Simulation of heat transfer from hot-air jets impinging a three-dimensional concave surface

Mathieu Fregeau; Mohammad Gabr; Ion Paraschivoiu; Farooq Saeed

doi:10.2514/1.39846

Simulation of heat transfer from hot-air jets impinging a three-dimensional concave surface

Mathieu Fregeau^*, Mohammad Gabr, Ion Paraschivoiu, Farooq Saeed

^*Corresponding author for this work

King Fahd University of Petroleum & Minerals

Research output: Contribution to journal › Article › peer-review

30 Scopus citations

Abstract

The simulation of heat transfer from hot-air jets impinging a three-dimensional concave surface was developed in order to enhance safety under natural icing conditions. The deployment magnifies a reliable ice-accretion and anti-icing simulation code CANICE geared towards the specific needs of Bombardier Aerospace. Also the use of computational fluid dynamics (CFD) tools to model the internal hot-air region in conjunction with a 3-D ice-accretion code requires extensive computational resources. The study has used the state-of-the-art commercial CFD software FLUENT, where the software comes with the mesh generator GAMBIT for modeling and meshing geometry. The results showed the decrease in the Nusselt number along with s axis much faster than along y axis. The study also speculated that the use of smaller H is likely to be more effective than increasing jet Mach number or the number of the jets.

Original language	English
Pages (from-to)	721-725
Number of pages	5
Journal	Journal of Aircraft
Volume	46
Issue number	2
DOIs	https://doi.org/10.2514/1.39846
State	Published - 2009

Bibliographical note

Funding Information:
The authors would like to acknowledge the support of the Natural Sciences and Engineering Research Council, Canada, through a cooperative research and development grant with Bombardier Aerospace. Helpful discussions with Fassi Kafyeke and his team at

Funding Information:
the Advanced Aerodynamics Department, Bombardier Aerospace, are gratefully acknowledged. The authors would also like to acknowledge the support of King Fahd University of Petroleum and Minerals for accomplishing this study.

ASJC Scopus subject areas

Aerospace Engineering

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10.2514/1.39846

Cite this

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title = "Simulation of heat transfer from hot-air jets impinging a three-dimensional concave surface",

abstract = "The simulation of heat transfer from hot-air jets impinging a three-dimensional concave surface was developed in order to enhance safety under natural icing conditions. The deployment magnifies a reliable ice-accretion and anti-icing simulation code CANICE geared towards the specific needs of Bombardier Aerospace. Also the use of computational fluid dynamics (CFD) tools to model the internal hot-air region in conjunction with a 3-D ice-accretion code requires extensive computational resources. The study has used the state-of-the-art commercial CFD software FLUENT, where the software comes with the mesh generator GAMBIT for modeling and meshing geometry. The results showed the decrease in the Nusselt number along with s axis much faster than along y axis. The study also speculated that the use of smaller H is likely to be more effective than increasing jet Mach number or the number of the jets.",

author = "Mathieu Fregeau and Mohammad Gabr and Ion Paraschivoiu and Farooq Saeed",

note = "Funding Information: The authors would like to acknowledge the support of the Natural Sciences and Engineering Research Council, Canada, through a cooperative research and development grant with Bombardier Aerospace. Helpful discussions with Fassi Kafyeke and his team at Funding Information: the Advanced Aerodynamics Department, Bombardier Aerospace, are gratefully acknowledged. The authors would also like to acknowledge the support of King Fahd University of Petroleum and Minerals for accomplishing this study.",

year = "2009",

doi = "10.2514/1.39846",

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AU - Gabr, Mohammad

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AU - Saeed, Farooq

N1 - Funding Information: The authors would like to acknowledge the support of the Natural Sciences and Engineering Research Council, Canada, through a cooperative research and development grant with Bombardier Aerospace. Helpful discussions with Fassi Kafyeke and his team at Funding Information: the Advanced Aerodynamics Department, Bombardier Aerospace, are gratefully acknowledged. The authors would also like to acknowledge the support of King Fahd University of Petroleum and Minerals for accomplishing this study.

PY - 2009

Y1 - 2009

N2 - The simulation of heat transfer from hot-air jets impinging a three-dimensional concave surface was developed in order to enhance safety under natural icing conditions. The deployment magnifies a reliable ice-accretion and anti-icing simulation code CANICE geared towards the specific needs of Bombardier Aerospace. Also the use of computational fluid dynamics (CFD) tools to model the internal hot-air region in conjunction with a 3-D ice-accretion code requires extensive computational resources. The study has used the state-of-the-art commercial CFD software FLUENT, where the software comes with the mesh generator GAMBIT for modeling and meshing geometry. The results showed the decrease in the Nusselt number along with s axis much faster than along y axis. The study also speculated that the use of smaller H is likely to be more effective than increasing jet Mach number or the number of the jets.

AB - The simulation of heat transfer from hot-air jets impinging a three-dimensional concave surface was developed in order to enhance safety under natural icing conditions. The deployment magnifies a reliable ice-accretion and anti-icing simulation code CANICE geared towards the specific needs of Bombardier Aerospace. Also the use of computational fluid dynamics (CFD) tools to model the internal hot-air region in conjunction with a 3-D ice-accretion code requires extensive computational resources. The study has used the state-of-the-art commercial CFD software FLUENT, where the software comes with the mesh generator GAMBIT for modeling and meshing geometry. The results showed the decrease in the Nusselt number along with s axis much faster than along y axis. The study also speculated that the use of smaller H is likely to be more effective than increasing jet Mach number or the number of the jets.

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Simulation of heat transfer from hot-air jets impinging a three-dimensional concave surface

Abstract

Bibliographical note

ASJC Scopus subject areas

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