Computational Modeling of High-Speed Flows around Finned Missiles Article Swipe
In this study, flows around generic missiles were computationally modeled and analyzed using a coupled density-based solver, OpenFOAM-HiSA. The issues regarding the modeling procedures, e.g., turbulence modeling, were addressed, and analyses were conducted in subsonic, transonic, and supersonic ranges. The obtained numerical results were compared with the previously published measurements and predictions of other researchers. It was observed that the calculated drag coefficient values were in fairly good agreement with the measurements. Especially, using the SST turbulence model produced better results than using the Spalart-Allmaras model. In addition, the obtained flow pattern was qualitatively similar to the previously published calculation data. With this validated model, the flow field and the drag variation with respect to the freestream Mach number were investigated. Furthermore, the flow around a modified missile geometry was analyzed, and the results were examined comparatively. Hence, the drag reduction mechanism due to geometric modifications could be explained.
Related Topics
Concepts
Freestream
Turbulence
Drag coefficient
Drag
Mach number
Mechanics
Supersonic speed
Flow (mathematics)
Aerospace engineering
Missile
Drag divergence Mach number
Aerodynamics
Computational fluid dynamics
Physics
Wave drag
Angle of attack
Choked flow
Reduction (mathematics)
Mathematics
Field (mathematics)
Aerodynamic drag
Parasitic drag
Computer simulation
Reynolds number
Turbulence kinetic energy
Lift-to-drag ratio
Metadata
- Type
- article
- Language
- en
- Landing Page
- https://doi.org/10.37394/232013.2025.20.13
- https://doi.org/10.37394/232013.2025.20.13
- OA Status
- diamond
- References
- 17
- OpenAlex ID
- https://openalex.org/W7105680904
All OpenAlex metadata
Raw OpenAlex JSON
- OpenAlex ID
-
https://openalex.org/W7105680904Canonical identifier for this work in OpenAlex
- DOI
-
https://doi.org/10.37394/232013.2025.20.13Digital Object Identifier
- Title
-
Computational Modeling of High-Speed Flows around Finned MissilesWork title
- Type
-
articleOpenAlex work type
- Language
-
enPrimary language
- Publication year
-
2025Year of publication
- Publication date
-
2025-11-14Full publication date if available
- Authors
-
Markos CaganList of authors in order
- Landing page
-
https://doi.org/10.37394/232013.2025.20.13Publisher landing page
- PDF URL
-
https://doi.org/10.37394/232013.2025.20.13Direct link to full text PDF
- Open access
-
YesWhether a free full text is available
- OA status
-
diamondOpen access status per OpenAlex
- OA URL
-
https://doi.org/10.37394/232013.2025.20.13Direct OA link when available
- Concepts
-
Freestream, Turbulence, Drag coefficient, Drag, Mach number, Mechanics, Supersonic speed, Flow (mathematics), Aerospace engineering, Missile, Drag divergence Mach number, Aerodynamics, Computational fluid dynamics, Physics, Wave drag, Angle of attack, Choked flow, Reduction (mathematics), Mathematics, Field (mathematics), Aerodynamic drag, Parasitic drag, Computer simulation, Reynolds number, Turbulence kinetic energy, Lift-to-drag ratioTop concepts (fields/topics) attached by OpenAlex
- Cited by
-
0Total citation count in OpenAlex
- References (count)
-
17Number of works referenced by this work
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| abstract_inverted_index.mechanism | 141 |
| abstract_inverted_index.modeling, | 26 |
| abstract_inverted_index.numerical | 41 |
| abstract_inverted_index.published | 48, 98 |
| abstract_inverted_index.reduction | 140 |
| abstract_inverted_index.regarding | 20 |
| abstract_inverted_index.subsonic, | 34 |
| abstract_inverted_index.validated | 103 |
| abstract_inverted_index.variation | 111 |
| abstract_inverted_index.addressed, | 28 |
| abstract_inverted_index.calculated | 60 |
| abstract_inverted_index.explained. | 148 |
| abstract_inverted_index.freestream | 116 |
| abstract_inverted_index.previously | 47, 97 |
| abstract_inverted_index.supersonic | 37 |
| abstract_inverted_index.transonic, | 35 |
| abstract_inverted_index.turbulence | 25, 76 |
| abstract_inverted_index.Especially, | 72 |
| abstract_inverted_index.calculation | 99 |
| abstract_inverted_index.coefficient | 62 |
| abstract_inverted_index.predictions | 51 |
| abstract_inverted_index.procedures, | 23 |
| abstract_inverted_index.Furthermore, | 121 |
| abstract_inverted_index.measurements | 49 |
| abstract_inverted_index.researchers. | 54 |
| abstract_inverted_index.density-based | 15 |
| abstract_inverted_index.investigated. | 120 |
| abstract_inverted_index.measurements. | 71 |
| abstract_inverted_index.modifications | 145 |
| abstract_inverted_index.qualitatively | 93 |
| abstract_inverted_index.OpenFOAM-HiSA. | 17 |
| abstract_inverted_index.comparatively. | 136 |
| abstract_inverted_index.computationally | 8 |
| abstract_inverted_index.Spalart-Allmaras | 84 |
| cited_by_percentile_year | |
| countries_distinct_count | 1 |
| institutions_distinct_count | 1 |
| citation_normalized_percentile.value | 0.79319736 |
| citation_normalized_percentile.is_in_top_1_percent | False |
| citation_normalized_percentile.is_in_top_10_percent | False |