Numerical Investigation of Aerodynamic Hysteresis for Transonic Flow Over a Supercritical Airfoil Article Swipe
Mahbubur Rahman
,
A. B. M. Toufique Hasan
,
Md. Itmam Labib
·
YOU?
·
· 2015
· Open Access
·
· DOI: https://doi.org/10.1016/j.proeng.2015.05.021
YOU?
·
· 2015
· Open Access
·
· DOI: https://doi.org/10.1016/j.proeng.2015.05.021
A computational study is performed to investigate transonic flow over supercritical airfoil RAE 2822. In this study, Reynolds averaged Navier Stokes equations (RANS) with Spalart-Allmaras turbulence model have been applied. Results have been well validated with available experimental data. Results showed that the coefficients of lift and drag are not single valued functions of angle of attack, rather they assume multiple values regarding the increasing or decreasing trend of angle of attack. Depending on the increasing and decreasing processes, the lift and drag coefficients differ at same angle of attack. Consequently a hysteresis loop is formed. This hysteresis is closely related to the laminar boundary layer separation and transitions on airfoil. The flow exhibits noticeable ability to remember its past history. This memory of the flow is responsible for the hysteresis.
Related Topics
Concepts
Airfoil
Angle of attack
Mechanics
Transonic
Reynolds-averaged Navier–Stokes equations
Turbulence
Laminar flow
Hysteresis
Drag
Drag divergence Mach number
Lift (data mining)
Flow separation
Materials science
Boundary layer
Lift coefficient
Lift-to-drag ratio
Pitching moment
Aerodynamics
Reynolds number
Physics
Computer science
Data mining
Quantum mechanics
Metadata
- Type
- article
- Language
- en
- Landing Page
- https://doi.org/10.1016/j.proeng.2015.05.021
- OA Status
- diamond
- Cited By
- 1
- References
- 9
- Related Works
- 10
- OpenAlex ID
- https://openalex.org/W645839568
All OpenAlex metadata
Raw OpenAlex JSON
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https://openalex.org/W645839568Canonical identifier for this work in OpenAlex
- DOI
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https://doi.org/10.1016/j.proeng.2015.05.021Digital Object Identifier
- Title
-
Numerical Investigation of Aerodynamic Hysteresis for Transonic Flow Over a Supercritical AirfoilWork title
- Type
-
articleOpenAlex work type
- Language
-
enPrimary language
- Publication year
-
2015Year of publication
- Publication date
-
2015-01-01Full publication date if available
- Authors
-
Mahbubur Rahman, A. B. M. Toufique Hasan, Md. Itmam LabibList of authors in order
- Landing page
-
https://doi.org/10.1016/j.proeng.2015.05.021Publisher landing page
- Open access
-
YesWhether a free full text is available
- OA status
-
diamondOpen access status per OpenAlex
- OA URL
-
https://doi.org/10.1016/j.proeng.2015.05.021Direct OA link when available
- Concepts
-
Airfoil, Angle of attack, Mechanics, Transonic, Reynolds-averaged Navier–Stokes equations, Turbulence, Laminar flow, Hysteresis, Drag, Drag divergence Mach number, Lift (data mining), Flow separation, Materials science, Boundary layer, Lift coefficient, Lift-to-drag ratio, Pitching moment, Aerodynamics, Reynolds number, Physics, Computer science, Data mining, Quantum mechanicsTop concepts (fields/topics) attached by OpenAlex
- Cited by
-
1Total citation count in OpenAlex
- Citations by year (recent)
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2020: 1Per-year citation counts (last 5 years)
- References (count)
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9Number of works referenced by this work
- Related works (count)
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10Other works algorithmically related by OpenAlex
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| publication_year | 2015 |
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