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You searched for subject:(in flight icing). Showing records 1 – 5 of 5 total matches.

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1. Droz, Christophe. Guidage des ondes d'ordre élevé dans les composites : application au dégivrage en vol des pales d'hélicoptères : High-order wave propagation in composite waveguides : application to in-flight de-icing of helicopter rotor blades.

Degree: Docteur es, Dynamique des structures, 2015, Ecully, Ecole centrale de Lyon

Lorsqu’un hélicoptère opère dans des conditions givrantes extrêmes, l’accumulation de glace sur les pales peut considérablement impacter les performances de l’appareil. De nombreuses recherches portant… (more)

Subjects/Keywords: Pales d'hélicoptères; Dégivrage en vol; Helicopter rotor; In-flight de-icing

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Droz, C. (2015). Guidage des ondes d'ordre élevé dans les composites : application au dégivrage en vol des pales d'hélicoptères : High-order wave propagation in composite waveguides : application to in-flight de-icing of helicopter rotor blades. (Doctoral Dissertation). Ecully, Ecole centrale de Lyon. Retrieved from http://www.theses.fr/2015ECDL0026

Chicago Manual of Style (16th Edition):

Droz, Christophe. “Guidage des ondes d'ordre élevé dans les composites : application au dégivrage en vol des pales d'hélicoptères : High-order wave propagation in composite waveguides : application to in-flight de-icing of helicopter rotor blades.” 2015. Doctoral Dissertation, Ecully, Ecole centrale de Lyon. Accessed March 03, 2021. http://www.theses.fr/2015ECDL0026.

MLA Handbook (7th Edition):

Droz, Christophe. “Guidage des ondes d'ordre élevé dans les composites : application au dégivrage en vol des pales d'hélicoptères : High-order wave propagation in composite waveguides : application to in-flight de-icing of helicopter rotor blades.” 2015. Web. 03 Mar 2021.

Vancouver:

Droz C. Guidage des ondes d'ordre élevé dans les composites : application au dégivrage en vol des pales d'hélicoptères : High-order wave propagation in composite waveguides : application to in-flight de-icing of helicopter rotor blades. [Internet] [Doctoral dissertation]. Ecully, Ecole centrale de Lyon; 2015. [cited 2021 Mar 03]. Available from: http://www.theses.fr/2015ECDL0026.

Council of Science Editors:

Droz C. Guidage des ondes d'ordre élevé dans les composites : application au dégivrage en vol des pales d'hélicoptères : High-order wave propagation in composite waveguides : application to in-flight de-icing of helicopter rotor blades. [Doctoral Dissertation]. Ecully, Ecole centrale de Lyon; 2015. Available from: http://www.theses.fr/2015ECDL0026


Iowa State University

2. Li, Haixing. Experimental studies on the dynamics of in-flight and impacting water droplets pertinent to aircraft icing phenomena.

Degree: 2017, Iowa State University

 Aircraft icing is widely recognized as a significant hazard to aircraft operations in cold weather. When an aircraft or rotorcraft fly in a cold climate,… (more)

Subjects/Keywords: 3-D shape reconstruction of impact droplet; Aircraft icing; Droplet impact dynamics; Droplet impact on super-hydrophobic surface; In-flight droplets temperature measurement; Aerospace Engineering

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APA (6th Edition):

Li, H. (2017). Experimental studies on the dynamics of in-flight and impacting water droplets pertinent to aircraft icing phenomena. (Thesis). Iowa State University. Retrieved from https://lib.dr.iastate.edu/etd/15564

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Li, Haixing. “Experimental studies on the dynamics of in-flight and impacting water droplets pertinent to aircraft icing phenomena.” 2017. Thesis, Iowa State University. Accessed March 03, 2021. https://lib.dr.iastate.edu/etd/15564.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Li, Haixing. “Experimental studies on the dynamics of in-flight and impacting water droplets pertinent to aircraft icing phenomena.” 2017. Web. 03 Mar 2021.

Vancouver:

Li H. Experimental studies on the dynamics of in-flight and impacting water droplets pertinent to aircraft icing phenomena. [Internet] [Thesis]. Iowa State University; 2017. [cited 2021 Mar 03]. Available from: https://lib.dr.iastate.edu/etd/15564.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Li H. Experimental studies on the dynamics of in-flight and impacting water droplets pertinent to aircraft icing phenomena. [Thesis]. Iowa State University; 2017. Available from: https://lib.dr.iastate.edu/etd/15564

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

3. Pena, Dorian. Développement d'un code de givrage tridimensionnel avec méthode Level-Set : Development of a three-dimensional icing code using level-set method.

Degree: Docteur es, Mécanique des fluides, 2016, Strasbourg; Ecole polytechnique (Montréal, Canada)

Le travail réalisé dans cette thèse introduit le concept de l'utilisation de la méthode Level-Set pour simuler l'interface Glace/Air au cours du temps lors du… (more)

Subjects/Keywords: Givrage; Méthode Eulérienne de transport de particules; Thermodynamique du givrage; Méthode Level-Set; Méthode chimère; Icing; Eulerian approach; Process of in-flight aircraft icing; Level-Set method; Chimeria method; Navier-Stokes-Multi-Blocks; 629.1; 532.5

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APA (6th Edition):

Pena, D. (2016). Développement d'un code de givrage tridimensionnel avec méthode Level-Set : Development of a three-dimensional icing code using level-set method. (Doctoral Dissertation). Strasbourg; Ecole polytechnique (Montréal, Canada). Retrieved from http://www.theses.fr/2016STRAD014

Chicago Manual of Style (16th Edition):

Pena, Dorian. “Développement d'un code de givrage tridimensionnel avec méthode Level-Set : Development of a three-dimensional icing code using level-set method.” 2016. Doctoral Dissertation, Strasbourg; Ecole polytechnique (Montréal, Canada). Accessed March 03, 2021. http://www.theses.fr/2016STRAD014.

MLA Handbook (7th Edition):

Pena, Dorian. “Développement d'un code de givrage tridimensionnel avec méthode Level-Set : Development of a three-dimensional icing code using level-set method.” 2016. Web. 03 Mar 2021.

Vancouver:

Pena D. Développement d'un code de givrage tridimensionnel avec méthode Level-Set : Development of a three-dimensional icing code using level-set method. [Internet] [Doctoral dissertation]. Strasbourg; Ecole polytechnique (Montréal, Canada); 2016. [cited 2021 Mar 03]. Available from: http://www.theses.fr/2016STRAD014.

Council of Science Editors:

Pena D. Développement d'un code de givrage tridimensionnel avec méthode Level-Set : Development of a three-dimensional icing code using level-set method. [Doctoral Dissertation]. Strasbourg; Ecole polytechnique (Montréal, Canada); 2016. Available from: http://www.theses.fr/2016STRAD014


University of Waterloo

4. Geiger, Paul. Simulation of In-Flight Rime Icing Using a Non-Body-Fitted Mesh.

Degree: 2020, University of Waterloo

 In-flight rime icing occurs when supercooled droplets strike the surface of an aircraft and instantly freeze. This often occurs in the high moisture, cold environments… (more)

Subjects/Keywords: in-flight icing; rime icing; immersed boundary method; cut-cell method; finite volume method; level set method; non-body-fitted mesh

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Geiger, P. (2020). Simulation of In-Flight Rime Icing Using a Non-Body-Fitted Mesh. (Thesis). University of Waterloo. Retrieved from http://hdl.handle.net/10012/15810

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Geiger, Paul. “Simulation of In-Flight Rime Icing Using a Non-Body-Fitted Mesh.” 2020. Thesis, University of Waterloo. Accessed March 03, 2021. http://hdl.handle.net/10012/15810.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Geiger, Paul. “Simulation of In-Flight Rime Icing Using a Non-Body-Fitted Mesh.” 2020. Web. 03 Mar 2021.

Vancouver:

Geiger P. Simulation of In-Flight Rime Icing Using a Non-Body-Fitted Mesh. [Internet] [Thesis]. University of Waterloo; 2020. [cited 2021 Mar 03]. Available from: http://hdl.handle.net/10012/15810.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Geiger P. Simulation of In-Flight Rime Icing Using a Non-Body-Fitted Mesh. [Thesis]. University of Waterloo; 2020. Available from: http://hdl.handle.net/10012/15810

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

5. Andersson, Daniel. The performance of an iced aircraft wing.

Degree: Engineering Science, 2011, University West

  The goal of this thesis work has been to develop and manufacture an ice layer which was to be mounted on the tip of… (more)

Subjects/Keywords: Airfoil; ice layer; in-flight icing; wind tunnel; rapid prototyping; lift force

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Andersson, D. (2011). The performance of an iced aircraft wing. (Thesis). University West. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:hv:diva-4098

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Andersson, Daniel. “The performance of an iced aircraft wing.” 2011. Thesis, University West. Accessed March 03, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:hv:diva-4098.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Andersson, Daniel. “The performance of an iced aircraft wing.” 2011. Web. 03 Mar 2021.

Vancouver:

Andersson D. The performance of an iced aircraft wing. [Internet] [Thesis]. University West; 2011. [cited 2021 Mar 03]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:hv:diva-4098.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Andersson D. The performance of an iced aircraft wing. [Thesis]. University West; 2011. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:hv:diva-4098

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

.