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You searched for subject:(Helicopter rotor). Showing records 1 – 30 of 75 total matches.

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University of Texas – Austin

1. Karpatne, Anand. Study of compressible flow through a rotating duct.

Degree: PhD, Aerospace engineering, 2015, University of Texas – Austin

 Several rotorcraft applications such as circulation control and tip jet driven rotors involve internal spanwise flow along the interior of a rotor blade. This dissertation… (more)

Subjects/Keywords: Helicopter; Rotor; Internal flow

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APA (6th Edition):

Karpatne, A. (2015). Study of compressible flow through a rotating duct. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/31343

Chicago Manual of Style (16th Edition):

Karpatne, Anand. “Study of compressible flow through a rotating duct.” 2015. Doctoral Dissertation, University of Texas – Austin. Accessed March 07, 2021. http://hdl.handle.net/2152/31343.

MLA Handbook (7th Edition):

Karpatne, Anand. “Study of compressible flow through a rotating duct.” 2015. Web. 07 Mar 2021.

Vancouver:

Karpatne A. Study of compressible flow through a rotating duct. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2015. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/2152/31343.

Council of Science Editors:

Karpatne A. Study of compressible flow through a rotating duct. [Doctoral Dissertation]. University of Texas – Austin; 2015. Available from: http://hdl.handle.net/2152/31343


Brno University of Technology

2. Junas, Milan. Předběžný návrh malého dvoumístného vrtulníku: Preliminary Design of a Small Two Seat Helicopter.

Degree: 2019, Brno University of Technology

 The thesis deals the preliminary draft of the small two-seat helicopter with a piston engine. The aim of the thesis is not to propose a… (more)

Subjects/Keywords: vrtuľník; hlavný rotor; vyrovnávací rotor; rotorová hlava; rotorový list; helicopter; main rotor; tail rotor; rotor head; rotor blade

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APA (6th Edition):

Junas, M. (2019). Předběžný návrh malého dvoumístného vrtulníku: Preliminary Design of a Small Two Seat Helicopter. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/59691

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):

Junas, Milan. “Předběžný návrh malého dvoumístného vrtulníku: Preliminary Design of a Small Two Seat Helicopter.” 2019. Thesis, Brno University of Technology. Accessed March 07, 2021. http://hdl.handle.net/11012/59691.

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

MLA Handbook (7th Edition):

Junas, Milan. “Předběžný návrh malého dvoumístného vrtulníku: Preliminary Design of a Small Two Seat Helicopter.” 2019. Web. 07 Mar 2021.

Vancouver:

Junas M. Předběžný návrh malého dvoumístného vrtulníku: Preliminary Design of a Small Two Seat Helicopter. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/11012/59691.

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

Council of Science Editors:

Junas M. Předběžný návrh malého dvoumístného vrtulníku: Preliminary Design of a Small Two Seat Helicopter. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/59691

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


Cornell University

3. Fang, Austin. Improved Rotor Track And Balance Algorithm And System Identification Of Rotorcraft Using Flight Data.

Degree: PhD, Aerospace Engineering, 2015, Cornell University

Rotor track and balance is an essential part of maintenance for the rotorcraft industry. Methods for solving rotor track and balance problems to minimize undesirable… (more)

Subjects/Keywords: Rotor Track and Balance; Rotorcraft; Helicopter Tuning

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APA (6th Edition):

Fang, A. (2015). Improved Rotor Track And Balance Algorithm And System Identification Of Rotorcraft Using Flight Data. (Doctoral Dissertation). Cornell University. Retrieved from http://hdl.handle.net/1813/39294

Chicago Manual of Style (16th Edition):

Fang, Austin. “Improved Rotor Track And Balance Algorithm And System Identification Of Rotorcraft Using Flight Data.” 2015. Doctoral Dissertation, Cornell University. Accessed March 07, 2021. http://hdl.handle.net/1813/39294.

MLA Handbook (7th Edition):

Fang, Austin. “Improved Rotor Track And Balance Algorithm And System Identification Of Rotorcraft Using Flight Data.” 2015. Web. 07 Mar 2021.

Vancouver:

Fang A. Improved Rotor Track And Balance Algorithm And System Identification Of Rotorcraft Using Flight Data. [Internet] [Doctoral dissertation]. Cornell University; 2015. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/1813/39294.

Council of Science Editors:

Fang A. Improved Rotor Track And Balance Algorithm And System Identification Of Rotorcraft Using Flight Data. [Doctoral Dissertation]. Cornell University; 2015. Available from: http://hdl.handle.net/1813/39294


Penn State University

4. Villafana, Willca. Rotorcraft Noise Abatement Procedures Development.

Degree: 2016, Penn State University

 A rotorcraft noise prediction system has recently been developed as part of a project to develop and evaluate helicopter noise abatement procedures for a range… (more)

Subjects/Keywords: aeroacoustics; helicopter; rotor noise; simulation; modeling

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APA (6th Edition):

Villafana, W. (2016). Rotorcraft Noise Abatement Procedures Development. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/13106wrv105

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):

Villafana, Willca. “Rotorcraft Noise Abatement Procedures Development.” 2016. Thesis, Penn State University. Accessed March 07, 2021. https://submit-etda.libraries.psu.edu/catalog/13106wrv105.

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

MLA Handbook (7th Edition):

Villafana, Willca. “Rotorcraft Noise Abatement Procedures Development.” 2016. Web. 07 Mar 2021.

Vancouver:

Villafana W. Rotorcraft Noise Abatement Procedures Development. [Internet] [Thesis]. Penn State University; 2016. [cited 2021 Mar 07]. Available from: https://submit-etda.libraries.psu.edu/catalog/13106wrv105.

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

Council of Science Editors:

Villafana W. Rotorcraft Noise Abatement Procedures Development. [Thesis]. Penn State University; 2016. Available from: https://submit-etda.libraries.psu.edu/catalog/13106wrv105

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


University of Melbourne

5. Bourne, Kate. Vortex ring and rotor wake interaction with solid surfaces.

Degree: 2017, University of Melbourne

 The interaction between vortex structures and solid surfaces represents an inherently complex flow environment. When considering the rotor wake downwash generated by rotary-wing aircraft operating… (more)

Subjects/Keywords: rotor wake; vortex ring; brownout; helicopter

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APA (6th Edition):

Bourne, K. (2017). Vortex ring and rotor wake interaction with solid surfaces. (Doctoral Dissertation). University of Melbourne. Retrieved from http://hdl.handle.net/11343/192902

Chicago Manual of Style (16th Edition):

Bourne, Kate. “Vortex ring and rotor wake interaction with solid surfaces.” 2017. Doctoral Dissertation, University of Melbourne. Accessed March 07, 2021. http://hdl.handle.net/11343/192902.

MLA Handbook (7th Edition):

Bourne, Kate. “Vortex ring and rotor wake interaction with solid surfaces.” 2017. Web. 07 Mar 2021.

Vancouver:

Bourne K. Vortex ring and rotor wake interaction with solid surfaces. [Internet] [Doctoral dissertation]. University of Melbourne; 2017. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/11343/192902.

Council of Science Editors:

Bourne K. Vortex ring and rotor wake interaction with solid surfaces. [Doctoral Dissertation]. University of Melbourne; 2017. Available from: http://hdl.handle.net/11343/192902


Georgia Tech

6. Battey, Luke Sterling. A hybrid Navier Stokes/vortex particle wake methodology for modeling helicopter rotors in forward flight and maneuvers.

Degree: MS, Aerospace Engineering, 2018, Georgia Tech

 Maneuvering flight and high-speed flight are critical design points in any rotorcraft’s operating envelope. These conditions give complex flow phenomena, creating high stresses and vibrations.… (more)

Subjects/Keywords: Helicopter; Rotor; Rotorcraft; Hybrid; Wake; Vortex; Particle

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

APA (6th Edition):

Battey, L. S. (2018). A hybrid Navier Stokes/vortex particle wake methodology for modeling helicopter rotors in forward flight and maneuvers. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/59934

Chicago Manual of Style (16th Edition):

Battey, Luke Sterling. “A hybrid Navier Stokes/vortex particle wake methodology for modeling helicopter rotors in forward flight and maneuvers.” 2018. Masters Thesis, Georgia Tech. Accessed March 07, 2021. http://hdl.handle.net/1853/59934.

MLA Handbook (7th Edition):

Battey, Luke Sterling. “A hybrid Navier Stokes/vortex particle wake methodology for modeling helicopter rotors in forward flight and maneuvers.” 2018. Web. 07 Mar 2021.

Vancouver:

Battey LS. A hybrid Navier Stokes/vortex particle wake methodology for modeling helicopter rotors in forward flight and maneuvers. [Internet] [Masters thesis]. Georgia Tech; 2018. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/1853/59934.

Council of Science Editors:

Battey LS. A hybrid Navier Stokes/vortex particle wake methodology for modeling helicopter rotors in forward flight and maneuvers. [Masters Thesis]. Georgia Tech; 2018. Available from: http://hdl.handle.net/1853/59934


Penn State University

7. Cheng, Baofeng. HELICOPTER ROTOR NOISE INVESTIGATION DURING ICE ACCRETION.

Degree: 2016, Penn State University

 An investigation of helicopter rotor noise during ice accretion is conducted using experimental, theoretical, and numerical methods. This research is the acoustic part of a… (more)

Subjects/Keywords: Helicopter Rotor Noise; Rotor Broadband Noise; Helicopter Ice Accretion; Surface Roughness; Trailing Edge Noise

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

APA (6th Edition):

Cheng, B. (2016). HELICOPTER ROTOR NOISE INVESTIGATION DURING ICE ACCRETION. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/13412bqc5108

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):

Cheng, Baofeng. “HELICOPTER ROTOR NOISE INVESTIGATION DURING ICE ACCRETION.” 2016. Thesis, Penn State University. Accessed March 07, 2021. https://submit-etda.libraries.psu.edu/catalog/13412bqc5108.

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

MLA Handbook (7th Edition):

Cheng, Baofeng. “HELICOPTER ROTOR NOISE INVESTIGATION DURING ICE ACCRETION.” 2016. Web. 07 Mar 2021.

Vancouver:

Cheng B. HELICOPTER ROTOR NOISE INVESTIGATION DURING ICE ACCRETION. [Internet] [Thesis]. Penn State University; 2016. [cited 2021 Mar 07]. Available from: https://submit-etda.libraries.psu.edu/catalog/13412bqc5108.

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

Council of Science Editors:

Cheng B. HELICOPTER ROTOR NOISE INVESTIGATION DURING ICE ACCRETION. [Thesis]. Penn State University; 2016. Available from: https://submit-etda.libraries.psu.edu/catalog/13412bqc5108

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


Delft University of Technology

8. Declerck, Laurent (author). Feasibility Study of a Load Alleviation Strategy on a Compound Helicopter Using Redundant Controls.

Degree: 2019, Delft University of Technology

 <p class="MsoNormal">The compound helicopter gains interest as operational needs push future rotorcraft capabilities beyond current standards. The compound helicopter is investigated as part of the… (more)

Subjects/Keywords: Structural Load Alleviation; SLA; Compound Helicopter; Helicopter; Helicopter Model; Rotor; Flapping Dynamics; Blade Flap

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

APA (6th Edition):

Declerck, L. (. (2019). Feasibility Study of a Load Alleviation Strategy on a Compound Helicopter Using Redundant Controls. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:b96a69b6-7aac-436d-a2e6-d3b878d14761

Chicago Manual of Style (16th Edition):

Declerck, Laurent (author). “Feasibility Study of a Load Alleviation Strategy on a Compound Helicopter Using Redundant Controls.” 2019. Masters Thesis, Delft University of Technology. Accessed March 07, 2021. http://resolver.tudelft.nl/uuid:b96a69b6-7aac-436d-a2e6-d3b878d14761.

MLA Handbook (7th Edition):

Declerck, Laurent (author). “Feasibility Study of a Load Alleviation Strategy on a Compound Helicopter Using Redundant Controls.” 2019. Web. 07 Mar 2021.

Vancouver:

Declerck L(. Feasibility Study of a Load Alleviation Strategy on a Compound Helicopter Using Redundant Controls. [Internet] [Masters thesis]. Delft University of Technology; 2019. [cited 2021 Mar 07]. Available from: http://resolver.tudelft.nl/uuid:b96a69b6-7aac-436d-a2e6-d3b878d14761.

Council of Science Editors:

Declerck L(. Feasibility Study of a Load Alleviation Strategy on a Compound Helicopter Using Redundant Controls. [Masters Thesis]. Delft University of Technology; 2019. Available from: http://resolver.tudelft.nl/uuid:b96a69b6-7aac-436d-a2e6-d3b878d14761


Penn State University

9. Choephel, Tenzin. Aerodynamic Analysis of Helicopter Rotors Using a Higher-Order, Free-Wake Method.

Degree: 2016, Penn State University

 The wake has a strong influence on the aerodynamics of a helicopter rotor, and the accurate prediction of its geometry and the resulting induced velocity… (more)

Subjects/Keywords: Free-Wake; Inflow; Hover; Helicopter Rotor; Rotor Downwash

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APA (6th Edition):

Choephel, T. (2016). Aerodynamic Analysis of Helicopter Rotors Using a Higher-Order, Free-Wake Method. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/13102txc279

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):

Choephel, Tenzin. “Aerodynamic Analysis of Helicopter Rotors Using a Higher-Order, Free-Wake Method.” 2016. Thesis, Penn State University. Accessed March 07, 2021. https://submit-etda.libraries.psu.edu/catalog/13102txc279.

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

MLA Handbook (7th Edition):

Choephel, Tenzin. “Aerodynamic Analysis of Helicopter Rotors Using a Higher-Order, Free-Wake Method.” 2016. Web. 07 Mar 2021.

Vancouver:

Choephel T. Aerodynamic Analysis of Helicopter Rotors Using a Higher-Order, Free-Wake Method. [Internet] [Thesis]. Penn State University; 2016. [cited 2021 Mar 07]. Available from: https://submit-etda.libraries.psu.edu/catalog/13102txc279.

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

Council of Science Editors:

Choephel T. Aerodynamic Analysis of Helicopter Rotors Using a Higher-Order, Free-Wake Method. [Thesis]. Penn State University; 2016. Available from: https://submit-etda.libraries.psu.edu/catalog/13102txc279

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

10. Leusink, Debbie. Advanced numerical tools for aerodynamic optimization of helicopter rotor blades : Outils numériques avancés pour le dimensionnement de rotors sustentateurs d’hélicoptère.

Degree: Docteur es, Mécanique, 2013, Paris, ENSAM

La conception aérodynamique des pales du rotor principal d’un hélicoptère doitsimultanément prendre en compte plusieurs objectifs relatifs aux critères du vol stationnaire etvol d’avancement. Cette… (more)

Subjects/Keywords: Helicoptère; Rotor; Dimensionnement; Aerodynamique; Optimisation; Helicopter; Rotor; Dimensioning; Aerodynamics; Optimization

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

APA (6th Edition):

Leusink, D. (2013). Advanced numerical tools for aerodynamic optimization of helicopter rotor blades : Outils numériques avancés pour le dimensionnement de rotors sustentateurs d’hélicoptère. (Doctoral Dissertation). Paris, ENSAM. Retrieved from http://www.theses.fr/2013ENAM0010

Chicago Manual of Style (16th Edition):

Leusink, Debbie. “Advanced numerical tools for aerodynamic optimization of helicopter rotor blades : Outils numériques avancés pour le dimensionnement de rotors sustentateurs d’hélicoptère.” 2013. Doctoral Dissertation, Paris, ENSAM. Accessed March 07, 2021. http://www.theses.fr/2013ENAM0010.

MLA Handbook (7th Edition):

Leusink, Debbie. “Advanced numerical tools for aerodynamic optimization of helicopter rotor blades : Outils numériques avancés pour le dimensionnement de rotors sustentateurs d’hélicoptère.” 2013. Web. 07 Mar 2021.

Vancouver:

Leusink D. Advanced numerical tools for aerodynamic optimization of helicopter rotor blades : Outils numériques avancés pour le dimensionnement de rotors sustentateurs d’hélicoptère. [Internet] [Doctoral dissertation]. Paris, ENSAM; 2013. [cited 2021 Mar 07]. Available from: http://www.theses.fr/2013ENAM0010.

Council of Science Editors:

Leusink D. Advanced numerical tools for aerodynamic optimization of helicopter rotor blades : Outils numériques avancés pour le dimensionnement de rotors sustentateurs d’hélicoptère. [Doctoral Dissertation]. Paris, ENSAM; 2013. Available from: http://www.theses.fr/2013ENAM0010

11. Xie, Lihan. Suivi numérique des bifurcations pour l'analyse paramétrique de la dynamique non-linéaire des rotors : Numerical tracking of bifurcations for parametric analysis of nonlinear rotor dynamics.

Degree: Docteur es, Mécanique, 2016, Lyon

Au cœur des moyens de transport, de transformation d'énergie, et de biens d'équipements, les machines tournantes peuvent avoir des comportements dynamiques complexes dus à de… (more)

Subjects/Keywords: Dynamique du rotor; Rotor; Rotor d'hélicoptère; Hélicoptère; Méthode numérique; Machines tournantes; Bifurcation; Rotor dynamics; Rotor; Helicopter rotor; Helicopter; Numerical methods; Rotating machine; Bifurcation; 620.104 072

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APA (6th Edition):

Xie, L. (2016). Suivi numérique des bifurcations pour l'analyse paramétrique de la dynamique non-linéaire des rotors : Numerical tracking of bifurcations for parametric analysis of nonlinear rotor dynamics. (Doctoral Dissertation). Lyon. Retrieved from http://www.theses.fr/2016LYSEI018

Chicago Manual of Style (16th Edition):

Xie, Lihan. “Suivi numérique des bifurcations pour l'analyse paramétrique de la dynamique non-linéaire des rotors : Numerical tracking of bifurcations for parametric analysis of nonlinear rotor dynamics.” 2016. Doctoral Dissertation, Lyon. Accessed March 07, 2021. http://www.theses.fr/2016LYSEI018.

MLA Handbook (7th Edition):

Xie, Lihan. “Suivi numérique des bifurcations pour l'analyse paramétrique de la dynamique non-linéaire des rotors : Numerical tracking of bifurcations for parametric analysis of nonlinear rotor dynamics.” 2016. Web. 07 Mar 2021.

Vancouver:

Xie L. Suivi numérique des bifurcations pour l'analyse paramétrique de la dynamique non-linéaire des rotors : Numerical tracking of bifurcations for parametric analysis of nonlinear rotor dynamics. [Internet] [Doctoral dissertation]. Lyon; 2016. [cited 2021 Mar 07]. Available from: http://www.theses.fr/2016LYSEI018.

Council of Science Editors:

Xie L. Suivi numérique des bifurcations pour l'analyse paramétrique de la dynamique non-linéaire des rotors : Numerical tracking of bifurcations for parametric analysis of nonlinear rotor dynamics. [Doctoral Dissertation]. Lyon; 2016. Available from: http://www.theses.fr/2016LYSEI018


Brno University of Technology

12. Rybka, Slavomír. Dopravní vrtulníky: Air transport helicopters.

Degree: 2019, Brno University of Technology

 The Bachelor thesis contains introduction of the helicopter techniques from the beginning of their development to the present. The work includes complex view on the… (more)

Subjects/Keywords: Helikoptéra; nosnej rotor; rotorová hlava; vyrovnávací rotor; NOTAR; Helicopter; main rotor system; rotor head; tail rotor; NOTAR

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

APA (6th Edition):

Rybka, S. (2019). Dopravní vrtulníky: Air transport helicopters. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/4473

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):

Rybka, Slavomír. “Dopravní vrtulníky: Air transport helicopters.” 2019. Thesis, Brno University of Technology. Accessed March 07, 2021. http://hdl.handle.net/11012/4473.

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

MLA Handbook (7th Edition):

Rybka, Slavomír. “Dopravní vrtulníky: Air transport helicopters.” 2019. Web. 07 Mar 2021.

Vancouver:

Rybka S. Dopravní vrtulníky: Air transport helicopters. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/11012/4473.

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

Council of Science Editors:

Rybka S. Dopravní vrtulníky: Air transport helicopters. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/4473

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


University of Texas – Austin

13. Cameron, Christopher Glenn. Comprehensive aeromechanical measurements of a model-scale, coaxial, counter-rotating rotor system.

Degree: PhD, Aerospace Engineering, 2016, University of Texas – Austin

 With the renewed interest in rigid, counter-rotating coaxial rotor designs, and the increased fidelity of fully coupled CFD/CSD simulations, there exists a lack of comprehensive… (more)

Subjects/Keywords: Helicopter; Rotorcraft; Coaxial; Operational Modal Analysis; Aeroelasticity; Counter-rotating rotor systems; Rotor systems; Rotor designs

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

APA (6th Edition):

Cameron, C. G. (2016). Comprehensive aeromechanical measurements of a model-scale, coaxial, counter-rotating rotor system. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/47136

Chicago Manual of Style (16th Edition):

Cameron, Christopher Glenn. “Comprehensive aeromechanical measurements of a model-scale, coaxial, counter-rotating rotor system.” 2016. Doctoral Dissertation, University of Texas – Austin. Accessed March 07, 2021. http://hdl.handle.net/2152/47136.

MLA Handbook (7th Edition):

Cameron, Christopher Glenn. “Comprehensive aeromechanical measurements of a model-scale, coaxial, counter-rotating rotor system.” 2016. Web. 07 Mar 2021.

Vancouver:

Cameron CG. Comprehensive aeromechanical measurements of a model-scale, coaxial, counter-rotating rotor system. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2016. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/2152/47136.

Council of Science Editors:

Cameron CG. Comprehensive aeromechanical measurements of a model-scale, coaxial, counter-rotating rotor system. [Doctoral Dissertation]. University of Texas – Austin; 2016. Available from: http://hdl.handle.net/2152/47136


Penn State University

14. Reich, David B. Water Tunnel Experiments on a Model Scale Helicopter Rotor Hub.

Degree: 2013, Penn State University

 A scaled model of a notional helicopter rotor hub was tested at hub-diameter-based Reynolds numbers of 2.45 million and 4.9 million based on the hub… (more)

Subjects/Keywords: Helicopter; Rotorcraft; Fluids; Fluid Dynamics; Experimental Fluid Dynamics; Experimental; Rotor; Rotor Hub; Water Tunnel

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APA (6th Edition):

Reich, D. B. (2013). Water Tunnel Experiments on a Model Scale Helicopter Rotor Hub. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/19791

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):

Reich, David B. “Water Tunnel Experiments on a Model Scale Helicopter Rotor Hub.” 2013. Thesis, Penn State University. Accessed March 07, 2021. https://submit-etda.libraries.psu.edu/catalog/19791.

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

MLA Handbook (7th Edition):

Reich, David B. “Water Tunnel Experiments on a Model Scale Helicopter Rotor Hub.” 2013. Web. 07 Mar 2021.

Vancouver:

Reich DB. Water Tunnel Experiments on a Model Scale Helicopter Rotor Hub. [Internet] [Thesis]. Penn State University; 2013. [cited 2021 Mar 07]. Available from: https://submit-etda.libraries.psu.edu/catalog/19791.

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

Council of Science Editors:

Reich DB. Water Tunnel Experiments on a Model Scale Helicopter Rotor Hub. [Thesis]. Penn State University; 2013. Available from: https://submit-etda.libraries.psu.edu/catalog/19791

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

15. Roca León, Enric. Simulations aéro-mécaniques pour l'optimisation de rotors d'hélicoptère en vol d'avancement : Aeromechanical simulations for the optimization of helicopter rotors in forward flight.

Degree: Docteur es, Mathématiques appliquées, 2014, Nice

Un cadre d'optimisation multi-Objectif pour les pales d'hélicoptère est développé en utilisant des modèles de simulation de haute fidélité. Des fonctions objectives caractérisant la performance… (more)

Subjects/Keywords: Optimisation; Jeu de Nash; Hélicoptère; Rotor; Aérodynamique; Optimization; Nash game; Helicopter; Rotor; Aerodynamics

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

APA (6th Edition):

Roca León, E. (2014). Simulations aéro-mécaniques pour l'optimisation de rotors d'hélicoptère en vol d'avancement : Aeromechanical simulations for the optimization of helicopter rotors in forward flight. (Doctoral Dissertation). Nice. Retrieved from http://www.theses.fr/2014NICE4076

Chicago Manual of Style (16th Edition):

Roca León, Enric. “Simulations aéro-mécaniques pour l'optimisation de rotors d'hélicoptère en vol d'avancement : Aeromechanical simulations for the optimization of helicopter rotors in forward flight.” 2014. Doctoral Dissertation, Nice. Accessed March 07, 2021. http://www.theses.fr/2014NICE4076.

MLA Handbook (7th Edition):

Roca León, Enric. “Simulations aéro-mécaniques pour l'optimisation de rotors d'hélicoptère en vol d'avancement : Aeromechanical simulations for the optimization of helicopter rotors in forward flight.” 2014. Web. 07 Mar 2021.

Vancouver:

Roca León E. Simulations aéro-mécaniques pour l'optimisation de rotors d'hélicoptère en vol d'avancement : Aeromechanical simulations for the optimization of helicopter rotors in forward flight. [Internet] [Doctoral dissertation]. Nice; 2014. [cited 2021 Mar 07]. Available from: http://www.theses.fr/2014NICE4076.

Council of Science Editors:

Roca León E. Simulations aéro-mécaniques pour l'optimisation de rotors d'hélicoptère en vol d'avancement : Aeromechanical simulations for the optimization of helicopter rotors in forward flight. [Doctoral Dissertation]. Nice; 2014. Available from: http://www.theses.fr/2014NICE4076

16. Velkova, Cvetelina Vladimirova. Modélisation du comportement dynamique des rotors d’hélicoptères : Modeling the dynamics of helicopter's rotor.

Degree: Docteur es, Navigation, gestion et fonctionnement du transport aérien, 2013, Paris, ENSAM

Modélisation du comportement dynamique des rotors d'hélicoptèresL'objectif de la thèse est l'étude et la modélisation du comportement dynamique et aérodynamique du rotor de l'hélicoptère en… (more)

Subjects/Keywords: Modélisation; Dynamique; Rotor; Hélicoptère; Aérodynamique; Simulation; Modeling; Dynamics; Main rotor; Helicopter; Aerodynamics; Simulation

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

APA (6th Edition):

Velkova, C. V. (2013). Modélisation du comportement dynamique des rotors d’hélicoptères : Modeling the dynamics of helicopter's rotor. (Doctoral Dissertation). Paris, ENSAM. Retrieved from http://www.theses.fr/2013ENAM0055

Chicago Manual of Style (16th Edition):

Velkova, Cvetelina Vladimirova. “Modélisation du comportement dynamique des rotors d’hélicoptères : Modeling the dynamics of helicopter's rotor.” 2013. Doctoral Dissertation, Paris, ENSAM. Accessed March 07, 2021. http://www.theses.fr/2013ENAM0055.

MLA Handbook (7th Edition):

Velkova, Cvetelina Vladimirova. “Modélisation du comportement dynamique des rotors d’hélicoptères : Modeling the dynamics of helicopter's rotor.” 2013. Web. 07 Mar 2021.

Vancouver:

Velkova CV. Modélisation du comportement dynamique des rotors d’hélicoptères : Modeling the dynamics of helicopter's rotor. [Internet] [Doctoral dissertation]. Paris, ENSAM; 2013. [cited 2021 Mar 07]. Available from: http://www.theses.fr/2013ENAM0055.

Council of Science Editors:

Velkova CV. Modélisation du comportement dynamique des rotors d’hélicoptères : Modeling the dynamics of helicopter's rotor. [Doctoral Dissertation]. Paris, ENSAM; 2013. Available from: http://www.theses.fr/2013ENAM0055


Penn State University

17. Corl, Jonas Daniel. A COMPARISON OF HELICOPTER ACTIVE ROTOR GUST REJECTION AND VIBRATION ALLEVIATION METHODS .

Degree: 2009, Penn State University

 Dynamic Interface (DI) tasks such as station keeping, takeoff, and landing during helicopter-ship interactions are often unacceptably workload-intensive due not only to close quarters and… (more)

Subjects/Keywords: helicopter; swashplate; active rotor

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APA (6th Edition):

Corl, J. D. (2009). A COMPARISON OF HELICOPTER ACTIVE ROTOR GUST REJECTION AND VIBRATION ALLEVIATION METHODS . (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/9978

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):

Corl, Jonas Daniel. “A COMPARISON OF HELICOPTER ACTIVE ROTOR GUST REJECTION AND VIBRATION ALLEVIATION METHODS .” 2009. Thesis, Penn State University. Accessed March 07, 2021. https://submit-etda.libraries.psu.edu/catalog/9978.

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

MLA Handbook (7th Edition):

Corl, Jonas Daniel. “A COMPARISON OF HELICOPTER ACTIVE ROTOR GUST REJECTION AND VIBRATION ALLEVIATION METHODS .” 2009. Web. 07 Mar 2021.

Vancouver:

Corl JD. A COMPARISON OF HELICOPTER ACTIVE ROTOR GUST REJECTION AND VIBRATION ALLEVIATION METHODS . [Internet] [Thesis]. Penn State University; 2009. [cited 2021 Mar 07]. Available from: https://submit-etda.libraries.psu.edu/catalog/9978.

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

Council of Science Editors:

Corl JD. A COMPARISON OF HELICOPTER ACTIVE ROTOR GUST REJECTION AND VIBRATION ALLEVIATION METHODS . [Thesis]. Penn State University; 2009. Available from: https://submit-etda.libraries.psu.edu/catalog/9978

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


Penn State University

18. Chen, Hsuan-nien. Rotor Noise in Maneuvering Flight .

Degree: 2008, Penn State University

 The objective of this research is to understand the physics of rotor noise in the maneuvering flight. To achieve this objective, an integrated noise prediction… (more)

Subjects/Keywords: Maneuvering; Rotor noise; Helicopter

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

APA (6th Edition):

Chen, H. (2008). Rotor Noise in Maneuvering Flight . (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/7286

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):

Chen, Hsuan-nien. “Rotor Noise in Maneuvering Flight .” 2008. Thesis, Penn State University. Accessed March 07, 2021. https://submit-etda.libraries.psu.edu/catalog/7286.

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

MLA Handbook (7th Edition):

Chen, Hsuan-nien. “Rotor Noise in Maneuvering Flight .” 2008. Web. 07 Mar 2021.

Vancouver:

Chen H. Rotor Noise in Maneuvering Flight . [Internet] [Thesis]. Penn State University; 2008. [cited 2021 Mar 07]. Available from: https://submit-etda.libraries.psu.edu/catalog/7286.

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

Council of Science Editors:

Chen H. Rotor Noise in Maneuvering Flight . [Thesis]. Penn State University; 2008. Available from: https://submit-etda.libraries.psu.edu/catalog/7286

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


Penn State University

19. Barron, Heather Marie. Acoustic Analysis of Compound Helicopters with Trim Variations.

Degree: 2013, Penn State University

 This thesis presents a prediction method that analyzes the acoustic radiation of compound helicopters when trim is varied. The goal of this thesis was to… (more)

Subjects/Keywords: Helicopter; rotorcraft; rotor; craft; acoustic; WOPWOP; PSU-WOPWOP; aerospace; compound; analysis

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

APA (6th Edition):

Barron, H. M. (2013). Acoustic Analysis of Compound Helicopters with Trim Variations. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/19082

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):

Barron, Heather Marie. “Acoustic Analysis of Compound Helicopters with Trim Variations.” 2013. Thesis, Penn State University. Accessed March 07, 2021. https://submit-etda.libraries.psu.edu/catalog/19082.

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

MLA Handbook (7th Edition):

Barron, Heather Marie. “Acoustic Analysis of Compound Helicopters with Trim Variations.” 2013. Web. 07 Mar 2021.

Vancouver:

Barron HM. Acoustic Analysis of Compound Helicopters with Trim Variations. [Internet] [Thesis]. Penn State University; 2013. [cited 2021 Mar 07]. Available from: https://submit-etda.libraries.psu.edu/catalog/19082.

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

Council of Science Editors:

Barron HM. Acoustic Analysis of Compound Helicopters with Trim Variations. [Thesis]. Penn State University; 2013. Available from: https://submit-etda.libraries.psu.edu/catalog/19082

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


Penn State University

20. Treacy, Shawn Michael. STABILITY ANALYSIS AND EXPERIMENTAL TESTING OF FLUIDIC PITCH LINKS IN HELICOPTERS WITH ARTICULATED ROTORS.

Degree: 2017, Penn State University

 Vibration levels in helicopters impact many aspects of flight including performance, comfort, and reliability. Three types of vibration control exist to dissipate these effects: passive… (more)

Subjects/Keywords: fluidic pitch link; FPL; stability; articulated; helicopter; experiment; test; rotor

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APA (6th Edition):

Treacy, S. M. (2017). STABILITY ANALYSIS AND EXPERIMENTAL TESTING OF FLUIDIC PITCH LINKS IN HELICOPTERS WITH ARTICULATED ROTORS. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/14572smt249

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):

Treacy, Shawn Michael. “STABILITY ANALYSIS AND EXPERIMENTAL TESTING OF FLUIDIC PITCH LINKS IN HELICOPTERS WITH ARTICULATED ROTORS.” 2017. Thesis, Penn State University. Accessed March 07, 2021. https://submit-etda.libraries.psu.edu/catalog/14572smt249.

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

MLA Handbook (7th Edition):

Treacy, Shawn Michael. “STABILITY ANALYSIS AND EXPERIMENTAL TESTING OF FLUIDIC PITCH LINKS IN HELICOPTERS WITH ARTICULATED ROTORS.” 2017. Web. 07 Mar 2021.

Vancouver:

Treacy SM. STABILITY ANALYSIS AND EXPERIMENTAL TESTING OF FLUIDIC PITCH LINKS IN HELICOPTERS WITH ARTICULATED ROTORS. [Internet] [Thesis]. Penn State University; 2017. [cited 2021 Mar 07]. Available from: https://submit-etda.libraries.psu.edu/catalog/14572smt249.

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

Council of Science Editors:

Treacy SM. STABILITY ANALYSIS AND EXPERIMENTAL TESTING OF FLUIDIC PITCH LINKS IN HELICOPTERS WITH ARTICULATED ROTORS. [Thesis]. Penn State University; 2017. Available from: https://submit-etda.libraries.psu.edu/catalog/14572smt249

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


Penn State University

21. Hayden, Eric William. Design and Testing of a Helicopter Rotor Blade Chord Extension System.

Degree: 2012, Penn State University

 In high gross weight, high altitude, and high speed operations, the helicopter main rotor is susceptible to stall. The onset of stall both limits the… (more)

Subjects/Keywords: aerospace; helicopter; morphing; rotor; chord; extension; design; test

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

APA (6th Edition):

Hayden, E. W. (2012). Design and Testing of a Helicopter Rotor Blade Chord Extension System. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/15507

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):

Hayden, Eric William. “Design and Testing of a Helicopter Rotor Blade Chord Extension System.” 2012. Thesis, Penn State University. Accessed March 07, 2021. https://submit-etda.libraries.psu.edu/catalog/15507.

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

MLA Handbook (7th Edition):

Hayden, Eric William. “Design and Testing of a Helicopter Rotor Blade Chord Extension System.” 2012. Web. 07 Mar 2021.

Vancouver:

Hayden EW. Design and Testing of a Helicopter Rotor Blade Chord Extension System. [Internet] [Thesis]. Penn State University; 2012. [cited 2021 Mar 07]. Available from: https://submit-etda.libraries.psu.edu/catalog/15507.

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

Council of Science Editors:

Hayden EW. Design and Testing of a Helicopter Rotor Blade Chord Extension System. [Thesis]. Penn State University; 2012. Available from: https://submit-etda.libraries.psu.edu/catalog/15507

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


Penn State University

22. Corle, Ethan Lewis. Optimization of Active Flap Deployment for Efficient In-plane Rotor Noise Reduction.

Degree: 2015, Penn State University

 Active rotor concepts have been shown to effectively target helicopter acoustics, performance, or vibrations. This work focuses on a conceptual integrated optimization scheme in which… (more)

Subjects/Keywords: active flap; rotor noise; aeroacoustics; genetic algorithm; helicopter quieting

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APA (6th Edition):

Corle, E. L. (2015). Optimization of Active Flap Deployment for Efficient In-plane Rotor Noise Reduction. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/26651

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):

Corle, Ethan Lewis. “Optimization of Active Flap Deployment for Efficient In-plane Rotor Noise Reduction.” 2015. Thesis, Penn State University. Accessed March 07, 2021. https://submit-etda.libraries.psu.edu/catalog/26651.

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

MLA Handbook (7th Edition):

Corle, Ethan Lewis. “Optimization of Active Flap Deployment for Efficient In-plane Rotor Noise Reduction.” 2015. Web. 07 Mar 2021.

Vancouver:

Corle EL. Optimization of Active Flap Deployment for Efficient In-plane Rotor Noise Reduction. [Internet] [Thesis]. Penn State University; 2015. [cited 2021 Mar 07]. Available from: https://submit-etda.libraries.psu.edu/catalog/26651.

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

Council of Science Editors:

Corle EL. Optimization of Active Flap Deployment for Efficient In-plane Rotor Noise Reduction. [Thesis]. Penn State University; 2015. Available from: https://submit-etda.libraries.psu.edu/catalog/26651

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


Penn State University

23. Quintangeli, Michael Vincent. AN ENERGY HARVESTING DEVICE FOR POWERING ROTOR LOAD MONITORING SENSORS .

Degree: 2011, Penn State University

 Health and Usage Monitoring Systems (HUMS) are designed to improve safety, increase operational efficiency, and reduce the cost of owning and operating a helicopter. They… (more)

Subjects/Keywords: rotor; electromechanical; electromagnetic; pitch link; helicopter; energy harvesting; rod end; HUMS

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APA (6th Edition):

Quintangeli, M. V. (2011). AN ENERGY HARVESTING DEVICE FOR POWERING ROTOR LOAD MONITORING SENSORS . (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/12422

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):

Quintangeli, Michael Vincent. “AN ENERGY HARVESTING DEVICE FOR POWERING ROTOR LOAD MONITORING SENSORS .” 2011. Thesis, Penn State University. Accessed March 07, 2021. https://submit-etda.libraries.psu.edu/catalog/12422.

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

MLA Handbook (7th Edition):

Quintangeli, Michael Vincent. “AN ENERGY HARVESTING DEVICE FOR POWERING ROTOR LOAD MONITORING SENSORS .” 2011. Web. 07 Mar 2021.

Vancouver:

Quintangeli MV. AN ENERGY HARVESTING DEVICE FOR POWERING ROTOR LOAD MONITORING SENSORS . [Internet] [Thesis]. Penn State University; 2011. [cited 2021 Mar 07]. Available from: https://submit-etda.libraries.psu.edu/catalog/12422.

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

Council of Science Editors:

Quintangeli MV. AN ENERGY HARVESTING DEVICE FOR POWERING ROTOR LOAD MONITORING SENSORS . [Thesis]. Penn State University; 2011. Available from: https://submit-etda.libraries.psu.edu/catalog/12422

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

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

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

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Droz, Christophe. “Guidage des ondes d'ordre élevé dans les composites : application au dégivrage en vol des pales d'hélicoptères : High-order wave propagation in composite waveguides : application to in-flight de-icing of helicopter rotor blades.” 2015. Doctoral Dissertation, Ecully, Ecole centrale de Lyon. Accessed March 07, 2021. http://www.theses.fr/2015ECDL0026.

MLA Handbook (7th Edition):

Droz, Christophe. “Guidage des ondes d'ordre élevé dans les composites : application au dégivrage en vol des pales d'hélicoptères : High-order wave propagation in composite waveguides : application to in-flight de-icing of helicopter rotor blades.” 2015. Web. 07 Mar 2021.

Vancouver:

Droz C. Guidage des ondes d'ordre élevé dans les composites : application au dégivrage en vol des pales d'hélicoptères : High-order wave propagation in composite waveguides : application to in-flight de-icing of helicopter rotor blades. [Internet] [Doctoral dissertation]. Ecully, Ecole centrale de Lyon; 2015. [cited 2021 Mar 07]. Available from: http://www.theses.fr/2015ECDL0026.

Council of Science Editors:

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


Georgia Tech

25. Schatzman, Natasha Lydia. Aerodynamics and aeroacoustic sources of a coaxial rotor.

Degree: PhD, Aerospace Engineering, 2018, Georgia Tech

 Vehicles with coaxial, contra-rotating rotor systems (CACR) are being considered for a range of applications, including those requiring high speed and operations in urban environments.… (more)

Subjects/Keywords: Rotorcraft; Helicopter; Coaxial; Noise; Aerodynamics; Aeroacoustic; Rotor; CFD

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APA (6th Edition):

Schatzman, N. L. (2018). Aerodynamics and aeroacoustic sources of a coaxial rotor. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/59922

Chicago Manual of Style (16th Edition):

Schatzman, Natasha Lydia. “Aerodynamics and aeroacoustic sources of a coaxial rotor.” 2018. Doctoral Dissertation, Georgia Tech. Accessed March 07, 2021. http://hdl.handle.net/1853/59922.

MLA Handbook (7th Edition):

Schatzman, Natasha Lydia. “Aerodynamics and aeroacoustic sources of a coaxial rotor.” 2018. Web. 07 Mar 2021.

Vancouver:

Schatzman NL. Aerodynamics and aeroacoustic sources of a coaxial rotor. [Internet] [Doctoral dissertation]. Georgia Tech; 2018. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/1853/59922.

Council of Science Editors:

Schatzman NL. Aerodynamics and aeroacoustic sources of a coaxial rotor. [Doctoral Dissertation]. Georgia Tech; 2018. Available from: http://hdl.handle.net/1853/59922


University of Maryland

26. Berry, Benjamin Otto. Fundamental Understanding of Rotor Aeromechanics at High Advance Ratio Through Wind Tunnel Testing.

Degree: Aerospace Engineering, 2016, University of Maryland

 The purpose of this research is to further the understanding of rotor aeromechanics at advance ratios (mu) beyond the maximum of 0.5 (ratio of forward… (more)

Subjects/Keywords: Aerospace engineering; Helicopter; High Advance Ratio; Rotor; Rotorcraft; Slowed; Wind Tunnel

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APA (6th Edition):

Berry, B. O. (2016). Fundamental Understanding of Rotor Aeromechanics at High Advance Ratio Through Wind Tunnel Testing. (Thesis). University of Maryland. Retrieved from http://hdl.handle.net/1903/19318

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):

Berry, Benjamin Otto. “Fundamental Understanding of Rotor Aeromechanics at High Advance Ratio Through Wind Tunnel Testing.” 2016. Thesis, University of Maryland. Accessed March 07, 2021. http://hdl.handle.net/1903/19318.

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

MLA Handbook (7th Edition):

Berry, Benjamin Otto. “Fundamental Understanding of Rotor Aeromechanics at High Advance Ratio Through Wind Tunnel Testing.” 2016. Web. 07 Mar 2021.

Vancouver:

Berry BO. Fundamental Understanding of Rotor Aeromechanics at High Advance Ratio Through Wind Tunnel Testing. [Internet] [Thesis]. University of Maryland; 2016. [cited 2021 Mar 07]. Available from: http://hdl.handle.net/1903/19318.

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

Council of Science Editors:

Berry BO. Fundamental Understanding of Rotor Aeromechanics at High Advance Ratio Through Wind Tunnel Testing. [Thesis]. University of Maryland; 2016. Available from: http://hdl.handle.net/1903/19318

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


Indian Institute of Science

27. Chandra Sekhar, D. Efficient Trim In Helicopter Aeroelastic Analysis.

Degree: MSc Engg, Faculty of Engineering, 2011, Indian Institute of Science

Helicopter aeroelastic analysis is highly complex and multidisciplinary in nature; the flexibility of main rotor blades is coupled with aerodynamics, dynamics and control systems. A… (more)

Subjects/Keywords: Helicopter - Aeroelasticity; Helicopter Rotor Blades; Helicopters - Aerolastic Analysis; Rotocraft Trim; Helicopters - Trim Analysis; Rotors (Helicopters); Helicopter Trim - Numerical Analysis; Rotors - Aeroelastic Optimization; Aeroelastic Analysis; Helicopter Trim; Aeronautics

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

APA (6th Edition):

Chandra Sekhar, D. (2011). Efficient Trim In Helicopter Aeroelastic Analysis. (Masters Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ac.in/handle/2005/1118

Chicago Manual of Style (16th Edition):

Chandra Sekhar, D. “Efficient Trim In Helicopter Aeroelastic Analysis.” 2011. Masters Thesis, Indian Institute of Science. Accessed March 07, 2021. http://etd.iisc.ac.in/handle/2005/1118.

MLA Handbook (7th Edition):

Chandra Sekhar, D. “Efficient Trim In Helicopter Aeroelastic Analysis.” 2011. Web. 07 Mar 2021.

Vancouver:

Chandra Sekhar D. Efficient Trim In Helicopter Aeroelastic Analysis. [Internet] [Masters thesis]. Indian Institute of Science; 2011. [cited 2021 Mar 07]. Available from: http://etd.iisc.ac.in/handle/2005/1118.

Council of Science Editors:

Chandra Sekhar D. Efficient Trim In Helicopter Aeroelastic Analysis. [Masters Thesis]. Indian Institute of Science; 2011. Available from: http://etd.iisc.ac.in/handle/2005/1118


Indian Institute of Science

28. Suresh, J K. Response, Loads And Stabillity Of Helicopters With Interconnected Rotor Blades.

Degree: PhD, Faculty of Engineering, 2012, Indian Institute of Science

Subjects/Keywords: Helicopter - Compressor Blades; Rotors (Helicopter) - Compressor Blades; Rotor Blades - Load; Rotor Blades - Stability; Rotors; Rotor-Body Systems; Helicopter Rotor Blades; Aeronautics

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

APA (6th Edition):

Suresh, J. K. (2012). Response, Loads And Stabillity Of Helicopters With Interconnected Rotor Blades. (Doctoral Dissertation). Indian Institute of Science. Retrieved from http://etd.iisc.ac.in/handle/2005/1861

Chicago Manual of Style (16th Edition):

Suresh, J K. “Response, Loads And Stabillity Of Helicopters With Interconnected Rotor Blades.” 2012. Doctoral Dissertation, Indian Institute of Science. Accessed March 07, 2021. http://etd.iisc.ac.in/handle/2005/1861.

MLA Handbook (7th Edition):

Suresh, J K. “Response, Loads And Stabillity Of Helicopters With Interconnected Rotor Blades.” 2012. Web. 07 Mar 2021.

Vancouver:

Suresh JK. Response, Loads And Stabillity Of Helicopters With Interconnected Rotor Blades. [Internet] [Doctoral dissertation]. Indian Institute of Science; 2012. [cited 2021 Mar 07]. Available from: http://etd.iisc.ac.in/handle/2005/1861.

Council of Science Editors:

Suresh JK. Response, Loads And Stabillity Of Helicopters With Interconnected Rotor Blades. [Doctoral Dissertation]. Indian Institute of Science; 2012. Available from: http://etd.iisc.ac.in/handle/2005/1861


Penn State University

29. Reich, David B. Experimental Investigation of A Helicopter Rotor Hub Flow.

Degree: 2017, Penn State University

 The rotor hub system is by far the largest contributor to helicopter parasite drag and a barrier to increasing helicopter forward-flight speed and range. Additionally,… (more)

Subjects/Keywords: Helicopter; Rotorcraft; Aerodynamics; Rotor Hub; Hub Drag; Rotor Hub Drag; Rotorcraft Aerodynamics; Rotorcraft Aeromechanics; Unsteady Aerodynamics

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

APA (6th Edition):

Reich, D. B. (2017). Experimental Investigation of A Helicopter Rotor Hub Flow. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/14509dbr141

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):

Reich, David B. “Experimental Investigation of A Helicopter Rotor Hub Flow.” 2017. Thesis, Penn State University. Accessed March 07, 2021. https://submit-etda.libraries.psu.edu/catalog/14509dbr141.

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

MLA Handbook (7th Edition):

Reich, David B. “Experimental Investigation of A Helicopter Rotor Hub Flow.” 2017. Web. 07 Mar 2021.

Vancouver:

Reich DB. Experimental Investigation of A Helicopter Rotor Hub Flow. [Internet] [Thesis]. Penn State University; 2017. [cited 2021 Mar 07]. Available from: https://submit-etda.libraries.psu.edu/catalog/14509dbr141.

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

Council of Science Editors:

Reich DB. Experimental Investigation of A Helicopter Rotor Hub Flow. [Thesis]. Penn State University; 2017. Available from: https://submit-etda.libraries.psu.edu/catalog/14509dbr141

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


Indian Institute of Science

30. Mallick, Rajnish. Design and Development of Piezoelectric Stack Actuated Trailing Edge Flap for Helicopter Vibration Reduction.

Degree: PhD, Faculty of Engineering, 2018, Indian Institute of Science

 This research investigates on-blade partial span active plain trailing edge flaps (TEFs)with an aim to alleviate the helicopter vibrations. Among all the available smart materials,… (more)

Subjects/Keywords: Piezoelectric Stack Actuators; Helicopter Vibration Control; Trailing Edge Flaps (TEFs); Helicopter Aeroelastic Analysis; Rotors (Helicopters); Piezoelectric Actuator Hysteresis; Flaps (Airplanes); Heicopte r- Aerodynamics; Aeroelastic Optimization; Helicopter Rotor Blades; Helicopter Vibrations; Helicopter Vibration Reduction; Helicopter Trailing Edge Flap; Piezoelectric Stack Actuator (PEA); Aerospace Engineering

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

APA (6th Edition):

Mallick, R. (2018). Design and Development of Piezoelectric Stack Actuated Trailing Edge Flap for Helicopter Vibration Reduction. (Doctoral Dissertation). Indian Institute of Science. Retrieved from http://etd.iisc.ac.in/handle/2005/2990

Chicago Manual of Style (16th Edition):

Mallick, Rajnish. “Design and Development of Piezoelectric Stack Actuated Trailing Edge Flap for Helicopter Vibration Reduction.” 2018. Doctoral Dissertation, Indian Institute of Science. Accessed March 07, 2021. http://etd.iisc.ac.in/handle/2005/2990.

MLA Handbook (7th Edition):

Mallick, Rajnish. “Design and Development of Piezoelectric Stack Actuated Trailing Edge Flap for Helicopter Vibration Reduction.” 2018. Web. 07 Mar 2021.

Vancouver:

Mallick R. Design and Development of Piezoelectric Stack Actuated Trailing Edge Flap for Helicopter Vibration Reduction. [Internet] [Doctoral dissertation]. Indian Institute of Science; 2018. [cited 2021 Mar 07]. Available from: http://etd.iisc.ac.in/handle/2005/2990.

Council of Science Editors:

Mallick R. Design and Development of Piezoelectric Stack Actuated Trailing Edge Flap for Helicopter Vibration Reduction. [Doctoral Dissertation]. Indian Institute of Science; 2018. Available from: http://etd.iisc.ac.in/handle/2005/2990

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