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You searched for subject:(aircraft icing). Showing records 1 – 30 of 37 total matches.

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Baylor University

1. Shannon, Timothy Andrew, 1991-. Convection from realistic ice roughness on a simulated NACA 0012 airfoil.

Degree: M.S.M.E., Baylor University. School of Engineering., 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 (6th Edition):

Shannon, Timothy Andrew, 1. (2015). Convection from realistic ice roughness on a simulated NACA 0012 airfoil. (Masters Thesis). Baylor University. Retrieved from http://hdl.handle.net/2104/9534

Chicago Manual of Style (16th Edition):

Shannon, Timothy Andrew, 1991-. “Convection from realistic ice roughness on a simulated NACA 0012 airfoil.” 2015. Masters Thesis, Baylor University. Accessed January 25, 2021. http://hdl.handle.net/2104/9534.

MLA Handbook (7th Edition):

Shannon, Timothy Andrew, 1991-. “Convection from realistic ice roughness on a simulated NACA 0012 airfoil.” 2015. Web. 25 Jan 2021.

Vancouver:

Shannon, Timothy Andrew 1. Convection from realistic ice roughness on a simulated NACA 0012 airfoil. [Internet] [Masters thesis]. Baylor University; 2015. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/2104/9534.

Council of Science Editors:

Shannon, Timothy Andrew 1. Convection from realistic ice roughness on a simulated NACA 0012 airfoil. [Masters Thesis]. Baylor University; 2015. Available from: http://hdl.handle.net/2104/9534


Brno University of Technology

2. Fazekaš, Slavomír. Odmrazovací soustavy letadel: Aircraft de-icing systems.

Degree: 2018, Brno University of Technology

 The aim of my bachelor thesis is to make the acquaintance of the danger of ice coating on airplanes, it s creation and the way… (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. (2018). Odmrazovací soustavy letadel: Aircraft de-icing systems. (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: Aircraft de-icing systems.” 2018. Thesis, Brno University of Technology. Accessed January 25, 2021. 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: Aircraft de-icing systems.” 2018. Web. 25 Jan 2021.

Vancouver:

Fazekaš S. Odmrazovací soustavy letadel: Aircraft de-icing systems. [Internet] [Thesis]. Brno University of Technology; 2018. [cited 2021 Jan 25]. 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: Aircraft de-icing systems. [Thesis]. Brno University of Technology; 2018. 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


Penn State University

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

Degree: 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

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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. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/19062

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):

Soltis, Jared T. “Design and Testing of an Erosion Resistant Ultrasonic De-icing System for Rotorcraft Blades.” 2013. Thesis, Penn State University. Accessed January 25, 2021. https://submit-etda.libraries.psu.edu/catalog/19062.

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

MLA Handbook (7th Edition):

Soltis, Jared T. “Design and Testing of an Erosion Resistant Ultrasonic De-icing System for Rotorcraft Blades.” 2013. Web. 25 Jan 2021.

Vancouver:

Soltis JT. Design and Testing of an Erosion Resistant Ultrasonic De-icing System for Rotorcraft Blades. [Internet] [Thesis]. Penn State University; 2013. [cited 2021 Jan 25]. Available from: https://submit-etda.libraries.psu.edu/catalog/19062.

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

Council of Science Editors:

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

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: Aircraft de-icing systems.

Degree: 2019, Brno University of Technology

 The bachelor´s thesis is familiarization of me with icing on aircrafts. It includes the distribution systems for anti-icing and de-icing, energy intensity and efficiency are… (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. (2019). Odmrazovací soustavy letadel: Aircraft de-icing systems. (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: Aircraft de-icing systems.” 2019. Thesis, Brno University of Technology. Accessed January 25, 2021. 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: Aircraft de-icing systems.” 2019. Web. 25 Jan 2021.

Vancouver:

Smékal A. Odmrazovací soustavy letadel: Aircraft de-icing systems. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Jan 25]. 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: Aircraft de-icing systems. [Thesis]. Brno University of Technology; 2019. 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 25, 2021. 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. 25 Jan 2021.

Vancouver:

Charpin JPF. Water flow on accreting ice surfaces. [Internet] [Doctoral dissertation]. Cranfield University; 2002. [cited 2021 Jan 25]. 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

6. Ma, Liqun. Experimental investigations on bio-inspired surface coatings for aircraft icing mitigation.

Degree: 2019, Iowa State University

Aircraft icing is widely recognized as a significant hazard to aircraft operations in cold weathers. Bio-inspired water- and ice-phobic coatings are currently being investigated for… (more)

Subjects/Keywords: Aircraft icing; Icephobic coatings; Aerospace Engineering

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APA (6th Edition):

Ma, L. (2019). Experimental investigations on bio-inspired surface coatings for aircraft icing mitigation. (Thesis). Iowa State University. Retrieved from https://lib.dr.iastate.edu/etd/17053

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):

Ma, Liqun. “Experimental investigations on bio-inspired surface coatings for aircraft icing mitigation.” 2019. Thesis, Iowa State University. Accessed January 25, 2021. https://lib.dr.iastate.edu/etd/17053.

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

MLA Handbook (7th Edition):

Ma, Liqun. “Experimental investigations on bio-inspired surface coatings for aircraft icing mitigation.” 2019. Web. 25 Jan 2021.

Vancouver:

Ma L. Experimental investigations on bio-inspired surface coatings for aircraft icing mitigation. [Internet] [Thesis]. Iowa State University; 2019. [cited 2021 Jan 25]. Available from: https://lib.dr.iastate.edu/etd/17053.

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

Council of Science Editors:

Ma L. Experimental investigations on bio-inspired surface coatings for aircraft icing mitigation. [Thesis]. Iowa State University; 2019. Available from: https://lib.dr.iastate.edu/etd/17053

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


Oklahoma State University

7. Avery, Alyssa Shearon. Ice Accretion on Small Unmanned Aircraft.

Degree: Mechanical and Aerospace Engineering, 2019, Oklahoma State University

Aircraft icing is an important and complex problem. Small unmanned aerial systems are becoming increasingly common in high quality operations. The hazards of icing on… (more)

Subjects/Keywords: aircraft icing; heat transfer; unmanned systems

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APA (6th Edition):

Avery, A. S. (2019). Ice Accretion on Small Unmanned Aircraft. (Thesis). Oklahoma State University. Retrieved from http://hdl.handle.net/11244/323357

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):

Avery, Alyssa Shearon. “Ice Accretion on Small Unmanned Aircraft.” 2019. Thesis, Oklahoma State University. Accessed January 25, 2021. http://hdl.handle.net/11244/323357.

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

MLA Handbook (7th Edition):

Avery, Alyssa Shearon. “Ice Accretion on Small Unmanned Aircraft.” 2019. Web. 25 Jan 2021.

Vancouver:

Avery AS. Ice Accretion on Small Unmanned Aircraft. [Internet] [Thesis]. Oklahoma State University; 2019. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/11244/323357.

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

Council of Science Editors:

Avery AS. Ice Accretion on Small Unmanned Aircraft. [Thesis]. Oklahoma State University; 2019. Available from: http://hdl.handle.net/11244/323357

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


Penn State University

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

Degree: 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 (6th Edition):

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

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):

Borigo, Cody J. “A Novel Actuator Phasing Method for Ultrasonic De-icing of Aircraft Structures.” 2014. Thesis, Penn State University. Accessed January 25, 2021. https://submit-etda.libraries.psu.edu/catalog/23379.

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

MLA Handbook (7th Edition):

Borigo, Cody J. “A Novel Actuator Phasing Method for Ultrasonic De-icing of Aircraft Structures.” 2014. Web. 25 Jan 2021.

Vancouver:

Borigo CJ. A Novel Actuator Phasing Method for Ultrasonic De-icing of Aircraft Structures. [Internet] [Thesis]. Penn State University; 2014. [cited 2021 Jan 25]. Available from: https://submit-etda.libraries.psu.edu/catalog/23379.

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

Council of Science Editors:

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

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


Iowa State University

9. Kolbakir, Cem. Experimental investigations on thermodynamic characteristics of DBD plasma and applications for aircraft icing mitigation.

Degree: 2019, Iowa State University

Aircraft icing is widely recognized as a significant hazard to aircraft operations. When an airplane flies in a cold climate, some of the super-cooled droplets… (more)

Subjects/Keywords: Aircraft Icing; Anti-Icing; DBD; Dielectric Barrier Discharge; Plasma Actuator; Aerospace Engineering

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APA (6th Edition):

Kolbakir, C. (2019). Experimental investigations on thermodynamic characteristics of DBD plasma and applications for aircraft icing mitigation. (Thesis). Iowa State University. Retrieved from https://lib.dr.iastate.edu/etd/17721

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):

Kolbakir, Cem. “Experimental investigations on thermodynamic characteristics of DBD plasma and applications for aircraft icing mitigation.” 2019. Thesis, Iowa State University. Accessed January 25, 2021. https://lib.dr.iastate.edu/etd/17721.

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

MLA Handbook (7th Edition):

Kolbakir, Cem. “Experimental investigations on thermodynamic characteristics of DBD plasma and applications for aircraft icing mitigation.” 2019. Web. 25 Jan 2021.

Vancouver:

Kolbakir C. Experimental investigations on thermodynamic characteristics of DBD plasma and applications for aircraft icing mitigation. [Internet] [Thesis]. Iowa State University; 2019. [cited 2021 Jan 25]. Available from: https://lib.dr.iastate.edu/etd/17721.

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

Council of Science Editors:

Kolbakir C. Experimental investigations on thermodynamic characteristics of DBD plasma and applications for aircraft icing mitigation. [Thesis]. Iowa State University; 2019. Available from: https://lib.dr.iastate.edu/etd/17721

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


Baylor University

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

Degree: M.S.M.E., 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. (Masters Thesis). Baylor University. Retrieved from http://hdl.handle.net/2104/8757

Chicago Manual of Style (16th Edition):

Tecson, Joshua Logan. “Convective heat transfer from realistic ice roughness distributions.” 2013. Masters Thesis, Baylor University. Accessed January 25, 2021. http://hdl.handle.net/2104/8757.

MLA Handbook (7th Edition):

Tecson, Joshua Logan. “Convective heat transfer from realistic ice roughness distributions.” 2013. Web. 25 Jan 2021.

Vancouver:

Tecson JL. Convective heat transfer from realistic ice roughness distributions. [Internet] [Masters thesis]. Baylor University; 2013. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/2104/8757.

Council of Science Editors:

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

11. 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 25, 2021. 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. 25 Jan 2021.

Vancouver:

Triphahn C. Lagrangian Parcel Volume method applied to icing surfaces to predict impact efficiency. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2012. [cited 2021 Jan 25]. 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


University of Minnesota

12. Hooshanginejad, Alireza. Hydrodynamics Of Droplets In High-Reynolds-Number Flow Regimes.

Degree: PhD, Mechanical Engineering, 2020, University of Minnesota

 Partially wetting water droplets that run on a surface under wind are ubiquitous in nature. Despite its ubiquity, predicting a droplet's response to a high… (more)

Subjects/Keywords: aircraft icing; Droplet Stability; Lubrication Equation; Multiphase Flow

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APA (6th Edition):

Hooshanginejad, A. (2020). Hydrodynamics Of Droplets In High-Reynolds-Number Flow Regimes. (Doctoral Dissertation). University of Minnesota. Retrieved from http://hdl.handle.net/11299/215183

Chicago Manual of Style (16th Edition):

Hooshanginejad, Alireza. “Hydrodynamics Of Droplets In High-Reynolds-Number Flow Regimes.” 2020. Doctoral Dissertation, University of Minnesota. Accessed January 25, 2021. http://hdl.handle.net/11299/215183.

MLA Handbook (7th Edition):

Hooshanginejad, Alireza. “Hydrodynamics Of Droplets In High-Reynolds-Number Flow Regimes.” 2020. Web. 25 Jan 2021.

Vancouver:

Hooshanginejad A. Hydrodynamics Of Droplets In High-Reynolds-Number Flow Regimes. [Internet] [Doctoral dissertation]. University of Minnesota; 2020. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/11299/215183.

Council of Science Editors:

Hooshanginejad A. Hydrodynamics Of Droplets In High-Reynolds-Number Flow Regimes. [Doctoral Dissertation]. University of Minnesota; 2020. Available from: http://hdl.handle.net/11299/215183


Brno University of Technology

13. Zima, Martin. CFD analýza tvorby námrazy na letounu kategorie commuter: CFD analysis of icing effects on commuter aircraft configuration.

Degree: 2019, Brno University of Technology

 The Diploma Thesis concerns investigation of icing effects at L 410 NG aircraft. The aircraft is certified under FAR/CS/AP-23 Commuter category. An analysis was performed… (more)

Subjects/Keywords: CFD analýza; FENSAP-ICE; námraza v letectví; pneumatický odledňovací systém; CFD analysis; FENSAP-ICE; aircraft icing; Pneumatic De-icing Boots System

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APA (6th Edition):

Zima, M. (2019). CFD analýza tvorby námrazy na letounu kategorie commuter: CFD analysis of icing effects on commuter aircraft configuration. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/175530

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):

Zima, Martin. “CFD analýza tvorby námrazy na letounu kategorie commuter: CFD analysis of icing effects on commuter aircraft configuration.” 2019. Thesis, Brno University of Technology. Accessed January 25, 2021. http://hdl.handle.net/11012/175530.

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

MLA Handbook (7th Edition):

Zima, Martin. “CFD analýza tvorby námrazy na letounu kategorie commuter: CFD analysis of icing effects on commuter aircraft configuration.” 2019. Web. 25 Jan 2021.

Vancouver:

Zima M. CFD analýza tvorby námrazy na letounu kategorie commuter: CFD analysis of icing effects on commuter aircraft configuration. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/11012/175530.

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

Council of Science Editors:

Zima M. CFD analýza tvorby námrazy na letounu kategorie commuter: CFD analysis of icing effects on commuter aircraft configuration. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/175530

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


University of Dayton

14. Insana, Eric J. Low Reynolds Number Experimental Aerodynamic Verification of Scaled and LEWICE Simulated Ice Accretions in SLD Conditions.

Degree: MS(M.S.), Aerospace Engineering, 2020, University of Dayton

 Ice accretion is a primary operational flight hazard for which all FAA certified aircraft are evaluated. Due to the geometric limitation of icing research tunnels… (more)

Subjects/Keywords: Aerospace Engineering; Aircraft Icing, SLD, Supercooled Large Drop, LEWICE, Ice Shape Scaling, Low Reynolds Number Icing

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APA (6th Edition):

Insana, E. J. (2020). Low Reynolds Number Experimental Aerodynamic Verification of Scaled and LEWICE Simulated Ice Accretions in SLD Conditions. (Masters Thesis). University of Dayton. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=dayton1597082782224451

Chicago Manual of Style (16th Edition):

Insana, Eric J. “Low Reynolds Number Experimental Aerodynamic Verification of Scaled and LEWICE Simulated Ice Accretions in SLD Conditions.” 2020. Masters Thesis, University of Dayton. Accessed January 25, 2021. http://rave.ohiolink.edu/etdc/view?acc_num=dayton1597082782224451.

MLA Handbook (7th Edition):

Insana, Eric J. “Low Reynolds Number Experimental Aerodynamic Verification of Scaled and LEWICE Simulated Ice Accretions in SLD Conditions.” 2020. Web. 25 Jan 2021.

Vancouver:

Insana EJ. Low Reynolds Number Experimental Aerodynamic Verification of Scaled and LEWICE Simulated Ice Accretions in SLD Conditions. [Internet] [Masters thesis]. University of Dayton; 2020. [cited 2021 Jan 25]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=dayton1597082782224451.

Council of Science Editors:

Insana EJ. Low Reynolds Number Experimental Aerodynamic Verification of Scaled and LEWICE Simulated Ice Accretions in SLD Conditions. [Masters Thesis]. University of Dayton; 2020. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=dayton1597082782224451


Università degli studi di Bergamo

15. 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 25, 2021. 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. 25 Jan 2021.

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 2021 Jan 25]. 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


Penn State University

16. Rocco, Edward Thomas. 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 the ice accretion… (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. T. (2017). Super-cooled Large Droplet Experimental Reproduction, Ice Shape Modeling, and Scaling Law Assessment. (Thesis). Penn State University. Retrieved from https://submit-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 Thomas. “Super-cooled Large Droplet Experimental Reproduction, Ice Shape Modeling, and Scaling Law Assessment.” 2017. Thesis, Penn State University. Accessed January 25, 2021. https://submit-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 Thomas. “Super-cooled Large Droplet Experimental Reproduction, Ice Shape Modeling, and Scaling Law Assessment.” 2017. Web. 25 Jan 2021.

Vancouver:

Rocco ET. Super-cooled Large Droplet Experimental Reproduction, Ice Shape Modeling, and Scaling Law Assessment. [Internet] [Thesis]. Penn State University; 2017. [cited 2021 Jan 25]. Available from: https://submit-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 ET. Super-cooled Large Droplet Experimental Reproduction, Ice Shape Modeling, and Scaling Law Assessment. [Thesis]. Penn State University; 2017. Available from: https://submit-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


Penn State University

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

Degree: 2016, 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. (2016). Aerodynamics and Thermal Physics of Helicopter Ice Accretion. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/28036

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):

Han, Yiqiang. “Aerodynamics and Thermal Physics of Helicopter Ice Accretion.” 2016. Thesis, Penn State University. Accessed January 25, 2021. https://submit-etda.libraries.psu.edu/catalog/28036.

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

MLA Handbook (7th Edition):

Han, Yiqiang. “Aerodynamics and Thermal Physics of Helicopter Ice Accretion.” 2016. Web. 25 Jan 2021.

Vancouver:

Han Y. Aerodynamics and Thermal Physics of Helicopter Ice Accretion. [Internet] [Thesis]. Penn State University; 2016. [cited 2021 Jan 25]. Available from: https://submit-etda.libraries.psu.edu/catalog/28036.

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

Council of Science Editors:

Han Y. Aerodynamics and Thermal Physics of Helicopter Ice Accretion. [Thesis]. Penn State University; 2016. Available from: https://submit-etda.libraries.psu.edu/catalog/28036

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


Baylor University

18. Hughes, Michael T., 1991-. Convective enhancement on airfoils due to ice roughness elements in stagnation region flows.

Degree: M.S.M.E., Baylor University. School of Engineering., 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):

Hughes, Michael T., 1. (2015). Convective enhancement on airfoils due to ice roughness elements in stagnation region flows. (Masters Thesis). Baylor University. Retrieved from http://hdl.handle.net/2104/9559

Chicago Manual of Style (16th Edition):

Hughes, Michael T., 1991-. “Convective enhancement on airfoils due to ice roughness elements in stagnation region flows.” 2015. Masters Thesis, Baylor University. Accessed January 25, 2021. http://hdl.handle.net/2104/9559.

MLA Handbook (7th Edition):

Hughes, Michael T., 1991-. “Convective enhancement on airfoils due to ice roughness elements in stagnation region flows.” 2015. Web. 25 Jan 2021.

Vancouver:

Hughes, Michael T. 1. Convective enhancement on airfoils due to ice roughness elements in stagnation region flows. [Internet] [Masters thesis]. Baylor University; 2015. [cited 2021 Jan 25]. Available from: http://hdl.handle.net/2104/9559.

Council of Science Editors:

Hughes, Michael T. 1. Convective enhancement on airfoils due to ice roughness elements in stagnation region flows. [Masters Thesis]. Baylor University; 2015. Available from: http://hdl.handle.net/2104/9559


University of Washington

19. 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 25, 2021. 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. 25 Jan 2021.

Vancouver:

Sandhu N. Aerodynamics of a Swept Wing With Simulated Scalloped Ice at Low Reynolds Number. [Internet] [Thesis]. University of Washington; 2018. [cited 2021 Jan 25]. 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


Delft University of Technology

20. Van Hauwermeiren, Amber (author). Studying Ice Nucleation and Freezing Front Propagation with Infrared and Laser Speckle Imaging.

Degree: 2018, Delft University of Technology

 Clear ice formation on aircraft is a large economic and safety problem. The phenomenon, also known as ‘freezing rain’, usually occurs when subcooled rain droplets… (more)

Subjects/Keywords: Anti-icing; Laser Speckle Imaging; Infrared Imaging; Hydrophobic-hydrophilic patterns; Aircraft; Clear ice

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APA (6th Edition):

Van Hauwermeiren, A. (. (2018). Studying Ice Nucleation and Freezing Front Propagation with Infrared and Laser Speckle Imaging. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:9d157356-a942-48b6-9d0a-301e689efc02

Chicago Manual of Style (16th Edition):

Van Hauwermeiren, Amber (author). “Studying Ice Nucleation and Freezing Front Propagation with Infrared and Laser Speckle Imaging.” 2018. Masters Thesis, Delft University of Technology. Accessed January 25, 2021. http://resolver.tudelft.nl/uuid:9d157356-a942-48b6-9d0a-301e689efc02.

MLA Handbook (7th Edition):

Van Hauwermeiren, Amber (author). “Studying Ice Nucleation and Freezing Front Propagation with Infrared and Laser Speckle Imaging.” 2018. Web. 25 Jan 2021.

Vancouver:

Van Hauwermeiren A(. Studying Ice Nucleation and Freezing Front Propagation with Infrared and Laser Speckle Imaging. [Internet] [Masters thesis]. Delft University of Technology; 2018. [cited 2021 Jan 25]. Available from: http://resolver.tudelft.nl/uuid:9d157356-a942-48b6-9d0a-301e689efc02.

Council of Science Editors:

Van Hauwermeiren A(. Studying Ice Nucleation and Freezing Front Propagation with Infrared and Laser Speckle Imaging. [Masters Thesis]. Delft University of Technology; 2018. Available from: http://resolver.tudelft.nl/uuid:9d157356-a942-48b6-9d0a-301e689efc02

21. 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 25, 2021. 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. 25 Jan 2021.

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 2021 Jan 25]. 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


Mississippi State University

22. 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 25, 2021. 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. 25 Jan 2021.

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 2021 Jan 25]. 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

23. 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 25, 2021. 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. 25 Jan 2021.

Vancouver:

Zhang K. An experimental study of wind-driven surface water transport process pertinent to aircraft icing. [Internet] [Thesis]. Iowa State University; 2015. [cited 2021 Jan 25]. 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


University of Colorado

24. 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 https://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 25, 2021. https://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. 25 Jan 2021.

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 2021 Jan 25]. Available from: https://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: https://scholar.colorado.edu/atoc_gradetds/62


Tampere University

25. Maly, Yahya. Cold Sprayed SLIPS Coatings: A pathway towards process optimization and icephobicity .

Degree: 2020, Tampere University

 Ice accretion is a major problem that causes economic loss, damages structure, impedes transports, and potentially leads to human injury and death. There is a… (more)

Subjects/Keywords: Icephobicity ; Aircraft icing ; Ice wind tunnel ; Anti-icing ; De-icing ; Passive anti-ice systems ; Icephobic coatings ; Sprayed coatings ; Hydrophobicity ; superhydrophobicity ; Nature-inspired technology ; Lotus Effect ; SLIPS ; Slippery Liquid Infused Porous Surfaces ; Thermal spraying technology ; Cold spraying of polymers ; Flame spraying ; Process development

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APA (6th Edition):

Maly, Y. (2020). Cold Sprayed SLIPS Coatings: A pathway towards process optimization and icephobicity . (Masters Thesis). Tampere University. Retrieved from https://trepo.tuni.fi/handle/10024/122358

Chicago Manual of Style (16th Edition):

Maly, Yahya. “Cold Sprayed SLIPS Coatings: A pathway towards process optimization and icephobicity .” 2020. Masters Thesis, Tampere University. Accessed January 25, 2021. https://trepo.tuni.fi/handle/10024/122358.

MLA Handbook (7th Edition):

Maly, Yahya. “Cold Sprayed SLIPS Coatings: A pathway towards process optimization and icephobicity .” 2020. Web. 25 Jan 2021.

Vancouver:

Maly Y. Cold Sprayed SLIPS Coatings: A pathway towards process optimization and icephobicity . [Internet] [Masters thesis]. Tampere University; 2020. [cited 2021 Jan 25]. Available from: https://trepo.tuni.fi/handle/10024/122358.

Council of Science Editors:

Maly Y. Cold Sprayed SLIPS Coatings: A pathway towards process optimization and icephobicity . [Masters Thesis]. Tampere University; 2020. Available from: https://trepo.tuni.fi/handle/10024/122358

26. 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 25, 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. 25 Jan 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 Jan 25]. 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


Iowa State University

27. 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 25, 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. 25 Jan 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 Jan 25]. 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


Uppsala University

28. 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 25, 2021. 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. 25 Jan 2021.

Vancouver:

Marklund L. Flygplansavisningens miljöpåverkan vid svenska flygplatser. [Internet] [Thesis]. Uppsala University; 2004. [cited 2021 Jan 25]. 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


Iowa State University

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

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 25, 2021. 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. 25 Jan 2021.

Vancouver:

Otta SP. Instability of stagnation and attachment line icing. [Internet] [Thesis]. Iowa State University; 2008. [cited 2021 Jan 25]. 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


Brno University of Technology

30. Ryba, Přemysl. Bouřky na letištích LKTB a LKMT a jejich předpověď: The forecast of thunderstorm on the airports LKTB and LKMT.

Degree: 2018, Brno University of Technology

This bachelor’s thesis is focused on hazardous atmospheric phenomena namely presence of thunderstorms in Brno-Turany and Ostrava-Mosnov aerodrome area and it’s forecasting. Extra care is taken for observed period since 2005 till 2009. Advisors/Committee Members: Krška, Karel (advisor), Hudec, František (referee).

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

APA (6th Edition):

Ryba, P. (2018). Bouřky na letištích LKTB a LKMT a jejich předpověď: The forecast of thunderstorm on the airports LKTB and LKMT. (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: The forecast of thunderstorm on the airports LKTB and LKMT.” 2018. Thesis, Brno University of Technology. Accessed January 25, 2021. 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: The forecast of thunderstorm on the airports LKTB and LKMT.” 2018. Web. 25 Jan 2021.

Vancouver:

Ryba P. Bouřky na letištích LKTB a LKMT a jejich předpověď: The forecast of thunderstorm on the airports LKTB and LKMT. [Internet] [Thesis]. Brno University of Technology; 2018. [cited 2021 Jan 25]. 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: The forecast of thunderstorm on the airports LKTB and LKMT. [Thesis]. Brno University of Technology; 2018. 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

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