A comparative study of turbulence models for predicting the aerodynamic drag of a spin-stabilized projectile Article Swipe
Introduction/purpose: In this research, the influence of different turbulence models on the aerodynamic drag prediction of a generic spin-stabilized projectile was analyzed. The turbulence models chosen for investigation were one-equation Spalart-Allmaras, two-equation models Standard k-e, Realizable k-e, Standard k-o and SST k-o. The special sniper projectile M118 was selected for the study. Methods: The flows around the projectile were numerically simulated using RANS equations intergrated into ANSYS Fluent software with different turbulence models. The numerical simulation was carried out at various Mach numbers to study the effect of turbulence models on the projectile aerodynamic drag prediction. The computational results were compared to the available experimental data to evaluate the ability of the turbulence models. Results: The research results have shown that the turbulence models significantly affect the numerical simulation results. The Spalart-Allmaras turbulence model performs better than other models in the subsonic flow regime. The Standard k-e, Realizable k-e and SST k-o models perform better than other models in the supersonic flow regime. Conclusion: Computational Fluid Dynamics is a powerful tool to analyze the aerodynamics of flying bodies. By appropriately selecting turbulence models, the flow around flying bodies can be accurately investigated. In the case of generic ogive-cylinder-boattail projectiles, on the one hand, the Spalart-Allmaras model is suitable for subsonic flow, and the Standard k-e, Realizable k-e and SST k-o models are recommended for the supersonic flight regime, on the other hand.
Related Topics
Concepts
Drag
Projectile
Aerodynamics
Turbulence
Physics
Mechanics
Aerodynamic drag
Range of a projectile
Spin (aerodynamics)
Zero-lift drag coefficient
Aerospace engineering
Drag coefficient
Classical mechanics
Lift-induced drag
Engineering
Quantum mechanics
Metadata
- Type
- article
- Language
- en
- Landing Page
- https://doi.org/10.5937/vojtehg73-54634
- OA Status
- diamond
- References
- 23
- Related Works
- 10
- OpenAlex ID
- https://openalex.org/W4407219287
All OpenAlex metadata
Raw OpenAlex JSON
- OpenAlex ID
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https://openalex.org/W4407219287Canonical identifier for this work in OpenAlex
- DOI
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https://doi.org/10.5937/vojtehg73-54634Digital Object Identifier
- Title
-
A comparative study of turbulence models for predicting the aerodynamic drag of a spin-stabilized projectileWork title
- Type
-
articleOpenAlex work type
- Language
-
enPrimary language
- Publication year
-
2025Year of publication
- Publication date
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2025-01-01Full publication date if available
- Authors
-
Nguyễn Quang TuấnList of authors in order
- Landing page
-
https://doi.org/10.5937/vojtehg73-54634Publisher landing page
- Open access
-
YesWhether a free full text is available
- OA status
-
diamondOpen access status per OpenAlex
- OA URL
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https://doi.org/10.5937/vojtehg73-54634Direct OA link when available
- Concepts
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Drag, Projectile, Aerodynamics, Turbulence, Physics, Mechanics, Aerodynamic drag, Range of a projectile, Spin (aerodynamics), Zero-lift drag coefficient, Aerospace engineering, Drag coefficient, Classical mechanics, Lift-induced drag, Engineering, Quantum mechanicsTop concepts (fields/topics) attached by OpenAlex
- Cited by
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0Total citation count in OpenAlex
- References (count)
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23Number of works referenced by this work
- Related works (count)
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10Other works algorithmically related by OpenAlex
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| abstract_inverted_index.results | 98, 117 |
| abstract_inverted_index.special | 43 |
| abstract_inverted_index.various | 80 |
| abstract_inverted_index.Dynamics | 166 |
| abstract_inverted_index.Methods: | 52 |
| abstract_inverted_index.Results: | 114 |
| abstract_inverted_index.Standard | 33, 37, 145, 213 |
| abstract_inverted_index.compared | 100 |
| abstract_inverted_index.evaluate | 107 |
| abstract_inverted_index.performs | 134 |
| abstract_inverted_index.powerful | 169 |
| abstract_inverted_index.research | 116 |
| abstract_inverted_index.results. | 129 |
| abstract_inverted_index.selected | 48 |
| abstract_inverted_index.software | 68 |
| abstract_inverted_index.subsonic | 141, 209 |
| abstract_inverted_index.suitable | 207 |
| abstract_inverted_index.analyzed. | 21 |
| abstract_inverted_index.available | 103 |
| abstract_inverted_index.different | 7, 70 |
| abstract_inverted_index.equations | 63 |
| abstract_inverted_index.influence | 5 |
| abstract_inverted_index.numerical | 74, 127 |
| abstract_inverted_index.research, | 3 |
| abstract_inverted_index.selecting | 180 |
| abstract_inverted_index.simulated | 60 |
| abstract_inverted_index.Realizable | 35, 147, 215 |
| abstract_inverted_index.accurately | 190 |
| abstract_inverted_index.prediction | 14 |
| abstract_inverted_index.projectile | 19, 45, 57, 92 |
| abstract_inverted_index.simulation | 75, 128 |
| abstract_inverted_index.supersonic | 160, 225 |
| abstract_inverted_index.turbulence | 8, 23, 71, 88, 112, 122, 132, 181 |
| abstract_inverted_index.Conclusion: | 163 |
| abstract_inverted_index.aerodynamic | 12, 93 |
| abstract_inverted_index.intergrated | 64 |
| abstract_inverted_index.numerically | 59 |
| abstract_inverted_index.prediction. | 95 |
| abstract_inverted_index.recommended | 222 |
| abstract_inverted_index.aerodynamics | 174 |
| abstract_inverted_index.experimental | 104 |
| abstract_inverted_index.one-equation | 29 |
| abstract_inverted_index.projectiles, | 198 |
| abstract_inverted_index.two-equation | 31 |
| abstract_inverted_index.Computational | 164 |
| abstract_inverted_index.appropriately | 179 |
| abstract_inverted_index.computational | 97 |
| abstract_inverted_index.investigated. | 191 |
| abstract_inverted_index.investigation | 27 |
| abstract_inverted_index.significantly | 124 |
| abstract_inverted_index.spin-stabilized | 18 |
| abstract_inverted_index.Spalart-Allmaras | 131, 204 |
| abstract_inverted_index.Spalart-Allmaras, | 30 |
| abstract_inverted_index.Introduction/purpose: | 0 |
| abstract_inverted_index.ogive-cylinder-boattail | 197 |
| cited_by_percentile_year | |
| corresponding_author_ids | https://openalex.org/A5015221972 |
| countries_distinct_count | 0 |
| institutions_distinct_count | 1 |
| citation_normalized_percentile.value | 0.03938057 |
| citation_normalized_percentile.is_in_top_1_percent | False |
| citation_normalized_percentile.is_in_top_10_percent | False |