INVESTIGATION OF THE EFFECT OF TAPER STACKING LOCATION ON AERODYNAMIC LOADS FOR ONERA M6 WING AT A FIXED ANGLE OF ATTACK
The effect of taper stacking location for ONERA M6 wing is analyzed in terms of the lift, drag and lift-to-drag ratio. The stacking location is defined as the non-dimensional distance from the sectional leading edge to the taper axis. The non-dimensionalization is based on the sectional chord length...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
Turkish Air Force Academy
2019-01-01
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| Series: | Havacılık ve Uzay Teknolojileri Dergisi |
| Subjects: | |
| Online Access: | http://www.jast.hho.edu.tr/JAST/index.php/JAST/article/view/330/284 |
| _version_ | 1797915034557349888 |
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| author | Mustafa Kaya Munir Elfarra |
| author_facet | Mustafa Kaya Munir Elfarra |
| author_sort | Mustafa Kaya |
| collection | DOAJ |
| description | The effect of taper stacking location for ONERA M6 wing is analyzed in terms of the lift, drag and lift-to-drag ratio. The stacking location is defined as the non-dimensional distance from the sectional leading edge to the taper axis. The non-dimensionalization is based on the sectional chord length. Different wing shapes are generated by linearly or parabolically varying the stacking location along the span. Various wing cases are investigated under the same angle of attack. The steady-state turbulent flowfields are computed by solving the Reynolds Averaged Navier-Stokes equations. The Spalart-Allmaras turbulence model with the extended wall function is used to calculate the eddy viscosity. It is observed that there exist some cases in which the values of lift, drag and lift-to-drag ratio change significantly. Moreover, the spanwise variation of the stacking location has a pronounced effect on the formation and the characteristics of the shock wave. |
| first_indexed | 2024-04-10T12:35:18Z |
| format | Article |
| id | doaj.art-72f305e6d19c4a63b803c45d7bf585b5 |
| institution | Directory Open Access Journal |
| issn | 1304-0448 1304-0448 |
| language | English |
| last_indexed | 2024-04-10T12:35:18Z |
| publishDate | 2019-01-01 |
| publisher | Turkish Air Force Academy |
| record_format | Article |
| series | Havacılık ve Uzay Teknolojileri Dergisi |
| spelling | doaj.art-72f305e6d19c4a63b803c45d7bf585b52023-02-15T16:14:41ZengTurkish Air Force AcademyHavacılık ve Uzay Teknolojileri Dergisi1304-04481304-04482019-01-011215163INVESTIGATION OF THE EFFECT OF TAPER STACKING LOCATION ON AERODYNAMIC LOADS FOR ONERA M6 WING AT A FIXED ANGLE OF ATTACKMustafa Kaya0Munir Elfarra1Yildirim Beyazit UniversityAnkara Yildirim Beyazit UniversityThe effect of taper stacking location for ONERA M6 wing is analyzed in terms of the lift, drag and lift-to-drag ratio. The stacking location is defined as the non-dimensional distance from the sectional leading edge to the taper axis. The non-dimensionalization is based on the sectional chord length. Different wing shapes are generated by linearly or parabolically varying the stacking location along the span. Various wing cases are investigated under the same angle of attack. The steady-state turbulent flowfields are computed by solving the Reynolds Averaged Navier-Stokes equations. The Spalart-Allmaras turbulence model with the extended wall function is used to calculate the eddy viscosity. It is observed that there exist some cases in which the values of lift, drag and lift-to-drag ratio change significantly. Moreover, the spanwise variation of the stacking location has a pronounced effect on the formation and the characteristics of the shock wave.http://www.jast.hho.edu.tr/JAST/index.php/JAST/article/view/330/284CFDWing ShapeTaper StackingLift-to-Drag RatioShock Structure |
| spellingShingle | Mustafa Kaya Munir Elfarra INVESTIGATION OF THE EFFECT OF TAPER STACKING LOCATION ON AERODYNAMIC LOADS FOR ONERA M6 WING AT A FIXED ANGLE OF ATTACK Havacılık ve Uzay Teknolojileri Dergisi CFD Wing Shape Taper Stacking Lift-to-Drag Ratio Shock Structure |
| title | INVESTIGATION OF THE EFFECT OF TAPER STACKING LOCATION ON AERODYNAMIC LOADS FOR ONERA M6 WING AT A FIXED ANGLE OF ATTACK |
| title_full | INVESTIGATION OF THE EFFECT OF TAPER STACKING LOCATION ON AERODYNAMIC LOADS FOR ONERA M6 WING AT A FIXED ANGLE OF ATTACK |
| title_fullStr | INVESTIGATION OF THE EFFECT OF TAPER STACKING LOCATION ON AERODYNAMIC LOADS FOR ONERA M6 WING AT A FIXED ANGLE OF ATTACK |
| title_full_unstemmed | INVESTIGATION OF THE EFFECT OF TAPER STACKING LOCATION ON AERODYNAMIC LOADS FOR ONERA M6 WING AT A FIXED ANGLE OF ATTACK |
| title_short | INVESTIGATION OF THE EFFECT OF TAPER STACKING LOCATION ON AERODYNAMIC LOADS FOR ONERA M6 WING AT A FIXED ANGLE OF ATTACK |
| title_sort | investigation of the effect of taper stacking location on aerodynamic loads for onera m6 wing at a fixed angle of attack |
| topic | CFD Wing Shape Taper Stacking Lift-to-Drag Ratio Shock Structure |
| url | http://www.jast.hho.edu.tr/JAST/index.php/JAST/article/view/330/284 |
| work_keys_str_mv | AT mustafakaya investigationoftheeffectoftaperstackinglocationonaerodynamicloadsforoneram6wingatafixedangleofattack AT munirelfarra investigationoftheeffectoftaperstackinglocationonaerodynamicloadsforoneram6wingatafixedangleofattack |