CFD Analysis of Aircraft Curved C-D Nozzle: Technical Note Article Swipe
S. Sivaganesan
,
F. Ferdaus
,
C. Dhanasekaran
,
G. Sathishkumar
,
S. Sivabalan
·
YOU?
·
· 2019
· Open Access
·
· DOI: https://doi.org/10.4273/ijvss.11.3.07
YOU?
·
· 2019
· Open Access
·
· DOI: https://doi.org/10.4273/ijvss.11.3.07
A nozzle for the aircraft can be designed by considering the exit Mach number. In order to get a premeditated Mach number, we need to convert pressure energy into kinetic energy by using a nozzle. Convergent nozzles are utilized for subsonic flows while Convergent-Divergent (C-D) nozzle is utilized for supersonic flows. Curved nozzle flow is accelerated from low subsonic to sonic velocity at the throat and further expanded to supersonic velocities at the exit, in a C-D nozzle. This paper details the relevancies on designing a curved nozzle to attain super-sonic flow and maximizing the optimal thrust and devoid of flow separation due to shock waves. The navigation of the flow must be parallel to the axis of the nozzle for achieving extreme thrust and proficiency. Based on the fundamental gas dynamic equations, this study aims to develop a theoretical approach for the calculation of the flow properties along the axis of the C-D Nozzle. The flow conditions were selected in consideration of the pressure, temperature and gases accessible at the exit of the combustion chamber.
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- Type
- article
- Language
- en
- Landing Page
- https://doi.org/10.4273/ijvss.11.3.07
- OA Status
- hybrid
- Related Works
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- OpenAlex ID
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All OpenAlex metadata
Raw OpenAlex JSON
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https://openalex.org/W2993516543Canonical identifier for this work in OpenAlex
- DOI
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https://doi.org/10.4273/ijvss.11.3.07Digital Object Identifier
- Title
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CFD Analysis of Aircraft Curved C-D Nozzle: Technical NoteWork title
- Type
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articleOpenAlex work type
- Language
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enPrimary language
- Publication year
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2019Year of publication
- Publication date
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2019-12-02Full publication date if available
- Authors
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S. Sivaganesan, F. Ferdaus, C. Dhanasekaran, G. Sathishkumar, S. SivabalanList of authors in order
- Landing page
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https://doi.org/10.4273/ijvss.11.3.07Publisher landing page
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YesWhether a free full text is available
- OA status
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hybridOpen access status per OpenAlex
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https://doi.org/10.4273/ijvss.11.3.07Direct OA link when available
- Concepts
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Nozzle, Mach number, Supersonic speed, Discharge coefficient, Thrust, Mechanics, Aerospace engineering, Flow (mathematics), Shock (circulatory), Compressible flow, Mechanical engineering, Choked flow, Physics, Engineering, Compressibility, Medicine, Internal medicineTop concepts (fields/topics) attached by OpenAlex
- Cited by
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0Total citation count in OpenAlex
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10Other works algorithmically related by OpenAlex
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| abstract_inverted_index.get | 17 |
| abstract_inverted_index.low | 57 |
| abstract_inverted_index.the | 3, 10, 63, 72, 81, 94, 109, 115, 118, 128, 142, 145, 149, 152, 163, 170, 173 |
| abstract_inverted_index.Mach | 12, 20 |
| abstract_inverted_index.This | 78 |
| abstract_inverted_index.aims | 135 |
| abstract_inverted_index.axis | 116, 150 |
| abstract_inverted_index.exit | 11, 171 |
| abstract_inverted_index.flow | 53, 91, 100, 110, 146, 156 |
| abstract_inverted_index.from | 56 |
| abstract_inverted_index.into | 28 |
| abstract_inverted_index.must | 111 |
| abstract_inverted_index.need | 23 |
| abstract_inverted_index.this | 133 |
| abstract_inverted_index.were | 158 |
| abstract_inverted_index.(C-D) | 44 |
| abstract_inverted_index.Based | 126 |
| abstract_inverted_index.along | 148 |
| abstract_inverted_index.exit, | 73 |
| abstract_inverted_index.flows | 41 |
| abstract_inverted_index.gases | 167 |
| abstract_inverted_index.order | 15 |
| abstract_inverted_index.paper | 79 |
| abstract_inverted_index.shock | 104 |
| abstract_inverted_index.sonic | 60 |
| abstract_inverted_index.study | 134 |
| abstract_inverted_index.using | 32 |
| abstract_inverted_index.while | 42 |
| abstract_inverted_index.Curved | 51 |
| abstract_inverted_index.attain | 89 |
| abstract_inverted_index.curved | 86 |
| abstract_inverted_index.devoid | 98 |
| abstract_inverted_index.energy | 27, 30 |
| abstract_inverted_index.flows. | 50 |
| abstract_inverted_index.nozzle | 1, 45, 52, 87, 119 |
| abstract_inverted_index.throat | 64 |
| abstract_inverted_index.thrust | 96, 123 |
| abstract_inverted_index.waves. | 105 |
| abstract_inverted_index.Nozzle. | 154 |
| abstract_inverted_index.convert | 25 |
| abstract_inverted_index.details | 80 |
| abstract_inverted_index.develop | 137 |
| abstract_inverted_index.dynamic | 131 |
| abstract_inverted_index.extreme | 122 |
| abstract_inverted_index.further | 66 |
| abstract_inverted_index.kinetic | 29 |
| abstract_inverted_index.nozzle. | 34, 77 |
| abstract_inverted_index.nozzles | 36 |
| abstract_inverted_index.number, | 21 |
| abstract_inverted_index.number. | 13 |
| abstract_inverted_index.optimal | 95 |
| abstract_inverted_index.aircraft | 4 |
| abstract_inverted_index.approach | 140 |
| abstract_inverted_index.chamber. | 175 |
| abstract_inverted_index.designed | 7 |
| abstract_inverted_index.expanded | 67 |
| abstract_inverted_index.parallel | 113 |
| abstract_inverted_index.pressure | 26 |
| abstract_inverted_index.selected | 159 |
| abstract_inverted_index.subsonic | 40, 58 |
| abstract_inverted_index.utilized | 38, 47 |
| abstract_inverted_index.velocity | 61 |
| abstract_inverted_index.achieving | 121 |
| abstract_inverted_index.designing | 84 |
| abstract_inverted_index.pressure, | 164 |
| abstract_inverted_index.Convergent | 35 |
| abstract_inverted_index.accessible | 168 |
| abstract_inverted_index.combustion | 174 |
| abstract_inverted_index.conditions | 157 |
| abstract_inverted_index.equations, | 132 |
| abstract_inverted_index.maximizing | 93 |
| abstract_inverted_index.navigation | 107 |
| abstract_inverted_index.properties | 147 |
| abstract_inverted_index.separation | 101 |
| abstract_inverted_index.supersonic | 49, 69 |
| abstract_inverted_index.velocities | 70 |
| abstract_inverted_index.accelerated | 55 |
| abstract_inverted_index.calculation | 143 |
| abstract_inverted_index.considering | 9 |
| abstract_inverted_index.fundamental | 129 |
| abstract_inverted_index.relevancies | 82 |
| abstract_inverted_index.super-sonic | 90 |
| abstract_inverted_index.temperature | 165 |
| abstract_inverted_index.theoretical | 139 |
| abstract_inverted_index.premeditated | 19 |
| abstract_inverted_index.proficiency. | 125 |
| abstract_inverted_index.consideration | 161 |
| abstract_inverted_index.Convergent-Divergent | 43 |
| cited_by_percentile_year | |
| countries_distinct_count | 2 |
| institutions_distinct_count | 5 |
| sustainable_development_goals[0].id | https://metadata.un.org/sdg/7 |
| sustainable_development_goals[0].score | 0.8999999761581421 |
| sustainable_development_goals[0].display_name | Affordable and clean energy |
| citation_normalized_percentile.value | 0.16419842 |
| citation_normalized_percentile.is_in_top_1_percent | False |
| citation_normalized_percentile.is_in_top_10_percent | False |