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You searched for subject:(aircraft icing). Showing records 1 – 29 of 29 total matches.

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Baylor University

1. [No author]. Convection from realistic ice roughness on a simulated NACA 0012 airfoil.

Degree: 2015, Baylor University

 Ice roughness properties are critically important to the development of ice accretions on aircraft surfaces. Ice accretions degrade aircraft performance by increasing the skin friction… (more)

Subjects/Keywords: Aircraft icing. Ice roughness.

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

APA (6th Edition):

author], [. (2015). Convection from realistic ice roughness on a simulated NACA 0012 airfoil. (Thesis). Baylor University. Retrieved from http://hdl.handle.net/2104/9534

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):

author], [No. “Convection from realistic ice roughness on a simulated NACA 0012 airfoil. ” 2015. Thesis, Baylor University. Accessed January 18, 2019. http://hdl.handle.net/2104/9534.

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

MLA Handbook (7th Edition):

author], [No. “Convection from realistic ice roughness on a simulated NACA 0012 airfoil. ” 2015. Web. 18 Jan 2019.

Vancouver:

author] [. Convection from realistic ice roughness on a simulated NACA 0012 airfoil. [Internet] [Thesis]. Baylor University; 2015. [cited 2019 Jan 18]. Available from: http://hdl.handle.net/2104/9534.

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

Council of Science Editors:

author] [. Convection from realistic ice roughness on a simulated NACA 0012 airfoil. [Thesis]. Baylor University; 2015. Available from: http://hdl.handle.net/2104/9534

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


University of Virginia

2. Rankin, Korey. Adaptive Control of Aircraft in Uncertain Icing Conditions.

Degree: MS, 2014, University of Virginia

 Ice accretion on aircraft is, at times, unavoidable. The unpredictable effects of ice on aircraft dynamics makes an encounter with a weather pattern where ice… (more)

Subjects/Keywords: adaptive; adaptive control; icing; aircraft icing; airplane icing

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APA (6th Edition):

Rankin, K. (2014). Adaptive Control of Aircraft in Uncertain Icing Conditions. (Doctoral Dissertation). University of Virginia. Retrieved from http://libra.virginia.edu/catalog/libra-oa:6544

Chicago Manual of Style (16th Edition):

Rankin, Korey. “Adaptive Control of Aircraft in Uncertain Icing Conditions.” 2014. Doctoral Dissertation, University of Virginia. Accessed January 18, 2019. http://libra.virginia.edu/catalog/libra-oa:6544.

MLA Handbook (7th Edition):

Rankin, Korey. “Adaptive Control of Aircraft in Uncertain Icing Conditions.” 2014. Web. 18 Jan 2019.

Vancouver:

Rankin K. Adaptive Control of Aircraft in Uncertain Icing Conditions. [Internet] [Doctoral dissertation]. University of Virginia; 2014. [cited 2019 Jan 18]. Available from: http://libra.virginia.edu/catalog/libra-oa:6544.

Council of Science Editors:

Rankin K. Adaptive Control of Aircraft in Uncertain Icing Conditions. [Doctoral Dissertation]. University of Virginia; 2014. Available from: http://libra.virginia.edu/catalog/libra-oa:6544


Brno University of Technology

3. Fazekaš, Slavomír. Odmrazovací soustavy letadel .

Degree: 2013, Brno University of Technology

 Cieľom mojej bakalárskej práce je zoznámiť sa s nebezpečenstvom námrazy na lietadlách, jej vznikom a spôsobom odstránenia. Práca zahŕňa popis jednotlivých sústav na ochranu lietadla… (more)

Subjects/Keywords: Lietadlo; námraza; lietadlové systémy; protinámrazový systém; odmrazovanie; Aircraft; icing; aircraft systems; anti-icing; de-icing

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APA (6th Edition):

Fazekaš, S. (2013). Odmrazovací soustavy letadel . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/27286

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):

Fazekaš, Slavomír. “Odmrazovací soustavy letadel .” 2013. Thesis, Brno University of Technology. Accessed January 18, 2019. http://hdl.handle.net/11012/27286.

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

MLA Handbook (7th Edition):

Fazekaš, Slavomír. “Odmrazovací soustavy letadel .” 2013. Web. 18 Jan 2019.

Vancouver:

Fazekaš S. Odmrazovací soustavy letadel . [Internet] [Thesis]. Brno University of Technology; 2013. [cited 2019 Jan 18]. Available from: http://hdl.handle.net/11012/27286.

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

Council of Science Editors:

Fazekaš S. Odmrazovací soustavy letadel . [Thesis]. Brno University of Technology; 2013. Available from: http://hdl.handle.net/11012/27286

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


Brno University of Technology

4. Smékal, Aleš. Odmrazovací soustavy letadel .

Degree: 2014, Brno University of Technology

 Cílem této bakalářské práce je seznámení se s problematikou námrazy na letadlech. Obsahuje rozdělení jednotlivých systémů na odmrazovací a protinámrazové, dále je uvedena energetická náročnost… (more)

Subjects/Keywords: Námraza; protinámrazový; letadlové systémy; led; odmrazování; Icing; anti-icing; aircraft systems; ice; de-icing

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APA (6th Edition):

Smékal, A. (2014). Odmrazovací soustavy letadel . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/33535

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):

Smékal, Aleš. “Odmrazovací soustavy letadel .” 2014. Thesis, Brno University of Technology. Accessed January 18, 2019. http://hdl.handle.net/11012/33535.

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

MLA Handbook (7th Edition):

Smékal, Aleš. “Odmrazovací soustavy letadel .” 2014. Web. 18 Jan 2019.

Vancouver:

Smékal A. Odmrazovací soustavy letadel . [Internet] [Thesis]. Brno University of Technology; 2014. [cited 2019 Jan 18]. Available from: http://hdl.handle.net/11012/33535.

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

Council of Science Editors:

Smékal A. Odmrazovací soustavy letadel . [Thesis]. Brno University of Technology; 2014. Available from: http://hdl.handle.net/11012/33535

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


Cranfield University

5. Charpin, Jean P. F. Water flow on accreting ice surfaces.

Degree: PhD, 2002, Cranfield University

 Ice growth may rapidly degrade the aerodynamic performance of an aircraft. It can also severely damage structures such as communication towers or power lines. Subsequently,… (more)

Subjects/Keywords: 629; Aircraft icing

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APA (6th Edition):

Charpin, J. P. F. (2002). Water flow on accreting ice surfaces. (Doctoral Dissertation). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/10742 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.273526

Chicago Manual of Style (16th Edition):

Charpin, Jean P F. “Water flow on accreting ice surfaces.” 2002. Doctoral Dissertation, Cranfield University. Accessed January 18, 2019. http://dspace.lib.cranfield.ac.uk/handle/1826/10742 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.273526.

MLA Handbook (7th Edition):

Charpin, Jean P F. “Water flow on accreting ice surfaces.” 2002. Web. 18 Jan 2019.

Vancouver:

Charpin JPF. Water flow on accreting ice surfaces. [Internet] [Doctoral dissertation]. Cranfield University; 2002. [cited 2019 Jan 18]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/10742 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.273526.

Council of Science Editors:

Charpin JPF. Water flow on accreting ice surfaces. [Doctoral Dissertation]. Cranfield University; 2002. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/10742 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.273526


Penn State University

6. Borigo, Cody J. A Novel Actuator Phasing Method for Ultrasonic De-icing of Aircraft Structures.

Degree: PhD, Engineering Science and Mechanics, 2014, Penn State University

Aircraft icing is a critical concern for commercial and military rotorcraft and fixed-wing aircraft. In-flight icing can lead to dramatic decreases in lift and increases… (more)

Subjects/Keywords: de-icing; aircraft; ultrasound; ultrasonic; vibration; ice protection; anti-icing; phasing; piezoelectric

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

APA (6th Edition):

Borigo, C. J. (2014). A Novel Actuator Phasing Method for Ultrasonic De-icing of Aircraft Structures. (Doctoral Dissertation). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/23379

Chicago Manual of Style (16th Edition):

Borigo, Cody J. “A Novel Actuator Phasing Method for Ultrasonic De-icing of Aircraft Structures.” 2014. Doctoral Dissertation, Penn State University. Accessed January 18, 2019. https://etda.libraries.psu.edu/catalog/23379.

MLA Handbook (7th Edition):

Borigo, Cody J. “A Novel Actuator Phasing Method for Ultrasonic De-icing of Aircraft Structures.” 2014. Web. 18 Jan 2019.

Vancouver:

Borigo CJ. A Novel Actuator Phasing Method for Ultrasonic De-icing of Aircraft Structures. [Internet] [Doctoral dissertation]. Penn State University; 2014. [cited 2019 Jan 18]. Available from: https://etda.libraries.psu.edu/catalog/23379.

Council of Science Editors:

Borigo CJ. A Novel Actuator Phasing Method for Ultrasonic De-icing of Aircraft Structures. [Doctoral Dissertation]. Penn State University; 2014. Available from: https://etda.libraries.psu.edu/catalog/23379


Baylor University

7. Tecson, Joshua Logan. Convective heat transfer from realistic ice roughness distributions.

Degree: Mechanical Engineering., 2013, Baylor University

 As supercooled water droplets impinge the surfaces of in-flight aircraft, a layer of accreted ice will form. In the initial stages of the accretion process,… (more)

Subjects/Keywords: Convective heat transfer.; Aircraft icing.; Ice roughness.; Surface roughness.

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APA (6th Edition):

Tecson, J. L. (2013). Convective heat transfer from realistic ice roughness distributions. (Thesis). Baylor University. Retrieved from http://hdl.handle.net/2104/8757

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):

Tecson, Joshua Logan. “Convective heat transfer from realistic ice roughness distributions. ” 2013. Thesis, Baylor University. Accessed January 18, 2019. http://hdl.handle.net/2104/8757.

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

MLA Handbook (7th Edition):

Tecson, Joshua Logan. “Convective heat transfer from realistic ice roughness distributions. ” 2013. Web. 18 Jan 2019.

Vancouver:

Tecson JL. Convective heat transfer from realistic ice roughness distributions. [Internet] [Thesis]. Baylor University; 2013. [cited 2019 Jan 18]. Available from: http://hdl.handle.net/2104/8757.

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

Council of Science Editors:

Tecson JL. Convective heat transfer from realistic ice roughness distributions. [Thesis]. Baylor University; 2013. Available from: http://hdl.handle.net/2104/8757

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

8. Triphahn, Christopher. Lagrangian Parcel Volume method applied to icing surfaces to predict impact efficiency.

Degree: MS, 4048, 2012, University of Illinois – Urbana-Champaign

 When trying to predict how and where ice will accrete on an aircraft, engineers first need to be able to track the path and concentration… (more)

Subjects/Keywords: Impact Efficiency; Aircraft Icing

Aircraft icing is a major concern during the development of new aircraft components such as… …cause severe decreases in the performance, stability, and controllability of the aircraft. The… …on the surface. To better understand icing phenomena, representations of spatial and… …icing cloud in which the particles are polydisperse (i.e. multiple particle sizes)… 

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APA (6th Edition):

Triphahn, C. (2012). Lagrangian Parcel Volume method applied to icing surfaces to predict impact efficiency. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/42376

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):

Triphahn, Christopher. “Lagrangian Parcel Volume method applied to icing surfaces to predict impact efficiency.” 2012. Thesis, University of Illinois – Urbana-Champaign. Accessed January 18, 2019. http://hdl.handle.net/2142/42376.

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

MLA Handbook (7th Edition):

Triphahn, Christopher. “Lagrangian Parcel Volume method applied to icing surfaces to predict impact efficiency.” 2012. Web. 18 Jan 2019.

Vancouver:

Triphahn C. Lagrangian Parcel Volume method applied to icing surfaces to predict impact efficiency. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2012. [cited 2019 Jan 18]. Available from: http://hdl.handle.net/2142/42376.

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

Council of Science Editors:

Triphahn C. Lagrangian Parcel Volume method applied to icing surfaces to predict impact efficiency. [Thesis]. University of Illinois – Urbana-Champaign; 2012. Available from: http://hdl.handle.net/2142/42376

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


Università degli studi di Bergamo

9. Antonini, Carlo. Superhydrophobicity as a strategy against icing. Analysis of the water/surface dynamic interaction for icing mitigation.

Degree: 2011, Università degli studi di Bergamo

 The thesis illustrates the efforts made to proof how water repellent surfaces can help reducing ice accretion in icing conditions: tests performed in an icing(more)

Subjects/Keywords: Aircraft icing; icing mitigation; anti-icing; de-icing; icing protection; superhydrophobicity; superhydrophobic surfaces; SHS; superhydrophobic coatings; wettability; drop impact; contact angle; high speed video; ING-IND/09 - Sistemi per l'Energia e L'Ambiente

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APA (6th Edition):

Antonini, C. (2011). Superhydrophobicity as a strategy against icing. Analysis of the water/surface dynamic interaction for icing mitigation. (Thesis). Università degli studi di Bergamo. Retrieved from http://hdl.handle.net/10446/881

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):

Antonini, Carlo. “Superhydrophobicity as a strategy against icing. Analysis of the water/surface dynamic interaction for icing mitigation.” 2011. Thesis, Università degli studi di Bergamo. Accessed January 18, 2019. http://hdl.handle.net/10446/881.

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

MLA Handbook (7th Edition):

Antonini, Carlo. “Superhydrophobicity as a strategy against icing. Analysis of the water/surface dynamic interaction for icing mitigation.” 2011. Web. 18 Jan 2019.

Vancouver:

Antonini C. Superhydrophobicity as a strategy against icing. Analysis of the water/surface dynamic interaction for icing mitigation. [Internet] [Thesis]. Università degli studi di Bergamo; 2011. [cited 2019 Jan 18]. Available from: http://hdl.handle.net/10446/881.

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

Council of Science Editors:

Antonini C. Superhydrophobicity as a strategy against icing. Analysis of the water/surface dynamic interaction for icing mitigation. [Thesis]. Università degli studi di Bergamo; 2011. Available from: http://hdl.handle.net/10446/881

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


Baylor University

10. [No author]. Convective enhancement on airfoils due to ice roughness elements in stagnation region flows.

Degree: 2015, Baylor University

Aircraft icing is a dangerous phenomenon which has been studied in-depth by researchers since the earliest days of aviation in order to improve safety for… (more)

Subjects/Keywords: Aircraft. Icing. Branch. Aviation. Wind tunnel. LEWICE. VIST. NASA. Ice. Roughness. Convection. Heat. Transfer.

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APA (6th Edition):

author], [. (2015). Convective enhancement on airfoils due to ice roughness elements in stagnation region flows. (Thesis). Baylor University. Retrieved from http://hdl.handle.net/2104/9559

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):

author], [No. “Convective enhancement on airfoils due to ice roughness elements in stagnation region flows. ” 2015. Thesis, Baylor University. Accessed January 18, 2019. http://hdl.handle.net/2104/9559.

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

MLA Handbook (7th Edition):

author], [No. “Convective enhancement on airfoils due to ice roughness elements in stagnation region flows. ” 2015. Web. 18 Jan 2019.

Vancouver:

author] [. Convective enhancement on airfoils due to ice roughness elements in stagnation region flows. [Internet] [Thesis]. Baylor University; 2015. [cited 2019 Jan 18]. Available from: http://hdl.handle.net/2104/9559.

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

Council of Science Editors:

author] [. Convective enhancement on airfoils due to ice roughness elements in stagnation region flows. [Thesis]. Baylor University; 2015. Available from: http://hdl.handle.net/2104/9559

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


Penn State University

11. Han, Yiqiang. Aerodynamics and Thermal Physics of Helicopter Ice Accretion.

Degree: PhD, Aerospace Engineering, 2015, Penn State University

 Ice accretion on aircraft introduces significant loss in airfoil performance. Reduced lift-to-drag ratio reduces the vehicle capability to maintain altitude and also limits its maneuverability.… (more)

Subjects/Keywords: Aircraft Icing; Ice Accretion Modelling; Helicopter; Aerodynamics; Heat Transfer; Surface Roughness; Performance Degradation

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APA (6th Edition):

Han, Y. (2015). Aerodynamics and Thermal Physics of Helicopter Ice Accretion. (Doctoral Dissertation). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/28036

Chicago Manual of Style (16th Edition):

Han, Yiqiang. “Aerodynamics and Thermal Physics of Helicopter Ice Accretion.” 2015. Doctoral Dissertation, Penn State University. Accessed January 18, 2019. https://etda.libraries.psu.edu/catalog/28036.

MLA Handbook (7th Edition):

Han, Yiqiang. “Aerodynamics and Thermal Physics of Helicopter Ice Accretion.” 2015. Web. 18 Jan 2019.

Vancouver:

Han Y. Aerodynamics and Thermal Physics of Helicopter Ice Accretion. [Internet] [Doctoral dissertation]. Penn State University; 2015. [cited 2019 Jan 18]. Available from: https://etda.libraries.psu.edu/catalog/28036.

Council of Science Editors:

Han Y. Aerodynamics and Thermal Physics of Helicopter Ice Accretion. [Doctoral Dissertation]. Penn State University; 2015. Available from: https://etda.libraries.psu.edu/catalog/28036


University of Washington

12. Sandhu, Navdeep. Aerodynamics of a Swept Wing With Simulated Scalloped Ice at Low Reynolds Number.

Degree: 2018, University of Washington

 This thesis studied the aerodynamic effects of a single high-fidelity scalloped ice accretion simulation and a low-fidelity simulation of the same shape. These data were… (more)

Subjects/Keywords: aerodynamics; aircraft icing; CRM65; swept wing; wake survey; Aerospace engineering; Aeronautics and astronautics

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APA (6th Edition):

Sandhu, N. (2018). Aerodynamics of a Swept Wing With Simulated Scalloped Ice at Low Reynolds Number. (Thesis). University of Washington. Retrieved from http://hdl.handle.net/1773/42162

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):

Sandhu, Navdeep. “Aerodynamics of a Swept Wing With Simulated Scalloped Ice at Low Reynolds Number.” 2018. Thesis, University of Washington. Accessed January 18, 2019. http://hdl.handle.net/1773/42162.

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

MLA Handbook (7th Edition):

Sandhu, Navdeep. “Aerodynamics of a Swept Wing With Simulated Scalloped Ice at Low Reynolds Number.” 2018. Web. 18 Jan 2019.

Vancouver:

Sandhu N. Aerodynamics of a Swept Wing With Simulated Scalloped Ice at Low Reynolds Number. [Internet] [Thesis]. University of Washington; 2018. [cited 2019 Jan 18]. Available from: http://hdl.handle.net/1773/42162.

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

Council of Science Editors:

Sandhu N. Aerodynamics of a Swept Wing With Simulated Scalloped Ice at Low Reynolds Number. [Thesis]. University of Washington; 2018. Available from: http://hdl.handle.net/1773/42162

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


Penn State University

13. Rocco, Edward. Super-cooled Large Droplet Experimental Reproduction, Ice Shape Modeling, and Scaling Law Assessment.

Degree: 2017, Penn State University

 The simulation of icing conditions is sought for potential aircraft certification,and therefore test facilities that can generate conditions able to reproduce theice accretion phenomena are… (more)

Subjects/Keywords: SLD Accretion; Super-cooled Large Droplets; Aircraft Icing; Ice Scaling Methods; Ice Accretion Testing

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APA (6th Edition):

Rocco, E. (2017). Super-cooled Large Droplet Experimental Reproduction, Ice Shape Modeling, and Scaling Law Assessment. (Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/13819etr5040

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):

Rocco, Edward. “Super-cooled Large Droplet Experimental Reproduction, Ice Shape Modeling, and Scaling Law Assessment.” 2017. Thesis, Penn State University. Accessed January 18, 2019. https://etda.libraries.psu.edu/catalog/13819etr5040.

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

MLA Handbook (7th Edition):

Rocco, Edward. “Super-cooled Large Droplet Experimental Reproduction, Ice Shape Modeling, and Scaling Law Assessment.” 2017. Web. 18 Jan 2019.

Vancouver:

Rocco E. Super-cooled Large Droplet Experimental Reproduction, Ice Shape Modeling, and Scaling Law Assessment. [Internet] [Thesis]. Penn State University; 2017. [cited 2019 Jan 18]. Available from: https://etda.libraries.psu.edu/catalog/13819etr5040.

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

Council of Science Editors:

Rocco E. Super-cooled Large Droplet Experimental Reproduction, Ice Shape Modeling, and Scaling Law Assessment. [Thesis]. Penn State University; 2017. Available from: https://etda.libraries.psu.edu/catalog/13819etr5040

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

14. Diebold, Jeffrey. Aerodynamics of a swept wing with leading-edge ice at low Reynolds number.

Degree: MS, 4048, 2012, University of Illinois – Urbana-Champaign

 An experimental study of the aerodynamics of a swept wing with ice at low Reynolds number has been performed. The goal of this work was… (more)

Subjects/Keywords: aircraft icing; swept wing icing; swept wing aerodynamics

…especially important when studying aircraft icing because the presence of ice has the potential to… …35 Fig. 2.29 Ice accretion on a swept wing in glaze icing conditions. Arrows indicate… …35 Fig. 2.30 Photographs of ice shapes used by Papadakis et al. for corresponding icing… …After decades of research, airframe icing continues to present a significant challenge to… …aircraft designers and manufacturers. The accretion of ice, especially on lifting surfaces, can… 

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APA (6th Edition):

Diebold, J. (2012). Aerodynamics of a swept wing with leading-edge ice at low Reynolds number. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/34279

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):

Diebold, Jeffrey. “Aerodynamics of a swept wing with leading-edge ice at low Reynolds number.” 2012. Thesis, University of Illinois – Urbana-Champaign. Accessed January 18, 2019. http://hdl.handle.net/2142/34279.

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

MLA Handbook (7th Edition):

Diebold, Jeffrey. “Aerodynamics of a swept wing with leading-edge ice at low Reynolds number.” 2012. Web. 18 Jan 2019.

Vancouver:

Diebold J. Aerodynamics of a swept wing with leading-edge ice at low Reynolds number. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2012. [cited 2019 Jan 18]. Available from: http://hdl.handle.net/2142/34279.

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

Council of Science Editors:

Diebold J. Aerodynamics of a swept wing with leading-edge ice at low Reynolds number. [Thesis]. University of Illinois – Urbana-Champaign; 2012. Available from: http://hdl.handle.net/2142/34279

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


University of Colorado

15. Thompson, Gregory. Advances in a Microphysics Parameterization to Predict Supercooled Liquid Water and Application to Aircraft Icing.

Degree: PhD, Atmospheric & Oceanic Sciences, 2016, University of Colorado

 Aerosols influence cloud and precipitation development in complex ways due to myriad feedbacks at a variety of scales from individual clouds through entire storm systems.… (more)

Subjects/Keywords: supercooled water; ice activation; aircraft icing; interface changes; satellite data; ice accretion; graupel surface precipitation; Aerospace Engineering; Atmospheric Sciences; Meteorology

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APA (6th Edition):

Thompson, G. (2016). Advances in a Microphysics Parameterization to Predict Supercooled Liquid Water and Application to Aircraft Icing. (Doctoral Dissertation). University of Colorado. Retrieved from http://scholar.colorado.edu/atoc_gradetds/62

Chicago Manual of Style (16th Edition):

Thompson, Gregory. “Advances in a Microphysics Parameterization to Predict Supercooled Liquid Water and Application to Aircraft Icing.” 2016. Doctoral Dissertation, University of Colorado. Accessed January 18, 2019. http://scholar.colorado.edu/atoc_gradetds/62.

MLA Handbook (7th Edition):

Thompson, Gregory. “Advances in a Microphysics Parameterization to Predict Supercooled Liquid Water and Application to Aircraft Icing.” 2016. Web. 18 Jan 2019.

Vancouver:

Thompson G. Advances in a Microphysics Parameterization to Predict Supercooled Liquid Water and Application to Aircraft Icing. [Internet] [Doctoral dissertation]. University of Colorado; 2016. [cited 2019 Jan 18]. Available from: http://scholar.colorado.edu/atoc_gradetds/62.

Council of Science Editors:

Thompson G. Advances in a Microphysics Parameterization to Predict Supercooled Liquid Water and Application to Aircraft Icing. [Doctoral Dissertation]. University of Colorado; 2016. Available from: http://scholar.colorado.edu/atoc_gradetds/62


Mississippi State University

16. Mankada Covilakom, Mithun Varma. RANS AND HYBRID RANS/LES COMPUTATIONS FOR THREE-DIMENSIONAL WINGS WITH ICE ACCRETION.

Degree: MS, Aerospace Engineering, 2006, Mississippi State University

 Computational investigations were carried out to evaluate the effectiveness and usability of hybrid RANS/LES techniques for predicting the unsteady separated flow over wings with ice… (more)

Subjects/Keywords: CFD; DES; AIRCRAFT ICING; HYBRID RANS/LES

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APA (6th Edition):

Mankada Covilakom, M. V. (2006). RANS AND HYBRID RANS/LES COMPUTATIONS FOR THREE-DIMENSIONAL WINGS WITH ICE ACCRETION. (Masters Thesis). Mississippi State University. Retrieved from http://sun.library.msstate.edu/ETD-db/theses/available/etd-11092006-232711/ ;

Chicago Manual of Style (16th Edition):

Mankada Covilakom, Mithun Varma. “RANS AND HYBRID RANS/LES COMPUTATIONS FOR THREE-DIMENSIONAL WINGS WITH ICE ACCRETION.” 2006. Masters Thesis, Mississippi State University. Accessed January 18, 2019. http://sun.library.msstate.edu/ETD-db/theses/available/etd-11092006-232711/ ;.

MLA Handbook (7th Edition):

Mankada Covilakom, Mithun Varma. “RANS AND HYBRID RANS/LES COMPUTATIONS FOR THREE-DIMENSIONAL WINGS WITH ICE ACCRETION.” 2006. Web. 18 Jan 2019.

Vancouver:

Mankada Covilakom MV. RANS AND HYBRID RANS/LES COMPUTATIONS FOR THREE-DIMENSIONAL WINGS WITH ICE ACCRETION. [Internet] [Masters thesis]. Mississippi State University; 2006. [cited 2019 Jan 18]. Available from: http://sun.library.msstate.edu/ETD-db/theses/available/etd-11092006-232711/ ;.

Council of Science Editors:

Mankada Covilakom MV. RANS AND HYBRID RANS/LES COMPUTATIONS FOR THREE-DIMENSIONAL WINGS WITH ICE ACCRETION. [Masters Thesis]. Mississippi State University; 2006. Available from: http://sun.library.msstate.edu/ETD-db/theses/available/etd-11092006-232711/ ;


Iowa State University

17. Zhang, Kai. An experimental study of wind-driven surface water transport process pertinent to aircraft icing.

Degree: 2015, Iowa State University

 Water transport behaviors will significantly influence the icing accretion process during glaze icing conditions. Many important micro-physical processes associated with water transport phenomena, such as… (more)

Subjects/Keywords: Aerospace Engineering; Aircraft icing; Digital image projection; film thickness; rivulet stagnation; trapped ratio; water transport; Aerospace Engineering

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APA (6th Edition):

Zhang, K. (2015). An experimental study of wind-driven surface water transport process pertinent to aircraft icing. (Thesis). Iowa State University. Retrieved from https://lib.dr.iastate.edu/etd/14465

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):

Zhang, Kai. “An experimental study of wind-driven surface water transport process pertinent to aircraft icing.” 2015. Thesis, Iowa State University. Accessed January 18, 2019. https://lib.dr.iastate.edu/etd/14465.

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

MLA Handbook (7th Edition):

Zhang, Kai. “An experimental study of wind-driven surface water transport process pertinent to aircraft icing.” 2015. Web. 18 Jan 2019.

Vancouver:

Zhang K. An experimental study of wind-driven surface water transport process pertinent to aircraft icing. [Internet] [Thesis]. Iowa State University; 2015. [cited 2019 Jan 18]. Available from: https://lib.dr.iastate.edu/etd/14465.

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

Council of Science Editors:

Zhang K. An experimental study of wind-driven surface water transport process pertinent to aircraft icing. [Thesis]. Iowa State University; 2015. Available from: https://lib.dr.iastate.edu/etd/14465

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

18. Soltis, Jared T. Design and Testing of an Erosion Resistant Ultrasonic De-icing System for Rotorcraft Blades.

Degree: MS, Aerospace Engineering, 2013, Penn State University

 The goal of this research was to design a helicopter rotor blade lead edge that had high sand erosion resistance and was conducive to ultrasonic… (more)

Subjects/Keywords: aircraft icing; de-icing systems; ice adhesion strength; ultrasonic de-icing; erosion resistant materials

…thereon. xv 1. Introduction 1.1. Icing Overview 1.1.1. Aircraft Ice Testing History… …Aircraft icing was not a concern for early aviators, mainly because the lack of technical… …problem of aircraft icing, the National Advisory Council for Aeronautics (NACA) began… …protection systems is recommended. 1.1.2. Ice Accretion Physics As aircraft fly through icing… …the aircraft is dependent upon a number of atmospheric conditions in the icing cloud and… 

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APA (6th Edition):

Soltis, J. T. (2013). Design and Testing of an Erosion Resistant Ultrasonic De-icing System for Rotorcraft Blades. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/19062

Chicago Manual of Style (16th Edition):

Soltis, Jared T. “Design and Testing of an Erosion Resistant Ultrasonic De-icing System for Rotorcraft Blades.” 2013. Masters Thesis, Penn State University. Accessed January 18, 2019. https://etda.libraries.psu.edu/catalog/19062.

MLA Handbook (7th Edition):

Soltis, Jared T. “Design and Testing of an Erosion Resistant Ultrasonic De-icing System for Rotorcraft Blades.” 2013. Web. 18 Jan 2019.

Vancouver:

Soltis JT. Design and Testing of an Erosion Resistant Ultrasonic De-icing System for Rotorcraft Blades. [Internet] [Masters thesis]. Penn State University; 2013. [cited 2019 Jan 18]. Available from: https://etda.libraries.psu.edu/catalog/19062.

Council of Science Editors:

Soltis JT. Design and Testing of an Erosion Resistant Ultrasonic De-icing System for Rotorcraft Blades. [Masters Thesis]. Penn State University; 2013. Available from: https://etda.libraries.psu.edu/catalog/19062

19. 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 January 18, 2019. 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. 18 Jan 2019.

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 2019 Jan 18]. 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


Uppsala University

20. Marklund, Lars. Flygplansavisningens miljöpåverkan vid svenska flygplatser.

Degree: Earth Sciences, 2004, Uppsala University

The aim of this thesis was to answer a number of questions about the environmental consequences of aircraft de-icing. A further aim was to… (more)

Subjects/Keywords: Aircraft de-icing; environmental impact; glycol; collection; BOD; TOC; MPG.; Environmental engineering; Miljöteknik

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APA (6th Edition):

Marklund, L. (2004). Flygplansavisningens miljöpåverkan vid svenska flygplatser. (Thesis). Uppsala University. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:uu:diva-88865

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):

Marklund, Lars. “Flygplansavisningens miljöpåverkan vid svenska flygplatser.” 2004. Thesis, Uppsala University. Accessed January 18, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:uu:diva-88865.

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

MLA Handbook (7th Edition):

Marklund, Lars. “Flygplansavisningens miljöpåverkan vid svenska flygplatser.” 2004. Web. 18 Jan 2019.

Vancouver:

Marklund L. Flygplansavisningens miljöpåverkan vid svenska flygplatser. [Internet] [Thesis]. Uppsala University; 2004. [cited 2019 Jan 18]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:uu:diva-88865.

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

Council of Science Editors:

Marklund L. Flygplansavisningens miljöpåverkan vid svenska flygplatser. [Thesis]. Uppsala University; 2004. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:uu:diva-88865

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


Brno University of Technology

21. Ryba, Přemysl. Bouřky na letištích LKTB a LKMT a jejich předpověď .

Degree: 2010, Brno University of Technology

 Tato bakalářská práce je zaměřena na nebezpečné jevy v letectví, na přítomnost bouřek v prostoru letišť Brno-Tuřany a Ostrava-Mošnov se zvláštním zřetelem na sledované období… (more)

Subjects/Keywords: Blesk; kumulonimbus; meteorologie letecká; námraza v letectví; propad studeného vzduchu; předpovídání bouřek; supercela; vznik bouřky; Aircraft icing; aeronautical meteorology; cumulonimbus; downburst; lightning; supercell; thunderstorm development; thunderstorm forecasting

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APA (6th Edition):

Ryba, P. (2010). Bouřky na letištích LKTB a LKMT a jejich předpověď . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/2450

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):

Ryba, Přemysl. “Bouřky na letištích LKTB a LKMT a jejich předpověď .” 2010. Thesis, Brno University of Technology. Accessed January 18, 2019. http://hdl.handle.net/11012/2450.

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

MLA Handbook (7th Edition):

Ryba, Přemysl. “Bouřky na letištích LKTB a LKMT a jejich předpověď .” 2010. Web. 18 Jan 2019.

Vancouver:

Ryba P. Bouřky na letištích LKTB a LKMT a jejich předpověď . [Internet] [Thesis]. Brno University of Technology; 2010. [cited 2019 Jan 18]. Available from: http://hdl.handle.net/11012/2450.

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

Council of Science Editors:

Ryba P. Bouřky na letištích LKTB a LKMT a jejich předpověď . [Thesis]. Brno University of Technology; 2010. Available from: http://hdl.handle.net/11012/2450

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


Iowa State University

22. 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 January 18, 2019. 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. 18 Jan 2019.

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 2019 Jan 18]. 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


Iowa State University

23. Otta, Shourya Prakash. Instability of stagnation and attachment line icing.

Degree: 2008, Iowa State University

 Ice accretion for in-flight icing conditions often yields complicated shapes which can significantly affect the performance of an aircraft. This has been a primary motivation… (more)

Subjects/Keywords: aircraft icing; ice surface instability; linear stability; multiple scales; Aerospace Engineering

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APA (6th Edition):

Otta, S. P. (2008). Instability of stagnation and attachment line icing. (Thesis). Iowa State University. Retrieved from https://lib.dr.iastate.edu/etd/11499

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):

Otta, Shourya Prakash. “Instability of stagnation and attachment line icing.” 2008. Thesis, Iowa State University. Accessed January 18, 2019. https://lib.dr.iastate.edu/etd/11499.

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

MLA Handbook (7th Edition):

Otta, Shourya Prakash. “Instability of stagnation and attachment line icing.” 2008. Web. 18 Jan 2019.

Vancouver:

Otta SP. Instability of stagnation and attachment line icing. [Internet] [Thesis]. Iowa State University; 2008. [cited 2019 Jan 18]. Available from: https://lib.dr.iastate.edu/etd/11499.

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

Council of Science Editors:

Otta SP. Instability of stagnation and attachment line icing. [Thesis]. Iowa State University; 2008. Available from: https://lib.dr.iastate.edu/etd/11499

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

24. Wiberg, Brock. Large-scale swept-wing ice accretion modeling in the NASA Glenn Icing Research Tunnel using LEWICE3D.

Degree: MS, 4048, 2014, University of Illinois – Urbana-Champaign

 The study of aircraft icing is necessary to ensure the safety of commercial, military, and general aviation aircraft. The certification of modern commercial transports requires… (more)

Subjects/Keywords: aircraft icing; icing; ice shape; Accretion; sweep; swept; wing; computational fluid dynamics (CFD); aircraft certification; hybrid; similitude

icing is critical to the safe operation of commercial, military, and general aviation aircraft… …on the structures of aircraft [1]. This first look at aircraft icing resulted… …aircraft. The need for a laboratory environment that would allow better control of icing… …better understand aircraft icing on large-scale, swept wings, NASA, the FAA, The French… …framework for aircraft manufacturers designing test articles for icing tunnel experiments. An… 

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APA (6th Edition):

Wiberg, B. (2014). Large-scale swept-wing ice accretion modeling in the NASA Glenn Icing Research Tunnel using LEWICE3D. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/46609

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):

Wiberg, Brock. “Large-scale swept-wing ice accretion modeling in the NASA Glenn Icing Research Tunnel using LEWICE3D.” 2014. Thesis, University of Illinois – Urbana-Champaign. Accessed January 18, 2019. http://hdl.handle.net/2142/46609.

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

MLA Handbook (7th Edition):

Wiberg, Brock. “Large-scale swept-wing ice accretion modeling in the NASA Glenn Icing Research Tunnel using LEWICE3D.” 2014. Web. 18 Jan 2019.

Vancouver:

Wiberg B. Large-scale swept-wing ice accretion modeling in the NASA Glenn Icing Research Tunnel using LEWICE3D. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2014. [cited 2019 Jan 18]. Available from: http://hdl.handle.net/2142/46609.

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

Council of Science Editors:

Wiberg B. Large-scale swept-wing ice accretion modeling in the NASA Glenn Icing Research Tunnel using LEWICE3D. [Thesis]. University of Illinois – Urbana-Champaign; 2014. Available from: http://hdl.handle.net/2142/46609

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

25. Camarinha Fujiwara, Gustavo. Design of 3D swept wing hybrid models for icing wind tunnel tests.

Degree: MS, 4048, 2015, University of Illinois – Urbana-Champaign

 The study of aircraft icing is critical to ensure the safety of any aircraft that might experience icing conditions in flight, including general, commercial, and… (more)

Subjects/Keywords: Aerodynamics; aircraft icing; wind tunnel; icing; ice shape; Accretion; hybrid; sweep; swept; wing; computational fluid dynamics (CFD); aircraft certification; wing design

…study of aircraft icing is a topic of major importance for the safety and operation of any… …aircraft that might experience icing conditions in flight, including general, commercial, and… …aircraft performance. To maintain altitude and counter the effects of drag during flight in icing… …research in aircraft icing began in 1928 at the National Advisory Committee for Aeronautics (… …aircraft structures [5]. This was motivated by the frequent icing encounters… 

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APA (6th Edition):

Camarinha Fujiwara, G. (2015). Design of 3D swept wing hybrid models for icing wind tunnel tests. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/72880

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):

Camarinha Fujiwara, Gustavo. “Design of 3D swept wing hybrid models for icing wind tunnel tests.” 2015. Thesis, University of Illinois – Urbana-Champaign. Accessed January 18, 2019. http://hdl.handle.net/2142/72880.

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

MLA Handbook (7th Edition):

Camarinha Fujiwara, Gustavo. “Design of 3D swept wing hybrid models for icing wind tunnel tests.” 2015. Web. 18 Jan 2019.

Vancouver:

Camarinha Fujiwara G. Design of 3D swept wing hybrid models for icing wind tunnel tests. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2015. [cited 2019 Jan 18]. Available from: http://hdl.handle.net/2142/72880.

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

Council of Science Editors:

Camarinha Fujiwara G. Design of 3D swept wing hybrid models for icing wind tunnel tests. [Thesis]. University of Illinois – Urbana-Champaign; 2015. Available from: http://hdl.handle.net/2142/72880

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

26. Silva, Guilherme Araújo Lima da. Transferência de calor e massa no escoamento bifásico em torno de aerofólios equipados com sistemas de antigelo aeronáuticos.

Degree: PhD, Engenharia Mecânica de Energia de Fluidos, 2009, University of São Paulo

Há a necessidade de prevenir formação de gelo nas asas e nos estabilizadores de aeronaves, pois as formas de gelo podem causar a degradação do… (more)

Subjects/Keywords: Aerodinâmica de aeronaves (simulação); Aircraft simulation; Anti-Ice; Boundary layer; Escoamento bifásico; Film breakdown; Heat transfer; Icing; Laminar turbulent transition; Mass transfer; Rivulets formation; Transferência de calor; Transferência de massa; Two-phase flow

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APA (6th Edition):

Silva, G. A. L. d. (2009). Transferência de calor e massa no escoamento bifásico em torno de aerofólios equipados com sistemas de antigelo aeronáuticos. (Doctoral Dissertation). University of São Paulo. Retrieved from http://www.teses.usp.br/teses/disponiveis/3/3150/tde-27032009-082825/ ;

Chicago Manual of Style (16th Edition):

Silva, Guilherme Araújo Lima da. “Transferência de calor e massa no escoamento bifásico em torno de aerofólios equipados com sistemas de antigelo aeronáuticos.” 2009. Doctoral Dissertation, University of São Paulo. Accessed January 18, 2019. http://www.teses.usp.br/teses/disponiveis/3/3150/tde-27032009-082825/ ;.

MLA Handbook (7th Edition):

Silva, Guilherme Araújo Lima da. “Transferência de calor e massa no escoamento bifásico em torno de aerofólios equipados com sistemas de antigelo aeronáuticos.” 2009. Web. 18 Jan 2019.

Vancouver:

Silva GALd. Transferência de calor e massa no escoamento bifásico em torno de aerofólios equipados com sistemas de antigelo aeronáuticos. [Internet] [Doctoral dissertation]. University of São Paulo; 2009. [cited 2019 Jan 18]. Available from: http://www.teses.usp.br/teses/disponiveis/3/3150/tde-27032009-082825/ ;.

Council of Science Editors:

Silva GALd. Transferência de calor e massa no escoamento bifásico em torno de aerofólios equipados com sistemas de antigelo aeronáuticos. [Doctoral Dissertation]. University of São Paulo; 2009. Available from: http://www.teses.usp.br/teses/disponiveis/3/3150/tde-27032009-082825/ ;

27. Liu, Yang. Experimental Investigations on Transient Surface Water Transport and Ice Accreting Processes Pertinent to Aircraft Icing Phenomena.

Degree: 2016, Iowa State University

 In the present study, an multi-transducer (sparse array) ultrasonic pulse-echo (MTUPE) technique was developed to quantify the transient surface behaviors of the water film flow… (more)

Subjects/Keywords: Aircraft icing; Heat transfer; Ice roughness; Ultrasonic Attenuation; Ultrasonic pulse-echo; Water transport; Aerospace Engineering

…important microphysical processes pertinent to aircraft icing phenomena to develop more effective… …and robust anti-/de-icing strategies to ensure safer and more efficient aircraft operations… …in cold weather. 1 CHAPTER 1 GENERAL INTRODUCTION 1.1 Literature Review Aircraft icing… …many efforts have been made to solve the icing problems, ice accretion on aircraft is still a… …aircraft wings, fuselage and control surfaces. Most of the in-flight aircraft icing events take… 

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APA (6th Edition):

Liu, Y. (2016). Experimental Investigations on Transient Surface Water Transport and Ice Accreting Processes Pertinent to Aircraft Icing Phenomena. (Thesis). Iowa State University. Retrieved from https://lib.dr.iastate.edu/etd/15748

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):

Liu, Yang. “Experimental Investigations on Transient Surface Water Transport and Ice Accreting Processes Pertinent to Aircraft Icing Phenomena.” 2016. Thesis, Iowa State University. Accessed January 18, 2019. https://lib.dr.iastate.edu/etd/15748.

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

MLA Handbook (7th Edition):

Liu, Yang. “Experimental Investigations on Transient Surface Water Transport and Ice Accreting Processes Pertinent to Aircraft Icing Phenomena.” 2016. Web. 18 Jan 2019.

Vancouver:

Liu Y. Experimental Investigations on Transient Surface Water Transport and Ice Accreting Processes Pertinent to Aircraft Icing Phenomena. [Internet] [Thesis]. Iowa State University; 2016. [cited 2019 Jan 18]. Available from: https://lib.dr.iastate.edu/etd/15748.

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

Council of Science Editors:

Liu Y. Experimental Investigations on Transient Surface Water Transport and Ice Accreting Processes Pertinent to Aircraft Icing Phenomena. [Thesis]. Iowa State University; 2016. Available from: https://lib.dr.iastate.edu/etd/15748

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

28. Ansell, Phillip J. Unsteady modes in the flowfield about an airfoil with a leading-edge horn-ice shape.

Degree: PhD, 4048, 2014, University of Illinois – Urbana-Champaign

 An analysis of unsteady modes present in the flowfield of an airfoil with a leading-edge horn-ice shape was performed in the current study. An NACA… (more)

Subjects/Keywords: airfoil; icing; ice accretion; flowfield unsteadiness; shear-layer flapping; vortex shedding; aircraft; separation bubble; separated flow; airfoil circulation; Strouhal number; shear-layer reattachment; stall; unsteady flow

…flight hazard that has persisted since the inception of aviation is airframe icing. Aircraft… …icing can occur on the ground prior to takeoff if the aircraft is exposed to freezing… …precipitation, but icing can also occur in flight as the aircraft flies through clouds of water… …Extended exposure to icing conditions can cause ice to accrete on the aircraft surface in various… …aviation technology has been swiftly advancing. While the aircraft of today become increasingly… 

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APA (6th Edition):

Ansell, P. J. (2014). Unsteady modes in the flowfield about an airfoil with a leading-edge horn-ice shape. (Doctoral Dissertation). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/46620

Chicago Manual of Style (16th Edition):

Ansell, Phillip J. “Unsteady modes in the flowfield about an airfoil with a leading-edge horn-ice shape.” 2014. Doctoral Dissertation, University of Illinois – Urbana-Champaign. Accessed January 18, 2019. http://hdl.handle.net/2142/46620.

MLA Handbook (7th Edition):

Ansell, Phillip J. “Unsteady modes in the flowfield about an airfoil with a leading-edge horn-ice shape.” 2014. Web. 18 Jan 2019.

Vancouver:

Ansell PJ. Unsteady modes in the flowfield about an airfoil with a leading-edge horn-ice shape. [Internet] [Doctoral dissertation]. University of Illinois – Urbana-Champaign; 2014. [cited 2019 Jan 18]. Available from: http://hdl.handle.net/2142/46620.

Council of Science Editors:

Ansell PJ. Unsteady modes in the flowfield about an airfoil with a leading-edge horn-ice shape. [Doctoral Dissertation]. University of Illinois – Urbana-Champaign; 2014. Available from: http://hdl.handle.net/2142/46620

29. Silva, Guilherme Araújo Lima da. Modelagem e simulação da operação de sistema antigelo eletrotérmico de um aerofólio.

Degree: Mestrado, Engenharia Mecânica, 2002, University of São Paulo

No presente trabalho foi implementado um modelo matemático para simular o sistema antigelo eletrotérmico de um aerofólio. Por meio do programa ONERA2D simulou-se o escoamento… (more)

Subjects/Keywords: Aerofólios; Aeronaves; Aircraft; Airfoil; Anti-ice; Antigelo; Boundary layer; Camada limite; Formação de gelo; Heat transfer; Ice protection; Icing; Laminar-turbulent transition; Mass transfer; Proteção contra gelo; Simulação térmica; Thermal simulation; Transferência de calor; Transferência de massa; Transição laminar-turbulenta

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

APA (6th Edition):

Silva, G. A. L. d. (2002). Modelagem e simulação da operação de sistema antigelo eletrotérmico de um aerofólio. (Masters Thesis). University of São Paulo. Retrieved from http://www.teses.usp.br/teses/disponiveis/3/3132/tde-19092007-000212/ ;

Chicago Manual of Style (16th Edition):

Silva, Guilherme Araújo Lima da. “Modelagem e simulação da operação de sistema antigelo eletrotérmico de um aerofólio.” 2002. Masters Thesis, University of São Paulo. Accessed January 18, 2019. http://www.teses.usp.br/teses/disponiveis/3/3132/tde-19092007-000212/ ;.

MLA Handbook (7th Edition):

Silva, Guilherme Araújo Lima da. “Modelagem e simulação da operação de sistema antigelo eletrotérmico de um aerofólio.” 2002. Web. 18 Jan 2019.

Vancouver:

Silva GALd. Modelagem e simulação da operação de sistema antigelo eletrotérmico de um aerofólio. [Internet] [Masters thesis]. University of São Paulo; 2002. [cited 2019 Jan 18]. Available from: http://www.teses.usp.br/teses/disponiveis/3/3132/tde-19092007-000212/ ;.

Council of Science Editors:

Silva GALd. Modelagem e simulação da operação de sistema antigelo eletrotérmico de um aerofólio. [Masters Thesis]. University of São Paulo; 2002. Available from: http://www.teses.usp.br/teses/disponiveis/3/3132/tde-19092007-000212/ ;

.