors
Kun Mao
Fei Xue
Feng Bai
Dongyun Zhang
Meihong Zhang
Copyright Year
2019
Publisher
Springer Singapore
Book
The Proceedings of the 2018 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2018)

Print ISBN: 978-981-13-3304-0

Electronic ISBN: 978-981-13-3305-7

Copyright Year: 2019

DOI
https://doi.org/10.1007/978-981-13-3305-7_10

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