Investigation of Reynolds Number Effects on Aerodynamic Characteristics of a Transport Aircraft
The scale difference between the real flight vehicle and the experimental model results in the Reynolds number effect, which makes it unreliable to predict the aerodynamic characteristics of flight vehicles by wind tunnel testing. To understand the mechanism of Reynolds number effects on the aerodyn...
| Main Authors: | , , , |
|---|---|
| Formato: | Artigo |
| Idioma: | English |
| Publicado em: |
MDPI AG
2021-07-01
|
| Colecção: | Aerospace |
| Assuntos: | |
| Acesso em linha: | https://www.mdpi.com/2226-4310/8/7/177 |
| _version_ | 1827688192691666944 |
|---|---|
| author | Yuanjing Wang Dawei Liu Xin Xu Guoshuai Li |
| author_facet | Yuanjing Wang Dawei Liu Xin Xu Guoshuai Li |
| author_sort | Yuanjing Wang |
| collection | DOAJ |
| description | The scale difference between the real flight vehicle and the experimental model results in the Reynolds number effect, which makes it unreliable to predict the aerodynamic characteristics of flight vehicles by wind tunnel testing. To understand the mechanism of Reynolds number effects on the aerodynamic characteristics of the supercritical wing that is commonly used in transport aircraft in more detail, surface pressure wind tunnel tests of a transport aircraft reference model with a wing-body configuration were conducted in the European Transonic Windtunnel (ETW) at different Reynolds numbers. There are 495 pressure taps in total equipped on the surface of the test model with the Mach numbers ranging from 0.6 to 0.86 and Reynolds number varying from 3.3 × 10<sup>6</sup> to 35 × 10<sup>6</sup>. In addition, an in-house developed CFD tool that has been validated by extensive experimental data was used to correct the wing deformation effect of the test model and achieve detailed flow structures. The results show that the Reynolds number has a significant impact on the boundary layer displacement thickness, surface pressure distribution, shock wave position, and overall aerodynamic force coefficients of the transport aircraft in the presence of shock wave and the induced boundary layer separation. The wind tunnel data combined with flow fields achieved from CFD show that the essence of the Reynolds number effect on the aerodynamic characteristics of transport aircraft is the difference of boundary layer development, shock wave/boundary layer interaction, and induced flow separation at different Reynolds numbers. |
| first_indexed | 2024-03-10T09:49:27Z |
| format | Article |
| id | doaj.art-ff4102daac324e72913564c69b5ed8cc |
| institution | Directory Open Access Journal |
| issn | 2226-4310 |
| language | English |
| last_indexed | 2024-03-10T09:49:27Z |
| publishDate | 2021-07-01 |
| publisher | MDPI AG |
| record_format | Article |
| series | Aerospace |
| spelling | doaj.art-ff4102daac324e72913564c69b5ed8cc2023-11-22T02:56:09ZengMDPI AGAerospace2226-43102021-07-018717710.3390/aerospace8070177Investigation of Reynolds Number Effects on Aerodynamic Characteristics of a Transport AircraftYuanjing Wang0Dawei Liu1Xin Xu2Guoshuai Li3State Key Lab of Aerodynamics, China Aerodynamics Research and Development Center, Mianyang 621000, ChinaState Key Lab of Aerodynamics, China Aerodynamics Research and Development Center, Mianyang 621000, ChinaState Key Lab of Aerodynamics, China Aerodynamics Research and Development Center, Mianyang 621000, ChinaState Key Lab of Aerodynamics, China Aerodynamics Research and Development Center, Mianyang 621000, ChinaThe scale difference between the real flight vehicle and the experimental model results in the Reynolds number effect, which makes it unreliable to predict the aerodynamic characteristics of flight vehicles by wind tunnel testing. To understand the mechanism of Reynolds number effects on the aerodynamic characteristics of the supercritical wing that is commonly used in transport aircraft in more detail, surface pressure wind tunnel tests of a transport aircraft reference model with a wing-body configuration were conducted in the European Transonic Windtunnel (ETW) at different Reynolds numbers. There are 495 pressure taps in total equipped on the surface of the test model with the Mach numbers ranging from 0.6 to 0.86 and Reynolds number varying from 3.3 × 10<sup>6</sup> to 35 × 10<sup>6</sup>. In addition, an in-house developed CFD tool that has been validated by extensive experimental data was used to correct the wing deformation effect of the test model and achieve detailed flow structures. The results show that the Reynolds number has a significant impact on the boundary layer displacement thickness, surface pressure distribution, shock wave position, and overall aerodynamic force coefficients of the transport aircraft in the presence of shock wave and the induced boundary layer separation. The wind tunnel data combined with flow fields achieved from CFD show that the essence of the Reynolds number effect on the aerodynamic characteristics of transport aircraft is the difference of boundary layer development, shock wave/boundary layer interaction, and induced flow separation at different Reynolds numbers.https://www.mdpi.com/2226-4310/8/7/177transport aircraftaerodynamic characteristicsReynolds number effects |
| spellingShingle | Yuanjing Wang Dawei Liu Xin Xu Guoshuai Li Investigation of Reynolds Number Effects on Aerodynamic Characteristics of a Transport Aircraft Aerospace transport aircraft aerodynamic characteristics Reynolds number effects |
| title | Investigation of Reynolds Number Effects on Aerodynamic Characteristics of a Transport Aircraft |
| title_full | Investigation of Reynolds Number Effects on Aerodynamic Characteristics of a Transport Aircraft |
| title_fullStr | Investigation of Reynolds Number Effects on Aerodynamic Characteristics of a Transport Aircraft |
| title_full_unstemmed | Investigation of Reynolds Number Effects on Aerodynamic Characteristics of a Transport Aircraft |
| title_short | Investigation of Reynolds Number Effects on Aerodynamic Characteristics of a Transport Aircraft |
| title_sort | investigation of reynolds number effects on aerodynamic characteristics of a transport aircraft |
| topic | transport aircraft aerodynamic characteristics Reynolds number effects |
| url | https://www.mdpi.com/2226-4310/8/7/177 |
| work_keys_str_mv | AT yuanjingwang investigationofreynoldsnumbereffectsonaerodynamiccharacteristicsofatransportaircraft AT daweiliu investigationofreynoldsnumbereffectsonaerodynamiccharacteristicsofatransportaircraft AT xinxu investigationofreynoldsnumbereffectsonaerodynamiccharacteristicsofatransportaircraft AT guoshuaili investigationofreynoldsnumbereffectsonaerodynamiccharacteristicsofatransportaircraft |