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You searched for subject:(Flutter). Showing records 1 – 30 of 219 total matches.

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1. Paulo, Luís António Dias. A preliminary study on passive and active flutter suppression concepts for aeronautical components.

Degree: 2009, RCAAP

 The scope of this work is to study computationally both passive and active flutter suppression characteristics of a cantilever cork agglomerate core sandwich with CFRP… (more)

Subjects/Keywords: Flutter; Flutter - Aglomerado de cortiça; Aeroelasticidade; Piezoeléctrico

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

APA (6th Edition):

Paulo, L. A. D. (2009). A preliminary study on passive and active flutter suppression concepts for aeronautical components. (Thesis). RCAAP. Retrieved from https://www.rcaap.pt/detail.jsp?id=oai:ubibliorum.ubi.pt:10400.6/3660

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):

Paulo, Luís António Dias. “A preliminary study on passive and active flutter suppression concepts for aeronautical components.” 2009. Thesis, RCAAP. Accessed November 12, 2019. https://www.rcaap.pt/detail.jsp?id=oai:ubibliorum.ubi.pt:10400.6/3660.

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

MLA Handbook (7th Edition):

Paulo, Luís António Dias. “A preliminary study on passive and active flutter suppression concepts for aeronautical components.” 2009. Web. 12 Nov 2019.

Vancouver:

Paulo LAD. A preliminary study on passive and active flutter suppression concepts for aeronautical components. [Internet] [Thesis]. RCAAP; 2009. [cited 2019 Nov 12]. Available from: https://www.rcaap.pt/detail.jsp?id=oai:ubibliorum.ubi.pt:10400.6/3660.

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

Council of Science Editors:

Paulo LAD. A preliminary study on passive and active flutter suppression concepts for aeronautical components. [Thesis]. RCAAP; 2009. Available from: https://www.rcaap.pt/detail.jsp?id=oai:ubibliorum.ubi.pt:10400.6/3660

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


Brno University of Technology

2. Zíka, Jakub. Návrh modelu křídla pro zkoušení flutteru .

Degree: 2018, Brno University of Technology

 Bakalářská práce se zabývá konstrukčním návrhem modelu křídla pro zkoušení dynamického aeroelastického jevu flutteru. První dvě teoreticky zaměřené kapitoly vysvětlují problematiku aeroelastických jevů a teorii… (more)

Subjects/Keywords: flutter; měřítko; model; flutter; scale; model

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APA (6th Edition):

Zíka, J. (2018). Návrh modelu křídla pro zkoušení flutteru . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/81666

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):

Zíka, Jakub. “Návrh modelu křídla pro zkoušení flutteru .” 2018. Thesis, Brno University of Technology. Accessed November 12, 2019. http://hdl.handle.net/11012/81666.

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

MLA Handbook (7th Edition):

Zíka, Jakub. “Návrh modelu křídla pro zkoušení flutteru .” 2018. Web. 12 Nov 2019.

Vancouver:

Zíka J. Návrh modelu křídla pro zkoušení flutteru . [Internet] [Thesis]. Brno University of Technology; 2018. [cited 2019 Nov 12]. Available from: http://hdl.handle.net/11012/81666.

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

Council of Science Editors:

Zíka J. Návrh modelu křídla pro zkoušení flutteru . [Thesis]. Brno University of Technology; 2018. Available from: http://hdl.handle.net/11012/81666

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


The Ohio State University

3. Sutton, Matthew Albert. Matrix methods of aircraft flutter analysis.

Degree: PhD, Graduate School, 1958, The Ohio State University

Subjects/Keywords: Engineering; Flutter

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APA (6th Edition):

Sutton, M. A. (1958). Matrix methods of aircraft flutter analysis. (Doctoral Dissertation). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1486470182523314

Chicago Manual of Style (16th Edition):

Sutton, Matthew Albert. “Matrix methods of aircraft flutter analysis.” 1958. Doctoral Dissertation, The Ohio State University. Accessed November 12, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=osu1486470182523314.

MLA Handbook (7th Edition):

Sutton, Matthew Albert. “Matrix methods of aircraft flutter analysis.” 1958. Web. 12 Nov 2019.

Vancouver:

Sutton MA. Matrix methods of aircraft flutter analysis. [Internet] [Doctoral dissertation]. The Ohio State University; 1958. [cited 2019 Nov 12]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1486470182523314.

Council of Science Editors:

Sutton MA. Matrix methods of aircraft flutter analysis. [Doctoral Dissertation]. The Ohio State University; 1958. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1486470182523314


Texas A&M University

4. Suryakumar, Vishvas Samuel. Fly-by-Feel Aeroservoelasticity.

Degree: 2016, Texas A&M University

 Recent experiments have suggested a strong correlation between local flow features on the airfoil surface such as the leading edge stagnation point (LESP), transition or… (more)

Subjects/Keywords: Aeroservoelasticity; Unsteady Aerodynamics; Flutter Suppression

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APA (6th Edition):

Suryakumar, V. S. (2016). Fly-by-Feel Aeroservoelasticity. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/159084

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):

Suryakumar, Vishvas Samuel. “Fly-by-Feel Aeroservoelasticity.” 2016. Thesis, Texas A&M University. Accessed November 12, 2019. http://hdl.handle.net/1969.1/159084.

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

MLA Handbook (7th Edition):

Suryakumar, Vishvas Samuel. “Fly-by-Feel Aeroservoelasticity.” 2016. Web. 12 Nov 2019.

Vancouver:

Suryakumar VS. Fly-by-Feel Aeroservoelasticity. [Internet] [Thesis]. Texas A&M University; 2016. [cited 2019 Nov 12]. Available from: http://hdl.handle.net/1969.1/159084.

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

Council of Science Editors:

Suryakumar VS. Fly-by-Feel Aeroservoelasticity. [Thesis]. Texas A&M University; 2016. Available from: http://hdl.handle.net/1969.1/159084

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


University of Hong Kong

5. Zhang, Chao. Cantilever plate flutter in wind tunnel tests and comparison with 2D theory.

Degree: PhD, 2015, University of Hong Kong

Cantilever plate flutter in axial flow has attracted more and more attention, as it is a typical model for the fluid-structure interaction which can be… (more)

Subjects/Keywords: Flutter (Aerodynamics); Wind tunnel models

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

APA (6th Edition):

Zhang, C. (2015). Cantilever plate flutter in wind tunnel tests and comparison with 2D theory. (Doctoral Dissertation). University of Hong Kong. Retrieved from Zhang, C. [張超]. (2015). Cantilever plate flutter in wind tunnel tests and comparison with 2D theory. (Thesis). University of Hong Kong, Pokfulam, Hong Kong SAR. Retrieved from http://dx.doi.org/10.5353/th_b5699944 ; http://hdl.handle.net/10722/223013

Chicago Manual of Style (16th Edition):

Zhang, Chao. “Cantilever plate flutter in wind tunnel tests and comparison with 2D theory.” 2015. Doctoral Dissertation, University of Hong Kong. Accessed November 12, 2019. Zhang, C. [張超]. (2015). Cantilever plate flutter in wind tunnel tests and comparison with 2D theory. (Thesis). University of Hong Kong, Pokfulam, Hong Kong SAR. Retrieved from http://dx.doi.org/10.5353/th_b5699944 ; http://hdl.handle.net/10722/223013.

MLA Handbook (7th Edition):

Zhang, Chao. “Cantilever plate flutter in wind tunnel tests and comparison with 2D theory.” 2015. Web. 12 Nov 2019.

Vancouver:

Zhang C. Cantilever plate flutter in wind tunnel tests and comparison with 2D theory. [Internet] [Doctoral dissertation]. University of Hong Kong; 2015. [cited 2019 Nov 12]. Available from: Zhang, C. [張超]. (2015). Cantilever plate flutter in wind tunnel tests and comparison with 2D theory. (Thesis). University of Hong Kong, Pokfulam, Hong Kong SAR. Retrieved from http://dx.doi.org/10.5353/th_b5699944 ; http://hdl.handle.net/10722/223013.

Council of Science Editors:

Zhang C. Cantilever plate flutter in wind tunnel tests and comparison with 2D theory. [Doctoral Dissertation]. University of Hong Kong; 2015. Available from: Zhang, C. [張超]. (2015). Cantilever plate flutter in wind tunnel tests and comparison with 2D theory. (Thesis). University of Hong Kong, Pokfulam, Hong Kong SAR. Retrieved from http://dx.doi.org/10.5353/th_b5699944 ; http://hdl.handle.net/10722/223013


UCLA

6. Mellquist, Erik Charles. Computational Transonic Flutter Solutions for Cranked Wings by the Direct Eulerian-Lagrangian Method.

Degree: Aerospace Engineering, 2014, UCLA

 In this dissertation, a three-dimensional computational aeroelastic simulation for cranked, highly-swept wings is developed, and solutions are presented for several wing models. The computational model… (more)

Subjects/Keywords: Aerospace engineering; aeroelasticity; flutter; transonic

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APA (6th Edition):

Mellquist, E. C. (2014). Computational Transonic Flutter Solutions for Cranked Wings by the Direct Eulerian-Lagrangian Method. (Thesis). UCLA. Retrieved from http://www.escholarship.org/uc/item/9rk54186

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):

Mellquist, Erik Charles. “Computational Transonic Flutter Solutions for Cranked Wings by the Direct Eulerian-Lagrangian Method.” 2014. Thesis, UCLA. Accessed November 12, 2019. http://www.escholarship.org/uc/item/9rk54186.

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

MLA Handbook (7th Edition):

Mellquist, Erik Charles. “Computational Transonic Flutter Solutions for Cranked Wings by the Direct Eulerian-Lagrangian Method.” 2014. Web. 12 Nov 2019.

Vancouver:

Mellquist EC. Computational Transonic Flutter Solutions for Cranked Wings by the Direct Eulerian-Lagrangian Method. [Internet] [Thesis]. UCLA; 2014. [cited 2019 Nov 12]. Available from: http://www.escholarship.org/uc/item/9rk54186.

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

Council of Science Editors:

Mellquist EC. Computational Transonic Flutter Solutions for Cranked Wings by the Direct Eulerian-Lagrangian Method. [Thesis]. UCLA; 2014. Available from: http://www.escholarship.org/uc/item/9rk54186

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

7. Pereira, Angelique Pinto. Estudo preliminar da supressão de flutter em componentes aeronáuticos.

Degree: 2009, RCAAP

 As instabilidades aeroelásticas são um dos principais factores que restringem o envelope de voo de uma aeronave. Um dos principais fenómenos aeroelásticos na aeronáutica é… (more)

Subjects/Keywords: Aeronáutica; Aeronáutica - Supressão de flutter

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APA (6th Edition):

Pereira, A. P. (2009). Estudo preliminar da supressão de flutter em componentes aeronáuticos. (Thesis). RCAAP. Retrieved from http://www.rcaap.pt/detail.jsp?id=oai:ubibliorum.ubi.pt:10400.6/3630

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):

Pereira, Angelique Pinto. “Estudo preliminar da supressão de flutter em componentes aeronáuticos.” 2009. Thesis, RCAAP. Accessed November 12, 2019. http://www.rcaap.pt/detail.jsp?id=oai:ubibliorum.ubi.pt:10400.6/3630.

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

MLA Handbook (7th Edition):

Pereira, Angelique Pinto. “Estudo preliminar da supressão de flutter em componentes aeronáuticos.” 2009. Web. 12 Nov 2019.

Vancouver:

Pereira AP. Estudo preliminar da supressão de flutter em componentes aeronáuticos. [Internet] [Thesis]. RCAAP; 2009. [cited 2019 Nov 12]. Available from: http://www.rcaap.pt/detail.jsp?id=oai:ubibliorum.ubi.pt:10400.6/3630.

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

Council of Science Editors:

Pereira AP. Estudo preliminar da supressão de flutter em componentes aeronáuticos. [Thesis]. RCAAP; 2009. Available from: http://www.rcaap.pt/detail.jsp?id=oai:ubibliorum.ubi.pt:10400.6/3630

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


KTH

8. Anchondo, Ruben Erives. Validation of non-linear time marching and time-linearised CFD solvers used for flutter prediction.

Degree: Heat and Power Technology, 2015, KTH

  The turbomachinery related industry relies heavily on numerical tools for the design and development of modern turbomachines. In order to be competitive turbomachines ought… (more)

Subjects/Keywords: Validation; flutter; linear; non-linear

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APA (6th Edition):

Anchondo, R. E. (2015). Validation of non-linear time marching and time-linearised CFD solvers used for flutter prediction. (Thesis). KTH. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-175542

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):

Anchondo, Ruben Erives. “Validation of non-linear time marching and time-linearised CFD solvers used for flutter prediction.” 2015. Thesis, KTH. Accessed November 12, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-175542.

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

MLA Handbook (7th Edition):

Anchondo, Ruben Erives. “Validation of non-linear time marching and time-linearised CFD solvers used for flutter prediction.” 2015. Web. 12 Nov 2019.

Vancouver:

Anchondo RE. Validation of non-linear time marching and time-linearised CFD solvers used for flutter prediction. [Internet] [Thesis]. KTH; 2015. [cited 2019 Nov 12]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-175542.

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

Council of Science Editors:

Anchondo RE. Validation of non-linear time marching and time-linearised CFD solvers used for flutter prediction. [Thesis]. KTH; 2015. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-175542

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

9. Bidinotto, Jorge Henrique. Proposta conceitual de excitador de \"flutter\" alternativo para ensaios em vôo.

Degree: Mestrado, Aeronaves, 2007, University of São Paulo

Os novos materiais utilizados nas estruturas de aeronaves, mais leves e flexíveis, tornam estas estruturas mais sujeitas a fenômenos aeroelásticos, sendo que o mais sério… (more)

Subjects/Keywords: Aeroelasticidade; Aeroelasticity; Ensaios em vôo; Excitador; Exciter; Flight test; Flutter; Flutter

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APA (6th Edition):

Bidinotto, J. H. (2007). Proposta conceitual de excitador de \"flutter\" alternativo para ensaios em vôo. (Masters Thesis). University of São Paulo. Retrieved from http://www.teses.usp.br/teses/disponiveis/18/18148/tde-27052009-142508/ ;

Chicago Manual of Style (16th Edition):

Bidinotto, Jorge Henrique. “Proposta conceitual de excitador de \"flutter\" alternativo para ensaios em vôo.” 2007. Masters Thesis, University of São Paulo. Accessed November 12, 2019. http://www.teses.usp.br/teses/disponiveis/18/18148/tde-27052009-142508/ ;.

MLA Handbook (7th Edition):

Bidinotto, Jorge Henrique. “Proposta conceitual de excitador de \"flutter\" alternativo para ensaios em vôo.” 2007. Web. 12 Nov 2019.

Vancouver:

Bidinotto JH. Proposta conceitual de excitador de \"flutter\" alternativo para ensaios em vôo. [Internet] [Masters thesis]. University of São Paulo; 2007. [cited 2019 Nov 12]. Available from: http://www.teses.usp.br/teses/disponiveis/18/18148/tde-27052009-142508/ ;.

Council of Science Editors:

Bidinotto JH. Proposta conceitual de excitador de \"flutter\" alternativo para ensaios em vôo. [Masters Thesis]. University of São Paulo; 2007. Available from: http://www.teses.usp.br/teses/disponiveis/18/18148/tde-27052009-142508/ ;

10. Costa, Tiago Francisco Gomes da. Estudo numérico de uma asa com controle ativo de flutter por realimentação da pressão medida num ponto.

Degree: Mestrado, Aeronaves, 2007, University of São Paulo

Neste trabalho é desenvolvido um sistema de controle ativo para supressão de flutter de uma asa utilizando-se sensores de pressão em pontos estratégicos de sua… (more)

Subjects/Keywords: Aerodinâmica não-estacionária; Aeroelasticidade; aeroelasticity; Aeroelasticity; Aeroservoelasticidade; aeroservoelasticity; Aeroservoelasticity; Flutter; Flutter; flutter suppression; Flutter suppression; non-stationary aerodynamics; Non-stationary aerodynamics; Supressão de flutter

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APA (6th Edition):

Costa, T. F. G. d. (2007). Estudo numérico de uma asa com controle ativo de flutter por realimentação da pressão medida num ponto. (Masters Thesis). University of São Paulo. Retrieved from http://www.teses.usp.br/teses/disponiveis/18/18148/tde-27112007-001723/ ;

Chicago Manual of Style (16th Edition):

Costa, Tiago Francisco Gomes da. “Estudo numérico de uma asa com controle ativo de flutter por realimentação da pressão medida num ponto.” 2007. Masters Thesis, University of São Paulo. Accessed November 12, 2019. http://www.teses.usp.br/teses/disponiveis/18/18148/tde-27112007-001723/ ;.

MLA Handbook (7th Edition):

Costa, Tiago Francisco Gomes da. “Estudo numérico de uma asa com controle ativo de flutter por realimentação da pressão medida num ponto.” 2007. Web. 12 Nov 2019.

Vancouver:

Costa TFGd. Estudo numérico de uma asa com controle ativo de flutter por realimentação da pressão medida num ponto. [Internet] [Masters thesis]. University of São Paulo; 2007. [cited 2019 Nov 12]. Available from: http://www.teses.usp.br/teses/disponiveis/18/18148/tde-27112007-001723/ ;.

Council of Science Editors:

Costa TFGd. Estudo numérico de uma asa com controle ativo de flutter por realimentação da pressão medida num ponto. [Masters Thesis]. University of São Paulo; 2007. Available from: http://www.teses.usp.br/teses/disponiveis/18/18148/tde-27112007-001723/ ;


Indian Institute of Science

11. Kumar, Brijesh. Flutter Susceptibility Assessment of Airplanes in Sub-critical Regime using Ameliorated Flutter Margin and Neural Network Based Methods.

Degree: 2014, Indian Institute of Science

 As flight flutter testing on an airplane progresses to high dynamic pressures and high Mach number region, it becomes very difficult for engineers to predict… (more)

Subjects/Keywords: Flight Flutter Tests (FFTs); Flutter Margin Method; Airplanes Flutter Susceptibility Assessment; Flight Flutter Testing; Aircraft Aeroelasticity; Computational Aeroelasticity Analysis; Ameliorated Flutter Margin; Flutter Susceptibility Assessment; Artificial Neural Network (ANN); Flutter Margin Prediction Equation (FMPE); Aerospace Engineering

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APA (6th Edition):

Kumar, B. (2014). Flutter Susceptibility Assessment of Airplanes in Sub-critical Regime using Ameliorated Flutter Margin and Neural Network Based Methods. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/3124

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):

Kumar, Brijesh. “Flutter Susceptibility Assessment of Airplanes in Sub-critical Regime using Ameliorated Flutter Margin and Neural Network Based Methods.” 2014. Thesis, Indian Institute of Science. Accessed November 12, 2019. http://hdl.handle.net/2005/3124.

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

MLA Handbook (7th Edition):

Kumar, Brijesh. “Flutter Susceptibility Assessment of Airplanes in Sub-critical Regime using Ameliorated Flutter Margin and Neural Network Based Methods.” 2014. Web. 12 Nov 2019.

Vancouver:

Kumar B. Flutter Susceptibility Assessment of Airplanes in Sub-critical Regime using Ameliorated Flutter Margin and Neural Network Based Methods. [Internet] [Thesis]. Indian Institute of Science; 2014. [cited 2019 Nov 12]. Available from: http://hdl.handle.net/2005/3124.

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

Council of Science Editors:

Kumar B. Flutter Susceptibility Assessment of Airplanes in Sub-critical Regime using Ameliorated Flutter Margin and Neural Network Based Methods. [Thesis]. Indian Institute of Science; 2014. Available from: http://hdl.handle.net/2005/3124

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


The Ohio State University

12. Dale, Ralph Gibson. Flutter analysis of an airfoil exhibiting camber deformations.

Degree: PhD, Graduate School, 1964, The Ohio State University

Subjects/Keywords: Engineering; Aerofoils; Flutter

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

APA (6th Edition):

Dale, R. G. (1964). Flutter analysis of an airfoil exhibiting camber deformations. (Doctoral Dissertation). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1486564960924631

Chicago Manual of Style (16th Edition):

Dale, Ralph Gibson. “Flutter analysis of an airfoil exhibiting camber deformations.” 1964. Doctoral Dissertation, The Ohio State University. Accessed November 12, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=osu1486564960924631.

MLA Handbook (7th Edition):

Dale, Ralph Gibson. “Flutter analysis of an airfoil exhibiting camber deformations.” 1964. Web. 12 Nov 2019.

Vancouver:

Dale RG. Flutter analysis of an airfoil exhibiting camber deformations. [Internet] [Doctoral dissertation]. The Ohio State University; 1964. [cited 2019 Nov 12]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1486564960924631.

Council of Science Editors:

Dale RG. Flutter analysis of an airfoil exhibiting camber deformations. [Doctoral Dissertation]. The Ohio State University; 1964. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1486564960924631


Indian Institute of Science

13. Vijay, B V. Some Investigations On Supersonic Flutter And Tailoring Of Laminated Composite Skin Panels.

Degree: 1997, Indian Institute of Science

Subjects/Keywords: Flutter (Aerodynamics); Flutter (Aerodynamics); Supersonic Aerodynamics; Composites - Flutter (Aerodynamics); Supersonic Flutter; Aeronautics

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APA (6th Edition):

Vijay, B. V. (1997). Some Investigations On Supersonic Flutter And Tailoring Of Laminated Composite Skin Panels. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/1772

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):

Vijay, B V. “Some Investigations On Supersonic Flutter And Tailoring Of Laminated Composite Skin Panels.” 1997. Thesis, Indian Institute of Science. Accessed November 12, 2019. http://hdl.handle.net/2005/1772.

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

MLA Handbook (7th Edition):

Vijay, B V. “Some Investigations On Supersonic Flutter And Tailoring Of Laminated Composite Skin Panels.” 1997. Web. 12 Nov 2019.

Vancouver:

Vijay BV. Some Investigations On Supersonic Flutter And Tailoring Of Laminated Composite Skin Panels. [Internet] [Thesis]. Indian Institute of Science; 1997. [cited 2019 Nov 12]. Available from: http://hdl.handle.net/2005/1772.

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

Council of Science Editors:

Vijay BV. Some Investigations On Supersonic Flutter And Tailoring Of Laminated Composite Skin Panels. [Thesis]. Indian Institute of Science; 1997. Available from: http://hdl.handle.net/2005/1772

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


Indian Institute of Science

14. Vijay, B V. Some Investigations On Supersonic Flutter And Tailoring Of Laminated Composite Skin Panels.

Degree: 1997, Indian Institute of Science

Subjects/Keywords: Flutter (Aerodynamics); Flutter (Aerodynamics); Supersonic Aerodynamics; Composites - Flutter (Aerodynamics); Supersonic Flutter; Aeronautics

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

APA (6th Edition):

Vijay, B. V. (1997). Some Investigations On Supersonic Flutter And Tailoring Of Laminated Composite Skin Panels. (Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ernet.in/handle/2005/1772 ; http://etd.ncsi.iisc.ernet.in/abstracts/2305/G14785-Abs.pdf

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):

Vijay, B V. “Some Investigations On Supersonic Flutter And Tailoring Of Laminated Composite Skin Panels.” 1997. Thesis, Indian Institute of Science. Accessed November 12, 2019. http://etd.iisc.ernet.in/handle/2005/1772 ; http://etd.ncsi.iisc.ernet.in/abstracts/2305/G14785-Abs.pdf.

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

MLA Handbook (7th Edition):

Vijay, B V. “Some Investigations On Supersonic Flutter And Tailoring Of Laminated Composite Skin Panels.” 1997. Web. 12 Nov 2019.

Vancouver:

Vijay BV. Some Investigations On Supersonic Flutter And Tailoring Of Laminated Composite Skin Panels. [Internet] [Thesis]. Indian Institute of Science; 1997. [cited 2019 Nov 12]. Available from: http://etd.iisc.ernet.in/handle/2005/1772 ; http://etd.ncsi.iisc.ernet.in/abstracts/2305/G14785-Abs.pdf.

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

Council of Science Editors:

Vijay BV. Some Investigations On Supersonic Flutter And Tailoring Of Laminated Composite Skin Panels. [Thesis]. Indian Institute of Science; 1997. Available from: http://etd.iisc.ernet.in/handle/2005/1772 ; http://etd.ncsi.iisc.ernet.in/abstracts/2305/G14785-Abs.pdf

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


University of Canterbury

15. Pons, Arion Douglas. Aeroelastic flutter as a multiparameter eigenvalue problem.

Degree: Department of Mechanical Engineering, 2015, University of Canterbury

 In this thesis we explore the relationship between aeroelastic flutter and multiparameter spectral theory. We first introduce the basic concept of the relationship between these… (more)

Subjects/Keywords: aeroelasticity; flutter; multiparameter; eigenvalue; instability; aerodynamics; vibration

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APA (6th Edition):

Pons, A. D. (2015). Aeroelastic flutter as a multiparameter eigenvalue problem. (Thesis). University of Canterbury. Retrieved from http://hdl.handle.net/10092/11265

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):

Pons, Arion Douglas. “Aeroelastic flutter as a multiparameter eigenvalue problem.” 2015. Thesis, University of Canterbury. Accessed November 12, 2019. http://hdl.handle.net/10092/11265.

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

MLA Handbook (7th Edition):

Pons, Arion Douglas. “Aeroelastic flutter as a multiparameter eigenvalue problem.” 2015. Web. 12 Nov 2019.

Vancouver:

Pons AD. Aeroelastic flutter as a multiparameter eigenvalue problem. [Internet] [Thesis]. University of Canterbury; 2015. [cited 2019 Nov 12]. Available from: http://hdl.handle.net/10092/11265.

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

Council of Science Editors:

Pons AD. Aeroelastic flutter as a multiparameter eigenvalue problem. [Thesis]. University of Canterbury; 2015. Available from: http://hdl.handle.net/10092/11265

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


University of Cincinnati

16. Cherry, Amy Kristine. Extended Techniques in Trumpet Performance and Pedagogy.

Degree: DMA, College-Conservatory of Music : Trumpet, 2009, University of Cincinnati

  The impetus for this study was the question of whether extended techniques are actually being taught in college trumpet studio settings as standard skills… (more)

Subjects/Keywords: Music; trumpet; extended techniques; multiphonics; flutter tonguing

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APA (6th Edition):

Cherry, A. K. (2009). Extended Techniques in Trumpet Performance and Pedagogy. (Doctoral Dissertation). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1242326372

Chicago Manual of Style (16th Edition):

Cherry, Amy Kristine. “Extended Techniques in Trumpet Performance and Pedagogy.” 2009. Doctoral Dissertation, University of Cincinnati. Accessed November 12, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1242326372.

MLA Handbook (7th Edition):

Cherry, Amy Kristine. “Extended Techniques in Trumpet Performance and Pedagogy.” 2009. Web. 12 Nov 2019.

Vancouver:

Cherry AK. Extended Techniques in Trumpet Performance and Pedagogy. [Internet] [Doctoral dissertation]. University of Cincinnati; 2009. [cited 2019 Nov 12]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1242326372.

Council of Science Editors:

Cherry AK. Extended Techniques in Trumpet Performance and Pedagogy. [Doctoral Dissertation]. University of Cincinnati; 2009. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1242326372

17. An, Sui. Aeroelastic design of a lightweight distributed electric propulsion aircraft with flutter and strength requirements.

Degree: MS, Aerospace Engineering, 2015, Georgia Tech

 Distributed electric propulsion is a promising technology currently being considered for gen- eral aviation-class aircraft that has the potential to increase range and performance without… (more)

Subjects/Keywords: Flutter; Optimization

…and flutter analysis. In this work, the Doublet-Lattice method is used to evaluate the… …structural model. Instead of utilizing a conventional flutter analysis, the Jacobi-Davidson method… …flutter constraints, wing aspect ratio, and electric propeller quantity are compared through a… …electric motors lead to heavier wings that are more susceptible to flutter. This framework can be… …satisfy strength and flutter requirements. x CHAPTER 1 INTRODUCTION Distributed electric… 

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APA (6th Edition):

An, S. (2015). Aeroelastic design of a lightweight distributed electric propulsion aircraft with flutter and strength requirements. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/53593

Chicago Manual of Style (16th Edition):

An, Sui. “Aeroelastic design of a lightweight distributed electric propulsion aircraft with flutter and strength requirements.” 2015. Masters Thesis, Georgia Tech. Accessed November 12, 2019. http://hdl.handle.net/1853/53593.

MLA Handbook (7th Edition):

An, Sui. “Aeroelastic design of a lightweight distributed electric propulsion aircraft with flutter and strength requirements.” 2015. Web. 12 Nov 2019.

Vancouver:

An S. Aeroelastic design of a lightweight distributed electric propulsion aircraft with flutter and strength requirements. [Internet] [Masters thesis]. Georgia Tech; 2015. [cited 2019 Nov 12]. Available from: http://hdl.handle.net/1853/53593.

Council of Science Editors:

An S. Aeroelastic design of a lightweight distributed electric propulsion aircraft with flutter and strength requirements. [Masters Thesis]. Georgia Tech; 2015. Available from: http://hdl.handle.net/1853/53593


Penn State University

18. Johnson, Samuel Craig. Design and Testing of a Small, Semi-span, Prop-rotor Model for Whirl Flutter Stability.

Degree: MS, Aerospace Engineering, 2014, Penn State University

 Modern tiltrotor aircraft are capable of ecient hover as well as high-speed forward ight. The large, exible rotors required for good hover performance make this… (more)

Subjects/Keywords: tiltrotor; wind tunnel; testing; whirl; flutter; stability

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APA (6th Edition):

Johnson, S. C. (2014). Design and Testing of a Small, Semi-span, Prop-rotor Model for Whirl Flutter Stability. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/21714

Chicago Manual of Style (16th Edition):

Johnson, Samuel Craig. “Design and Testing of a Small, Semi-span, Prop-rotor Model for Whirl Flutter Stability.” 2014. Masters Thesis, Penn State University. Accessed November 12, 2019. https://etda.libraries.psu.edu/catalog/21714.

MLA Handbook (7th Edition):

Johnson, Samuel Craig. “Design and Testing of a Small, Semi-span, Prop-rotor Model for Whirl Flutter Stability.” 2014. Web. 12 Nov 2019.

Vancouver:

Johnson SC. Design and Testing of a Small, Semi-span, Prop-rotor Model for Whirl Flutter Stability. [Internet] [Masters thesis]. Penn State University; 2014. [cited 2019 Nov 12]. Available from: https://etda.libraries.psu.edu/catalog/21714.

Council of Science Editors:

Johnson SC. Design and Testing of a Small, Semi-span, Prop-rotor Model for Whirl Flutter Stability. [Masters Thesis]. Penn State University; 2014. Available from: https://etda.libraries.psu.edu/catalog/21714


KTH

19. Zhuang, Qingyuan. Parametric Study on the Aeroelastic Stability of Rotor Seals.

Degree: Heat and Power Technology, 2012, KTH

  Labyrinth seals are widely used in rotating machinery and have been shown to experience aeroelastic instabilities. The rapid development of computational fluid dynamics now… (more)

Subjects/Keywords: Aeromechanics; turbomachinery; labyrinth seal; flutter; CFD; FEM

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APA (6th Edition):

Zhuang, Q. (2012). Parametric Study on the Aeroelastic Stability of Rotor Seals. (Thesis). KTH. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-116689

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):

Zhuang, Qingyuan. “Parametric Study on the Aeroelastic Stability of Rotor Seals.” 2012. Thesis, KTH. Accessed November 12, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-116689.

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

MLA Handbook (7th Edition):

Zhuang, Qingyuan. “Parametric Study on the Aeroelastic Stability of Rotor Seals.” 2012. Web. 12 Nov 2019.

Vancouver:

Zhuang Q. Parametric Study on the Aeroelastic Stability of Rotor Seals. [Internet] [Thesis]. KTH; 2012. [cited 2019 Nov 12]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-116689.

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

Council of Science Editors:

Zhuang Q. Parametric Study on the Aeroelastic Stability of Rotor Seals. [Thesis]. KTH; 2012. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-116689

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


Delft University of Technology

20. Visser, M. Linear parameter-varying model identification for flutter prediction:.

Degree: 2015, Delft University of Technology

Flutter-induced vibrations can easily cause large structures like airplanes and bridges to fail, which even today makes flutter prediction an important topic of research. To… (more)

Subjects/Keywords: linear parameter varying; system identification; flutter prediction

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APA (6th Edition):

Visser, M. (2015). Linear parameter-varying model identification for flutter prediction:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:0875f669-af4d-49a9-99e8-4cb5badfbaf8

Chicago Manual of Style (16th Edition):

Visser, M. “Linear parameter-varying model identification for flutter prediction:.” 2015. Masters Thesis, Delft University of Technology. Accessed November 12, 2019. http://resolver.tudelft.nl/uuid:0875f669-af4d-49a9-99e8-4cb5badfbaf8.

MLA Handbook (7th Edition):

Visser, M. “Linear parameter-varying model identification for flutter prediction:.” 2015. Web. 12 Nov 2019.

Vancouver:

Visser M. Linear parameter-varying model identification for flutter prediction:. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2019 Nov 12]. Available from: http://resolver.tudelft.nl/uuid:0875f669-af4d-49a9-99e8-4cb5badfbaf8.

Council of Science Editors:

Visser M. Linear parameter-varying model identification for flutter prediction:. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:0875f669-af4d-49a9-99e8-4cb5badfbaf8


University of Melbourne

21. Pathik, Manaswi Bhupesh. New insights into the mechanisms of atrial arrhythmias using novel three dimensional mapping techniques.

Degree: 2017, University of Melbourne

 Advances in our understanding of the pathophysiology of atrial fibrillation (AF) and atrial macro-reentry through improvements in technology has led to the development of treatment… (more)

Subjects/Keywords: atrial fibrillation; atrial flutter; phase mapping

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APA (6th Edition):

Pathik, M. B. (2017). New insights into the mechanisms of atrial arrhythmias using novel three dimensional mapping techniques. (Doctoral Dissertation). University of Melbourne. Retrieved from http://hdl.handle.net/11343/194696

Chicago Manual of Style (16th Edition):

Pathik, Manaswi Bhupesh. “New insights into the mechanisms of atrial arrhythmias using novel three dimensional mapping techniques.” 2017. Doctoral Dissertation, University of Melbourne. Accessed November 12, 2019. http://hdl.handle.net/11343/194696.

MLA Handbook (7th Edition):

Pathik, Manaswi Bhupesh. “New insights into the mechanisms of atrial arrhythmias using novel three dimensional mapping techniques.” 2017. Web. 12 Nov 2019.

Vancouver:

Pathik MB. New insights into the mechanisms of atrial arrhythmias using novel three dimensional mapping techniques. [Internet] [Doctoral dissertation]. University of Melbourne; 2017. [cited 2019 Nov 12]. Available from: http://hdl.handle.net/11343/194696.

Council of Science Editors:

Pathik MB. New insights into the mechanisms of atrial arrhythmias using novel three dimensional mapping techniques. [Doctoral Dissertation]. University of Melbourne; 2017. Available from: http://hdl.handle.net/11343/194696


University of Ottawa

22. Feng, Fan. Flutter Analysis of Stonecutters Cable-stayed Bridge using Finite Element Model .

Degree: 2015, University of Ottawa

 The current research analyzed the flutter response of the Stonecutters Cable-Stayed Bridge in Hong Kong, which has a twin deck configuration, under the effect of… (more)

Subjects/Keywords: Flutter; Stonecutters; Finite Element Model; Abaqus

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APA (6th Edition):

Feng, F. (2015). Flutter Analysis of Stonecutters Cable-stayed Bridge using Finite Element Model . (Thesis). University of Ottawa. Retrieved from http://hdl.handle.net/10393/32470

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):

Feng, Fan. “Flutter Analysis of Stonecutters Cable-stayed Bridge using Finite Element Model .” 2015. Thesis, University of Ottawa. Accessed November 12, 2019. http://hdl.handle.net/10393/32470.

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

MLA Handbook (7th Edition):

Feng, Fan. “Flutter Analysis of Stonecutters Cable-stayed Bridge using Finite Element Model .” 2015. Web. 12 Nov 2019.

Vancouver:

Feng F. Flutter Analysis of Stonecutters Cable-stayed Bridge using Finite Element Model . [Internet] [Thesis]. University of Ottawa; 2015. [cited 2019 Nov 12]. Available from: http://hdl.handle.net/10393/32470.

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

Council of Science Editors:

Feng F. Flutter Analysis of Stonecutters Cable-stayed Bridge using Finite Element Model . [Thesis]. University of Ottawa; 2015. Available from: http://hdl.handle.net/10393/32470

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


Texas A&M University

23. Brown II, Robert Lee. Numerical Simulations of Hypersonic Aerothermoelastic Phenomena.

Degree: PhD, Aerospace Engineering, 2016, Texas A&M University

 This dissertation examines the following subjects important to hypersonic aerothermoelastic flows: aerodynamic heating on a double-wedge airfoil, active cooling on a double-wedge airfoil, and aerothermoelastic… (more)

Subjects/Keywords: hypersonic; panel flutter; aerothermal; aeroelastic; aerothermoelastic; simulation

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APA (6th Edition):

Brown II, R. L. (2016). Numerical Simulations of Hypersonic Aerothermoelastic Phenomena. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/158046

Chicago Manual of Style (16th Edition):

Brown II, Robert Lee. “Numerical Simulations of Hypersonic Aerothermoelastic Phenomena.” 2016. Doctoral Dissertation, Texas A&M University. Accessed November 12, 2019. http://hdl.handle.net/1969.1/158046.

MLA Handbook (7th Edition):

Brown II, Robert Lee. “Numerical Simulations of Hypersonic Aerothermoelastic Phenomena.” 2016. Web. 12 Nov 2019.

Vancouver:

Brown II RL. Numerical Simulations of Hypersonic Aerothermoelastic Phenomena. [Internet] [Doctoral dissertation]. Texas A&M University; 2016. [cited 2019 Nov 12]. Available from: http://hdl.handle.net/1969.1/158046.

Council of Science Editors:

Brown II RL. Numerical Simulations of Hypersonic Aerothermoelastic Phenomena. [Doctoral Dissertation]. Texas A&M University; 2016. Available from: http://hdl.handle.net/1969.1/158046


University of Illinois – Urbana-Champaign

24. Singh, Prince. Fluid-structure interaction in noisy nonlinear systems.

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

 The first part of this work is concerned with the application of stochastic dimensional reduction to a twelve-dimensional aeroelastic model (i.e., two degrees of freedom… (more)

Subjects/Keywords: Homogenization; Flutter; Lyapunov Exponents; Large Deviations Theory

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APA (6th Edition):

Singh, P. (2014). Fluid-structure interaction in noisy nonlinear systems. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/50653

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):

Singh, Prince. “Fluid-structure interaction in noisy nonlinear systems.” 2014. Thesis, University of Illinois – Urbana-Champaign. Accessed November 12, 2019. http://hdl.handle.net/2142/50653.

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

MLA Handbook (7th Edition):

Singh, Prince. “Fluid-structure interaction in noisy nonlinear systems.” 2014. Web. 12 Nov 2019.

Vancouver:

Singh P. Fluid-structure interaction in noisy nonlinear systems. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2014. [cited 2019 Nov 12]. Available from: http://hdl.handle.net/2142/50653.

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

Council of Science Editors:

Singh P. Fluid-structure interaction in noisy nonlinear systems. [Thesis]. University of Illinois – Urbana-Champaign; 2014. Available from: http://hdl.handle.net/2142/50653

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


University of Manitoba

25. Fleming, Patrick Hugh. Wind tunnel studies on rotational effects in lightly-iced transmission line galloping.

Degree: Mechanical and Manufacturing Engineering, 2010, University of Manitoba

 Overhead transmission lines are prone to undergo large amplitude, low frequency vibrations when exposed to freezing rain and steady side winds. These vibrations are referred… (more)

Subjects/Keywords: galloping; conductor; wind; ice; flutter; transmission

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APA (6th Edition):

Fleming, P. H. (2010). Wind tunnel studies on rotational effects in lightly-iced transmission line galloping. (Masters Thesis). University of Manitoba. Retrieved from http://hdl.handle.net/1993/4017

Chicago Manual of Style (16th Edition):

Fleming, Patrick Hugh. “Wind tunnel studies on rotational effects in lightly-iced transmission line galloping.” 2010. Masters Thesis, University of Manitoba. Accessed November 12, 2019. http://hdl.handle.net/1993/4017.

MLA Handbook (7th Edition):

Fleming, Patrick Hugh. “Wind tunnel studies on rotational effects in lightly-iced transmission line galloping.” 2010. Web. 12 Nov 2019.

Vancouver:

Fleming PH. Wind tunnel studies on rotational effects in lightly-iced transmission line galloping. [Internet] [Masters thesis]. University of Manitoba; 2010. [cited 2019 Nov 12]. Available from: http://hdl.handle.net/1993/4017.

Council of Science Editors:

Fleming PH. Wind tunnel studies on rotational effects in lightly-iced transmission line galloping. [Masters Thesis]. University of Manitoba; 2010. Available from: http://hdl.handle.net/1993/4017

26. Lemler, Kaci. Modal Testing And Analysis Techniques And Their Application On A Small Uas.

Degree: MS, Mechanical Engineering, 2012, University of North Dakota

  This thesis focuses on experimental structural analysis using contemporary testing techniques. This includes modal testing topics such as data acquisition, data processing, sensor placement,… (more)

Subjects/Keywords: Flutter; Modal Testing; Sensor Location; UAS; Vibration

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APA (6th Edition):

Lemler, K. (2012). Modal Testing And Analysis Techniques And Their Application On A Small Uas. (Masters Thesis). University of North Dakota. Retrieved from https://commons.und.edu/theses/1359

Chicago Manual of Style (16th Edition):

Lemler, Kaci. “Modal Testing And Analysis Techniques And Their Application On A Small Uas.” 2012. Masters Thesis, University of North Dakota. Accessed November 12, 2019. https://commons.und.edu/theses/1359.

MLA Handbook (7th Edition):

Lemler, Kaci. “Modal Testing And Analysis Techniques And Their Application On A Small Uas.” 2012. Web. 12 Nov 2019.

Vancouver:

Lemler K. Modal Testing And Analysis Techniques And Their Application On A Small Uas. [Internet] [Masters thesis]. University of North Dakota; 2012. [cited 2019 Nov 12]. Available from: https://commons.und.edu/theses/1359.

Council of Science Editors:

Lemler K. Modal Testing And Analysis Techniques And Their Application On A Small Uas. [Masters Thesis]. University of North Dakota; 2012. Available from: https://commons.und.edu/theses/1359


Montana Tech

27. Niese, Robert Lawrence. WHY THE WEIRD WINGS? Investigating the morphology, function, and evolution of unusual feathers in pigeons and doves (Columbidae).

Degree: PhD, 2019, Montana Tech

  The feathers of the wing that power flight in birds (the remiges) are morphologically constrained by the demands of aerial locomotion, but peculiar morphologies… (more)

Subjects/Keywords: aerodynamics; flight; flutter; morphology; sonation; wing sounds

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APA (6th Edition):

Niese, R. L. (2019). WHY THE WEIRD WINGS? Investigating the morphology, function, and evolution of unusual feathers in pigeons and doves (Columbidae). (Doctoral Dissertation). Montana Tech. Retrieved from https://scholarworks.umt.edu/etd/11406

Chicago Manual of Style (16th Edition):

Niese, Robert Lawrence. “WHY THE WEIRD WINGS? Investigating the morphology, function, and evolution of unusual feathers in pigeons and doves (Columbidae).” 2019. Doctoral Dissertation, Montana Tech. Accessed November 12, 2019. https://scholarworks.umt.edu/etd/11406.

MLA Handbook (7th Edition):

Niese, Robert Lawrence. “WHY THE WEIRD WINGS? Investigating the morphology, function, and evolution of unusual feathers in pigeons and doves (Columbidae).” 2019. Web. 12 Nov 2019.

Vancouver:

Niese RL. WHY THE WEIRD WINGS? Investigating the morphology, function, and evolution of unusual feathers in pigeons and doves (Columbidae). [Internet] [Doctoral dissertation]. Montana Tech; 2019. [cited 2019 Nov 12]. Available from: https://scholarworks.umt.edu/etd/11406.

Council of Science Editors:

Niese RL. WHY THE WEIRD WINGS? Investigating the morphology, function, and evolution of unusual feathers in pigeons and doves (Columbidae). [Doctoral Dissertation]. Montana Tech; 2019. Available from: https://scholarworks.umt.edu/etd/11406


University of Minnesota

28. Alfifi, Salman. An Experimental Study of Wing Flutter.

Degree: PhD, Aerospace Engineering and Mechanics, 2017, University of Minnesota

 While many experimental studies use springs to model the bending and torsional motions of a fluttered wing in wind tunnel experiments, the mass of the… (more)

Subjects/Keywords: aerodynamics; aeroelasticity; flluid mechanics; flutter; wing

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APA (6th Edition):

Alfifi, S. (2017). An Experimental Study of Wing Flutter. (Doctoral Dissertation). University of Minnesota. Retrieved from http://hdl.handle.net/11299/206344

Chicago Manual of Style (16th Edition):

Alfifi, Salman. “An Experimental Study of Wing Flutter.” 2017. Doctoral Dissertation, University of Minnesota. Accessed November 12, 2019. http://hdl.handle.net/11299/206344.

MLA Handbook (7th Edition):

Alfifi, Salman. “An Experimental Study of Wing Flutter.” 2017. Web. 12 Nov 2019.

Vancouver:

Alfifi S. An Experimental Study of Wing Flutter. [Internet] [Doctoral dissertation]. University of Minnesota; 2017. [cited 2019 Nov 12]. Available from: http://hdl.handle.net/11299/206344.

Council of Science Editors:

Alfifi S. An Experimental Study of Wing Flutter. [Doctoral Dissertation]. University of Minnesota; 2017. Available from: http://hdl.handle.net/11299/206344


University of Washington

29. Phillips, Andrew David. Investigation of Aspects of Aeroservoelastic State-Space Modeling on Active Flutter Suppression LQR Control Synthesis.

Degree: 2018, University of Washington

 Whether motivated by cost or performance, the shift to structurally lighter aircraft has increased the demand for new developments in aeroservoelasticity. The William E. Boeing… (more)

Subjects/Keywords: active flutter suppression; aeroservoelasticity; flexible; flutter; roger approximation; state space; Aerospace engineering; Aeronautics and astronautics

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

APA (6th Edition):

Phillips, A. D. (2018). Investigation of Aspects of Aeroservoelastic State-Space Modeling on Active Flutter Suppression LQR Control Synthesis. (Thesis). University of Washington. Retrieved from http://hdl.handle.net/1773/41728

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):

Phillips, Andrew David. “Investigation of Aspects of Aeroservoelastic State-Space Modeling on Active Flutter Suppression LQR Control Synthesis.” 2018. Thesis, University of Washington. Accessed November 12, 2019. http://hdl.handle.net/1773/41728.

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

MLA Handbook (7th Edition):

Phillips, Andrew David. “Investigation of Aspects of Aeroservoelastic State-Space Modeling on Active Flutter Suppression LQR Control Synthesis.” 2018. Web. 12 Nov 2019.

Vancouver:

Phillips AD. Investigation of Aspects of Aeroservoelastic State-Space Modeling on Active Flutter Suppression LQR Control Synthesis. [Internet] [Thesis]. University of Washington; 2018. [cited 2019 Nov 12]. Available from: http://hdl.handle.net/1773/41728.

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

Council of Science Editors:

Phillips AD. Investigation of Aspects of Aeroservoelastic State-Space Modeling on Active Flutter Suppression LQR Control Synthesis. [Thesis]. University of Washington; 2018. Available from: http://hdl.handle.net/1773/41728

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


Brno University of Technology

30. Šrutová, Martina. Diagnostika ventrikulárních tachykardií z elektrokardiografického záznamu.

Degree: 2010, Brno University of Technology

 Cílem této práce je diagnostika ventrikulárních tachykardií, fibrilací a flutterů z elektrokardiogramu. Tyto poruchy srdečního rytmu patří mezi život ohrožující arytmie. V následující práci je… (more)

Subjects/Keywords: komorová tachykardie; fibrilace; flutter; detekční algoritmus; EKG; ventricular tachycardia; fibrillation; flutter; detection algorithm; ECG

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

APA (6th Edition):

Šrutová, M. (2010). Diagnostika ventrikulárních tachykardií z elektrokardiografického záznamu. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/15307

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):

Šrutová, Martina. “Diagnostika ventrikulárních tachykardií z elektrokardiografického záznamu. ” 2010. Thesis, Brno University of Technology. Accessed November 12, 2019. http://hdl.handle.net/11012/15307.

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

MLA Handbook (7th Edition):

Šrutová, Martina. “Diagnostika ventrikulárních tachykardií z elektrokardiografického záznamu. ” 2010. Web. 12 Nov 2019.

Vancouver:

Šrutová M. Diagnostika ventrikulárních tachykardií z elektrokardiografického záznamu. [Internet] [Thesis]. Brno University of Technology; 2010. [cited 2019 Nov 12]. Available from: http://hdl.handle.net/11012/15307.

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

Council of Science Editors:

Šrutová M. Diagnostika ventrikulárních tachykardií z elektrokardiografického záznamu. [Thesis]. Brno University of Technology; 2010. Available from: http://hdl.handle.net/11012/15307

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

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