Advanced search options

Advanced Search Options 🞨

Browse by author name (“Author name starts with…”).

Find ETDs with:

in
/  
in
/  
in
/  
in

Written in Published in Earliest date Latest date

Sorted by

Results per page:

Sorted by: relevance · author · university · dateNew search

You searched for subject:(Airfoil noise). Showing records 1 – 20 of 20 total matches.

Search Limiters

Last 2 Years | English Only

No search limiters apply to these results.

▼ Search Limiters


University of Adelaide

1. Laratro, Alex James. Self-noise of Airfoils Under Stalled Conditions.

Degree: 2017, University of Adelaide

 In recent years there have been reports of a transient impulsive noise signature being produced sporadically by wind turbines. Impulsive noise, where the noise level… (more)

Subjects/Keywords: Stall noise; Airfoil noise; Wind energy

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Laratro, A. J. (2017). Self-noise of Airfoils Under Stalled Conditions. (Thesis). University of Adelaide. Retrieved from http://hdl.handle.net/2440/119324

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):

Laratro, Alex James. “Self-noise of Airfoils Under Stalled Conditions.” 2017. Thesis, University of Adelaide. Accessed July 05, 2020. http://hdl.handle.net/2440/119324.

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

MLA Handbook (7th Edition):

Laratro, Alex James. “Self-noise of Airfoils Under Stalled Conditions.” 2017. Web. 05 Jul 2020.

Vancouver:

Laratro AJ. Self-noise of Airfoils Under Stalled Conditions. [Internet] [Thesis]. University of Adelaide; 2017. [cited 2020 Jul 05]. Available from: http://hdl.handle.net/2440/119324.

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

Council of Science Editors:

Laratro AJ. Self-noise of Airfoils Under Stalled Conditions. [Thesis]. University of Adelaide; 2017. Available from: http://hdl.handle.net/2440/119324

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

2. Botha, Jason. Predictions of Rotor Broadband Noise.

Degree: School of Engineering. Discipline of Mechanical & Manuf. Eng, 2018, Trinity College Dublin

 This thesis presents an enhanced method for predicting aerodynamically generated broadband noise, produced by rotating machinery. The method improves on existing work for Vertical Axis… (more)

Subjects/Keywords: Wind Turbine Noise; Aeroacoustics; Broadband Noise; Airfoil Noise; Computational Fluid Dynamics; Vertical Axis Wind Turbine

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Botha, J. (2018). Predictions of Rotor Broadband Noise. (Thesis). Trinity College Dublin. Retrieved from http://hdl.handle.net/2262/82699

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):

Botha, Jason. “Predictions of Rotor Broadband Noise.” 2018. Thesis, Trinity College Dublin. Accessed July 05, 2020. http://hdl.handle.net/2262/82699.

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

MLA Handbook (7th Edition):

Botha, Jason. “Predictions of Rotor Broadband Noise.” 2018. Web. 05 Jul 2020.

Vancouver:

Botha J. Predictions of Rotor Broadband Noise. [Internet] [Thesis]. Trinity College Dublin; 2018. [cited 2020 Jul 05]. Available from: http://hdl.handle.net/2262/82699.

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

Council of Science Editors:

Botha J. Predictions of Rotor Broadband Noise. [Thesis]. Trinity College Dublin; 2018. Available from: http://hdl.handle.net/2262/82699

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


Brunel University

3. Vathylakis, Alexandros. Reduction of broadband trailing edge noise by serrations.

Degree: PhD, 2015, Brunel University

 This thesis aims to investigate and reduce the aerodynamic noise source known as trailing edge noise, or airfoil self-noise, by using passive flow control techniques.… (more)

Subjects/Keywords: 629.134; Poro-serrations; Airfoil noise; Aeroacoustics; Flow control; Porous material

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Vathylakis, A. (2015). Reduction of broadband trailing edge noise by serrations. (Doctoral Dissertation). Brunel University. Retrieved from http://bura.brunel.ac.uk/handle/2438/11554 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.669131

Chicago Manual of Style (16th Edition):

Vathylakis, Alexandros. “Reduction of broadband trailing edge noise by serrations.” 2015. Doctoral Dissertation, Brunel University. Accessed July 05, 2020. http://bura.brunel.ac.uk/handle/2438/11554 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.669131.

MLA Handbook (7th Edition):

Vathylakis, Alexandros. “Reduction of broadband trailing edge noise by serrations.” 2015. Web. 05 Jul 2020.

Vancouver:

Vathylakis A. Reduction of broadband trailing edge noise by serrations. [Internet] [Doctoral dissertation]. Brunel University; 2015. [cited 2020 Jul 05]. Available from: http://bura.brunel.ac.uk/handle/2438/11554 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.669131.

Council of Science Editors:

Vathylakis A. Reduction of broadband trailing edge noise by serrations. [Doctoral Dissertation]. Brunel University; 2015. Available from: http://bura.brunel.ac.uk/handle/2438/11554 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.669131


University of Waterloo

4. Tam, Nicholas. An Aeroacoustic Study of Airfoil Self-Noise for Wind Turbine Applications.

Degree: 2017, University of Waterloo

 The current study addresses the issue of noise relating to both large and small scale wind turbines. In utility scale applications, larger size rotors in… (more)

Subjects/Keywords: Wind Turbine Noise; Aeroacoustics; Airfoil Self-Noise; Laminar Boundary Layer-Vortex Shedding Noise; IEC 61400-11; Tonal Noise; Sound

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Tam, N. (2017). An Aeroacoustic Study of Airfoil Self-Noise for Wind Turbine Applications. (Thesis). University of Waterloo. Retrieved from http://hdl.handle.net/10012/11736

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):

Tam, Nicholas. “An Aeroacoustic Study of Airfoil Self-Noise for Wind Turbine Applications.” 2017. Thesis, University of Waterloo. Accessed July 05, 2020. http://hdl.handle.net/10012/11736.

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

MLA Handbook (7th Edition):

Tam, Nicholas. “An Aeroacoustic Study of Airfoil Self-Noise for Wind Turbine Applications.” 2017. Web. 05 Jul 2020.

Vancouver:

Tam N. An Aeroacoustic Study of Airfoil Self-Noise for Wind Turbine Applications. [Internet] [Thesis]. University of Waterloo; 2017. [cited 2020 Jul 05]. Available from: http://hdl.handle.net/10012/11736.

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

Council of Science Editors:

Tam N. An Aeroacoustic Study of Airfoil Self-Noise for Wind Turbine Applications. [Thesis]. University of Waterloo; 2017. Available from: http://hdl.handle.net/10012/11736

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


Iowa State University

5. Agrawal, Bharat Raj. Modeling fan broadband noise from jet engines and rod-airfoil benchmark case for broadband noise prediction.

Degree: 2015, Iowa State University

 This work has two primary parts: (1) an exhaustive literature review highlighting the need and the direction to study broadband noise generation from the fan… (more)

Subjects/Keywords: Aerospace Engineering; Amiet's theory; computational aeroacoustics; fan broadband noise; openfoam; rod-airfoil noise; Aerospace Engineering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Agrawal, B. R. (2015). Modeling fan broadband noise from jet engines and rod-airfoil benchmark case for broadband noise prediction. (Thesis). Iowa State University. Retrieved from https://lib.dr.iastate.edu/etd/14326

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):

Agrawal, Bharat Raj. “Modeling fan broadband noise from jet engines and rod-airfoil benchmark case for broadband noise prediction.” 2015. Thesis, Iowa State University. Accessed July 05, 2020. https://lib.dr.iastate.edu/etd/14326.

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

MLA Handbook (7th Edition):

Agrawal, Bharat Raj. “Modeling fan broadband noise from jet engines and rod-airfoil benchmark case for broadband noise prediction.” 2015. Web. 05 Jul 2020.

Vancouver:

Agrawal BR. Modeling fan broadband noise from jet engines and rod-airfoil benchmark case for broadband noise prediction. [Internet] [Thesis]. Iowa State University; 2015. [cited 2020 Jul 05]. Available from: https://lib.dr.iastate.edu/etd/14326.

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

Council of Science Editors:

Agrawal BR. Modeling fan broadband noise from jet engines and rod-airfoil benchmark case for broadband noise prediction. [Thesis]. Iowa State University; 2015. Available from: https://lib.dr.iastate.edu/etd/14326

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


University of New South Wales

6. Zajamsek, Branko. Experimental investigation into airfoil self-noise, blade-tower interaction noise and wind farm noise character.

Degree: Mechanical & Manufacturing Engineering, 2017, University of New South Wales

 An experimental investigation into airfoil self-noise (trailing edge noise, tip vortex formation noise and bluntness trailing edge noise) and blade-tower interaction (BTI) noise from rotating… (more)

Subjects/Keywords: trailing edge noise; wind farm noise; airfoil self-noise; low-frequency noise; infrasound; blade-tower interaction noise; BTI; blade passage effect noise

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Zajamsek, B. (2017). Experimental investigation into airfoil self-noise, blade-tower interaction noise and wind farm noise character. (Doctoral Dissertation). University of New South Wales. Retrieved from http://handle.unsw.edu.au/1959.4/57370 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:43334/SOURCE02?view=true

Chicago Manual of Style (16th Edition):

Zajamsek, Branko. “Experimental investigation into airfoil self-noise, blade-tower interaction noise and wind farm noise character.” 2017. Doctoral Dissertation, University of New South Wales. Accessed July 05, 2020. http://handle.unsw.edu.au/1959.4/57370 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:43334/SOURCE02?view=true.

MLA Handbook (7th Edition):

Zajamsek, Branko. “Experimental investigation into airfoil self-noise, blade-tower interaction noise and wind farm noise character.” 2017. Web. 05 Jul 2020.

Vancouver:

Zajamsek B. Experimental investigation into airfoil self-noise, blade-tower interaction noise and wind farm noise character. [Internet] [Doctoral dissertation]. University of New South Wales; 2017. [cited 2020 Jul 05]. Available from: http://handle.unsw.edu.au/1959.4/57370 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:43334/SOURCE02?view=true.

Council of Science Editors:

Zajamsek B. Experimental investigation into airfoil self-noise, blade-tower interaction noise and wind farm noise character. [Doctoral Dissertation]. University of New South Wales; 2017. Available from: http://handle.unsw.edu.au/1959.4/57370 ; https://unsworks.unsw.edu.au/fapi/datastream/unsworks:43334/SOURCE02?view=true


Virginia Tech

7. Errasquin, Leonardo. Airfoil Self-Noise Prediction Using Neural Networks for Wind Turbines.

Degree: MS, Mechanical Engineering, 2009, Virginia Tech

 A neural network prediction method has been developed to compute self-noise of airfoils typically used in wind turbines. The neural networks were trained using experimental… (more)

Subjects/Keywords: Noise; wind turbine; neural network; airfoil

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Errasquin, L. (2009). Airfoil Self-Noise Prediction Using Neural Networks for Wind Turbines. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/35193

Chicago Manual of Style (16th Edition):

Errasquin, Leonardo. “Airfoil Self-Noise Prediction Using Neural Networks for Wind Turbines.” 2009. Masters Thesis, Virginia Tech. Accessed July 05, 2020. http://hdl.handle.net/10919/35193.

MLA Handbook (7th Edition):

Errasquin, Leonardo. “Airfoil Self-Noise Prediction Using Neural Networks for Wind Turbines.” 2009. Web. 05 Jul 2020.

Vancouver:

Errasquin L. Airfoil Self-Noise Prediction Using Neural Networks for Wind Turbines. [Internet] [Masters thesis]. Virginia Tech; 2009. [cited 2020 Jul 05]. Available from: http://hdl.handle.net/10919/35193.

Council of Science Editors:

Errasquin L. Airfoil Self-Noise Prediction Using Neural Networks for Wind Turbines. [Masters Thesis]. Virginia Tech; 2009. Available from: http://hdl.handle.net/10919/35193


University of Waterloo

8. Orlando, Stephen Michael. Laser Doppler Anemometry and Acoustic Measurements of an S822 Airfoil at Low Reynolds Numbers.

Degree: 2011, University of Waterloo

 Experimental aeroacoustic research was conducted on a wind turbine specific airfoil at low Reynolds numbers. The goal of this thesis was to study trailing edge… (more)

Subjects/Keywords: Wind turbine; Aeroacoustics; Airfoil; Phased array; S822; Laser Doppler anemometry; Beamforming; Noise

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Orlando, S. M. (2011). Laser Doppler Anemometry and Acoustic Measurements of an S822 Airfoil at Low Reynolds Numbers. (Thesis). University of Waterloo. Retrieved from http://hdl.handle.net/10012/5864

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):

Orlando, Stephen Michael. “Laser Doppler Anemometry and Acoustic Measurements of an S822 Airfoil at Low Reynolds Numbers.” 2011. Thesis, University of Waterloo. Accessed July 05, 2020. http://hdl.handle.net/10012/5864.

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

MLA Handbook (7th Edition):

Orlando, Stephen Michael. “Laser Doppler Anemometry and Acoustic Measurements of an S822 Airfoil at Low Reynolds Numbers.” 2011. Web. 05 Jul 2020.

Vancouver:

Orlando SM. Laser Doppler Anemometry and Acoustic Measurements of an S822 Airfoil at Low Reynolds Numbers. [Internet] [Thesis]. University of Waterloo; 2011. [cited 2020 Jul 05]. Available from: http://hdl.handle.net/10012/5864.

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

Council of Science Editors:

Orlando SM. Laser Doppler Anemometry and Acoustic Measurements of an S822 Airfoil at Low Reynolds Numbers. [Thesis]. University of Waterloo; 2011. Available from: http://hdl.handle.net/10012/5864

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


University of Waterloo

9. Zilstra, Alison. Computational Aeroacoustic Prediction of Airfoil Self-Noise at Static Angles of Attack.

Degree: 2019, University of Waterloo

 Aeroacoustic noise from wind turbines is often an obstacle in the implementation of wind farms. Reduction of this noise is key to allowing the expansion… (more)

Subjects/Keywords: computational fluid dynamics; computational aeroacoustics; wind turbine noise; static airfoil; SD 7037

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Zilstra, A. (2019). Computational Aeroacoustic Prediction of Airfoil Self-Noise at Static Angles of Attack. (Thesis). University of Waterloo. Retrieved from http://hdl.handle.net/10012/14532

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):

Zilstra, Alison. “Computational Aeroacoustic Prediction of Airfoil Self-Noise at Static Angles of Attack.” 2019. Thesis, University of Waterloo. Accessed July 05, 2020. http://hdl.handle.net/10012/14532.

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

MLA Handbook (7th Edition):

Zilstra, Alison. “Computational Aeroacoustic Prediction of Airfoil Self-Noise at Static Angles of Attack.” 2019. Web. 05 Jul 2020.

Vancouver:

Zilstra A. Computational Aeroacoustic Prediction of Airfoil Self-Noise at Static Angles of Attack. [Internet] [Thesis]. University of Waterloo; 2019. [cited 2020 Jul 05]. Available from: http://hdl.handle.net/10012/14532.

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

Council of Science Editors:

Zilstra A. Computational Aeroacoustic Prediction of Airfoil Self-Noise at Static Angles of Attack. [Thesis]. University of Waterloo; 2019. Available from: http://hdl.handle.net/10012/14532

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


Université de Sherbrooke

10. Wu, Hao. Direct numerical simulation of airfoil self-noise at high Reynolds numbers: Simulation directe du bruit propre de profil à haut nombre de Reynolds.

Degree: 2019, Université de Sherbrooke

 Abstract: This work proposes a numerical study using direct numerical simulation (DNS) to gain a better understanding of the generation mechanisms of the trailing-edge (TE)… (more)

Subjects/Keywords: SND; Aéroacoustique; Bruit au bord de fuite; Profil; DNS; Aeroacoustics; TE Noise; Airfoil

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Wu, H. (2019). Direct numerical simulation of airfoil self-noise at high Reynolds numbers: Simulation directe du bruit propre de profil à haut nombre de Reynolds. (Doctoral Dissertation). Université de Sherbrooke. Retrieved from http://hdl.handle.net/11143/15114

Chicago Manual of Style (16th Edition):

Wu, Hao. “Direct numerical simulation of airfoil self-noise at high Reynolds numbers: Simulation directe du bruit propre de profil à haut nombre de Reynolds.” 2019. Doctoral Dissertation, Université de Sherbrooke. Accessed July 05, 2020. http://hdl.handle.net/11143/15114.

MLA Handbook (7th Edition):

Wu, Hao. “Direct numerical simulation of airfoil self-noise at high Reynolds numbers: Simulation directe du bruit propre de profil à haut nombre de Reynolds.” 2019. Web. 05 Jul 2020.

Vancouver:

Wu H. Direct numerical simulation of airfoil self-noise at high Reynolds numbers: Simulation directe du bruit propre de profil à haut nombre de Reynolds. [Internet] [Doctoral dissertation]. Université de Sherbrooke; 2019. [cited 2020 Jul 05]. Available from: http://hdl.handle.net/11143/15114.

Council of Science Editors:

Wu H. Direct numerical simulation of airfoil self-noise at high Reynolds numbers: Simulation directe du bruit propre de profil à haut nombre de Reynolds. [Doctoral Dissertation]. Université de Sherbrooke; 2019. Available from: http://hdl.handle.net/11143/15114


University of Notre Dame

11. Ahmed Eltaweel. Numerical Investigation of Tandem-Cylinder Aerodynamic Noise and Its Control with Application to Airframe Noise</h1>.

Degree: Aerospace and Mechanical Engineering, 2013, University of Notre Dame

  Prediction and reduction of airframe noise are critically important to the development of quieter civil transport aircraft. The key to noise reduction is a… (more)

Subjects/Keywords: Hybrid Acoustic Approach; Plasma Flow Control; Landing Gear Noise; Active Flow and Noise Control; Tandem Cylinders; Rod-Airfoil Wake Interaction

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Eltaweel, A. (2013). Numerical Investigation of Tandem-Cylinder Aerodynamic Noise and Its Control with Application to Airframe Noise</h1>. (Thesis). University of Notre Dame. Retrieved from https://curate.nd.edu/show/tq57np21m1v

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):

Eltaweel, Ahmed. “Numerical Investigation of Tandem-Cylinder Aerodynamic Noise and Its Control with Application to Airframe Noise</h1>.” 2013. Thesis, University of Notre Dame. Accessed July 05, 2020. https://curate.nd.edu/show/tq57np21m1v.

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

MLA Handbook (7th Edition):

Eltaweel, Ahmed. “Numerical Investigation of Tandem-Cylinder Aerodynamic Noise and Its Control with Application to Airframe Noise</h1>.” 2013. Web. 05 Jul 2020.

Vancouver:

Eltaweel A. Numerical Investigation of Tandem-Cylinder Aerodynamic Noise and Its Control with Application to Airframe Noise</h1>. [Internet] [Thesis]. University of Notre Dame; 2013. [cited 2020 Jul 05]. Available from: https://curate.nd.edu/show/tq57np21m1v.

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

Council of Science Editors:

Eltaweel A. Numerical Investigation of Tandem-Cylinder Aerodynamic Noise and Its Control with Application to Airframe Noise</h1>. [Thesis]. University of Notre Dame; 2013. Available from: https://curate.nd.edu/show/tq57np21m1v

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


Delft University of Technology

12. Mayer, Jonathan (author). Active Change of Permeable Material Properties for Low-Noise Trailing Edge Applications.

Degree: 2019, Delft University of Technology

For many aerospace applications, the dominant airfoil self-noise source is Turbulent Boundary Layer Trailing Edge (TBL-TE) noise. The replacement of solid airfoil trailing edges with… (more)

Subjects/Keywords: porous material; trailing edge noise; polymeric coating; airfoil self-noise; trailing edge heating; aeroacoustic; permeable material

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Mayer, J. (. (2019). Active Change of Permeable Material Properties for Low-Noise Trailing Edge Applications. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:347c4509-16bc-4728-acb2-32a8ccec1c10

Chicago Manual of Style (16th Edition):

Mayer, Jonathan (author). “Active Change of Permeable Material Properties for Low-Noise Trailing Edge Applications.” 2019. Masters Thesis, Delft University of Technology. Accessed July 05, 2020. http://resolver.tudelft.nl/uuid:347c4509-16bc-4728-acb2-32a8ccec1c10.

MLA Handbook (7th Edition):

Mayer, Jonathan (author). “Active Change of Permeable Material Properties for Low-Noise Trailing Edge Applications.” 2019. Web. 05 Jul 2020.

Vancouver:

Mayer J(. Active Change of Permeable Material Properties for Low-Noise Trailing Edge Applications. [Internet] [Masters thesis]. Delft University of Technology; 2019. [cited 2020 Jul 05]. Available from: http://resolver.tudelft.nl/uuid:347c4509-16bc-4728-acb2-32a8ccec1c10.

Council of Science Editors:

Mayer J(. Active Change of Permeable Material Properties for Low-Noise Trailing Edge Applications. [Masters Thesis]. Delft University of Technology; 2019. Available from: http://resolver.tudelft.nl/uuid:347c4509-16bc-4728-acb2-32a8ccec1c10

13. Lysak, Peter Daniel. Unsteady Lift of Thick Airfoils in Incompressible Turbulent Flow.

Degree: PhD, Acoustics, 2011, Penn State University

 The unsteady lift forces that act on an airfoil in turbulent flow are an undesirable source of vibration and noise in many industrial applications. Methods… (more)

Subjects/Keywords: turbulence ingestion noise; airfoil gust response

…Background noise correction applied to the 12.5% thick airfoil. . . . . . . . 116 5.19 Background… …noise correction applied to the 16% thick airfoil. . . . . . . . . 116 5.20 Repeatability of… …Amiet (1977) measured the noise generated by a NACA 0012 airfoil in turbulent flow… …airfoil. They found that the noise from the flat plate and the thin cambered airfoil were well… …the thicker airfoil having up to 10 dB lower noise at high frequencies. Further analysis of… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Lysak, P. D. (2011). Unsteady Lift of Thick Airfoils in Incompressible Turbulent Flow. (Doctoral Dissertation). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/11768

Chicago Manual of Style (16th Edition):

Lysak, Peter Daniel. “Unsteady Lift of Thick Airfoils in Incompressible Turbulent Flow.” 2011. Doctoral Dissertation, Penn State University. Accessed July 05, 2020. https://etda.libraries.psu.edu/catalog/11768.

MLA Handbook (7th Edition):

Lysak, Peter Daniel. “Unsteady Lift of Thick Airfoils in Incompressible Turbulent Flow.” 2011. Web. 05 Jul 2020.

Vancouver:

Lysak PD. Unsteady Lift of Thick Airfoils in Incompressible Turbulent Flow. [Internet] [Doctoral dissertation]. Penn State University; 2011. [cited 2020 Jul 05]. Available from: https://etda.libraries.psu.edu/catalog/11768.

Council of Science Editors:

Lysak PD. Unsteady Lift of Thick Airfoils in Incompressible Turbulent Flow. [Doctoral Dissertation]. Penn State University; 2011. Available from: https://etda.libraries.psu.edu/catalog/11768


Delft University of Technology

14. Pröbsting, S. Airfoil Self-Noise - Investigation with Particle Image Velocimetry.

Degree: 2015, Delft University of Technology

Noise generated aerodynamically by the airflow over a lifting surface is often of concern for applications as diverse as air and ground transportation, heating, ventilation,… (more)

Subjects/Keywords: aeroacoustics; particle image velocimetry; fluid mechanics; trailing edge noise; airfoil self-noise

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Pröbsting, S. (2015). Airfoil Self-Noise - Investigation with Particle Image Velocimetry. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:8a938547-a829-4a79-b77c-a92633a9652a ; urn:NBN:nl:ui:24-uuid:8a938547-a829-4a79-b77c-a92633a9652a ; urn:NBN:nl:ui:24-uuid:8a938547-a829-4a79-b77c-a92633a9652a ; http://resolver.tudelft.nl/uuid:8a938547-a829-4a79-b77c-a92633a9652a

Chicago Manual of Style (16th Edition):

Pröbsting, S. “Airfoil Self-Noise - Investigation with Particle Image Velocimetry.” 2015. Doctoral Dissertation, Delft University of Technology. Accessed July 05, 2020. http://resolver.tudelft.nl/uuid:8a938547-a829-4a79-b77c-a92633a9652a ; urn:NBN:nl:ui:24-uuid:8a938547-a829-4a79-b77c-a92633a9652a ; urn:NBN:nl:ui:24-uuid:8a938547-a829-4a79-b77c-a92633a9652a ; http://resolver.tudelft.nl/uuid:8a938547-a829-4a79-b77c-a92633a9652a.

MLA Handbook (7th Edition):

Pröbsting, S. “Airfoil Self-Noise - Investigation with Particle Image Velocimetry.” 2015. Web. 05 Jul 2020.

Vancouver:

Pröbsting S. Airfoil Self-Noise - Investigation with Particle Image Velocimetry. [Internet] [Doctoral dissertation]. Delft University of Technology; 2015. [cited 2020 Jul 05]. Available from: http://resolver.tudelft.nl/uuid:8a938547-a829-4a79-b77c-a92633a9652a ; urn:NBN:nl:ui:24-uuid:8a938547-a829-4a79-b77c-a92633a9652a ; urn:NBN:nl:ui:24-uuid:8a938547-a829-4a79-b77c-a92633a9652a ; http://resolver.tudelft.nl/uuid:8a938547-a829-4a79-b77c-a92633a9652a.

Council of Science Editors:

Pröbsting S. Airfoil Self-Noise - Investigation with Particle Image Velocimetry. [Doctoral Dissertation]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:8a938547-a829-4a79-b77c-a92633a9652a ; urn:NBN:nl:ui:24-uuid:8a938547-a829-4a79-b77c-a92633a9652a ; urn:NBN:nl:ui:24-uuid:8a938547-a829-4a79-b77c-a92633a9652a ; http://resolver.tudelft.nl/uuid:8a938547-a829-4a79-b77c-a92633a9652a

15. Pagani Júnior, Carlos do Carmo. Mapeamento de fontes aeroacústicas de um eslate em túnel de vento de seção fechada utilizando beam-forming com deconvolução DAMAS.

Degree: PhD, Aeronaves, 2014, University of São Paulo

 A redução do ruído externo gerado por aeronaves operando nas proximidades de grandes centros urbanos é apontada como uma questão vital para a manutenção e… (more)

Subjects/Keywords: Beam-forming acústico; Acoustic beam-forming; Aeroacoustic measurements; Aerofólio hiper-sustentador; Deconvolução DAMAS; Deconvolution DAMAS.; High-lift airfoil; Medições aeroacústicas; Ruído de eslate; Slat noise

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Pagani Júnior, C. d. C. (2014). Mapeamento de fontes aeroacústicas de um eslate em túnel de vento de seção fechada utilizando beam-forming com deconvolução DAMAS. (Doctoral Dissertation). University of São Paulo. Retrieved from http://www.teses.usp.br/teses/disponiveis/18/18148/tde-06122014-232641/ ;

Chicago Manual of Style (16th Edition):

Pagani Júnior, Carlos do Carmo. “Mapeamento de fontes aeroacústicas de um eslate em túnel de vento de seção fechada utilizando beam-forming com deconvolução DAMAS.” 2014. Doctoral Dissertation, University of São Paulo. Accessed July 05, 2020. http://www.teses.usp.br/teses/disponiveis/18/18148/tde-06122014-232641/ ;.

MLA Handbook (7th Edition):

Pagani Júnior, Carlos do Carmo. “Mapeamento de fontes aeroacústicas de um eslate em túnel de vento de seção fechada utilizando beam-forming com deconvolução DAMAS.” 2014. Web. 05 Jul 2020.

Vancouver:

Pagani Júnior CdC. Mapeamento de fontes aeroacústicas de um eslate em túnel de vento de seção fechada utilizando beam-forming com deconvolução DAMAS. [Internet] [Doctoral dissertation]. University of São Paulo; 2014. [cited 2020 Jul 05]. Available from: http://www.teses.usp.br/teses/disponiveis/18/18148/tde-06122014-232641/ ;.

Council of Science Editors:

Pagani Júnior CdC. Mapeamento de fontes aeroacústicas de um eslate em túnel de vento de seção fechada utilizando beam-forming com deconvolução DAMAS. [Doctoral Dissertation]. University of São Paulo; 2014. Available from: http://www.teses.usp.br/teses/disponiveis/18/18148/tde-06122014-232641/ ;

16. He, Zhengkai. Study on the Vortex Wake of an Airfoil Equipped with Flexible Trailing Edge Fringes.

Degree: MSEgr, Mechanical Engineering, 2014, Wright State University

 With the inspiration of owl’s silent flight, a traditional airfoil S833 equipped with flexible fringes on the trailing edge is investigated through numerical simulation and… (more)

Subjects/Keywords: Mechanical Engineering; Airfoil S833; Trailing Edge Fringe; Noise Reduction

…can help to improve the flow condition 3 around the airfoil and also reduce the noise… …Flow induced noise is one of the major contributors in the noise generation of various… …industrial applications. For instance trailing edge noise is an important component of aircraft… …airframe noise, in particular during landing and approach. Moreover trailing edge noise is also a… …noise generation mechanism for wind turbine rotor blades and helicopter blades. Due to… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

He, Z. (2014). Study on the Vortex Wake of an Airfoil Equipped with Flexible Trailing Edge Fringes. (Masters Thesis). Wright State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=wright1401738102

Chicago Manual of Style (16th Edition):

He, Zhengkai. “Study on the Vortex Wake of an Airfoil Equipped with Flexible Trailing Edge Fringes.” 2014. Masters Thesis, Wright State University. Accessed July 05, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=wright1401738102.

MLA Handbook (7th Edition):

He, Zhengkai. “Study on the Vortex Wake of an Airfoil Equipped with Flexible Trailing Edge Fringes.” 2014. Web. 05 Jul 2020.

Vancouver:

He Z. Study on the Vortex Wake of an Airfoil Equipped with Flexible Trailing Edge Fringes. [Internet] [Masters thesis]. Wright State University; 2014. [cited 2020 Jul 05]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=wright1401738102.

Council of Science Editors:

He Z. Study on the Vortex Wake of an Airfoil Equipped with Flexible Trailing Edge Fringes. [Masters Thesis]. Wright State University; 2014. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=wright1401738102

17. Li, Chi Shing. Computational Acoustic Beamforming of Noise Source on Wind Turbine Airfoil.

Degree: 2014, University of Waterloo

 A new method, Computational Acoustic Beamforming, is proposed in this thesis. This novel numerical sound source localization methodology combines the advantages of the Computational Fluid… (more)

Subjects/Keywords: Computational Acoustic Beamforming; Aeroacoustics; Noise; Source Localization; Airfoil

…turbulence noise and airfoil self-noise [6]. Low frequency noise lies in the frequency… …produced noise due to changes in the inflow turbulence. The last group of noise, airfoil self… …16 Figure 4.1: NAH measurement setup for engine noise source localization… …30 Figure 4.2: Beamforming measurement of wind turbine noise… …46 Figure 5.5: Geometry of the Airfoil… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Li, C. S. (2014). Computational Acoustic Beamforming of Noise Source on Wind Turbine Airfoil. (Thesis). University of Waterloo. Retrieved from http://hdl.handle.net/10012/8425

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

Chicago Manual of Style (16th Edition):

Li, Chi Shing. “Computational Acoustic Beamforming of Noise Source on Wind Turbine Airfoil.” 2014. Thesis, University of Waterloo. Accessed July 05, 2020. http://hdl.handle.net/10012/8425.

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

MLA Handbook (7th Edition):

Li, Chi Shing. “Computational Acoustic Beamforming of Noise Source on Wind Turbine Airfoil.” 2014. Web. 05 Jul 2020.

Vancouver:

Li CS. Computational Acoustic Beamforming of Noise Source on Wind Turbine Airfoil. [Internet] [Thesis]. University of Waterloo; 2014. [cited 2020 Jul 05]. Available from: http://hdl.handle.net/10012/8425.

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

Council of Science Editors:

Li CS. Computational Acoustic Beamforming of Noise Source on Wind Turbine Airfoil. [Thesis]. University of Waterloo; 2014. Available from: http://hdl.handle.net/10012/8425

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

18. Yakhina, Gyuzel. Experimental study of the tonal trailing-edge noise generated by low-reynolds number airfoils and comparison with numerical simulations : Étude expérimentale du sifflement de bord de fuite pour des profils à faible nombre de Reynolds et comparaison avec des simulations numériques.

Degree: Docteur es, Acoustique, 2017, Lyon

 Le bruit tonal rayonné au bord de fuite des profils à faible nombre de Reynolds est un phénomène observé sur les ailes de drones ou… (more)

Subjects/Keywords: Aéroacoustique; Profils d'aile; Bruit tonal de bord de fuite; Mesures en soufflerie; Ondes de Tollmien-Schlichting; Ondes de Kelvin-Helmholtz; Aeroacoustics; Airfoil; Trailing-edge tonal noise; Wind-tunnel measurements; Tollmien-Schlichting waves; Kelvin-Helmholtz waves

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Yakhina, G. (2017). Experimental study of the tonal trailing-edge noise generated by low-reynolds number airfoils and comparison with numerical simulations : Étude expérimentale du sifflement de bord de fuite pour des profils à faible nombre de Reynolds et comparaison avec des simulations numériques. (Doctoral Dissertation). Lyon. Retrieved from http://www.theses.fr/2017LYSEC008

Chicago Manual of Style (16th Edition):

Yakhina, Gyuzel. “Experimental study of the tonal trailing-edge noise generated by low-reynolds number airfoils and comparison with numerical simulations : Étude expérimentale du sifflement de bord de fuite pour des profils à faible nombre de Reynolds et comparaison avec des simulations numériques.” 2017. Doctoral Dissertation, Lyon. Accessed July 05, 2020. http://www.theses.fr/2017LYSEC008.

MLA Handbook (7th Edition):

Yakhina, Gyuzel. “Experimental study of the tonal trailing-edge noise generated by low-reynolds number airfoils and comparison with numerical simulations : Étude expérimentale du sifflement de bord de fuite pour des profils à faible nombre de Reynolds et comparaison avec des simulations numériques.” 2017. Web. 05 Jul 2020.

Vancouver:

Yakhina G. Experimental study of the tonal trailing-edge noise generated by low-reynolds number airfoils and comparison with numerical simulations : Étude expérimentale du sifflement de bord de fuite pour des profils à faible nombre de Reynolds et comparaison avec des simulations numériques. [Internet] [Doctoral dissertation]. Lyon; 2017. [cited 2020 Jul 05]. Available from: http://www.theses.fr/2017LYSEC008.

Council of Science Editors:

Yakhina G. Experimental study of the tonal trailing-edge noise generated by low-reynolds number airfoils and comparison with numerical simulations : Étude expérimentale du sifflement de bord de fuite pour des profils à faible nombre de Reynolds et comparaison avec des simulations numériques. [Doctoral Dissertation]. Lyon; 2017. Available from: http://www.theses.fr/2017LYSEC008


Brno University of Technology

19. Dofek, Ivan. Parametrická tvarová optimalizace letounu z aerodynamického hlediska: Aerodynamics Parametric Shape Aircraft Optimization.

Degree: 2019, Brno University of Technology

 The work deals with the use of geometric parameterization for shape description of some parts of the airplane. Geometric parametrization is used for creating a… (more)

Subjects/Keywords: parametrizace; evoluční algoritmus; geometrická parametrizace; optimalizace; hluk vrtule; letecký profil; Ffowcs Williams–Hawkings; polynomická paremtetrizace; řízená distribuce paremetrů; aerodynamická optimalizace vrtule; evolutionary algorithm; parametrization; geometric parametrization; optimization; propeller noise; airfoil; Ffowcs Williams–Hawkings; direct parameters distribution; propeller aerodynamics optimization

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Dofek, I. (2019). Parametrická tvarová optimalizace letounu z aerodynamického hlediska: Aerodynamics Parametric Shape Aircraft Optimization. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/36292

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):

Dofek, Ivan. “Parametrická tvarová optimalizace letounu z aerodynamického hlediska: Aerodynamics Parametric Shape Aircraft Optimization.” 2019. Thesis, Brno University of Technology. Accessed July 05, 2020. http://hdl.handle.net/11012/36292.

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

MLA Handbook (7th Edition):

Dofek, Ivan. “Parametrická tvarová optimalizace letounu z aerodynamického hlediska: Aerodynamics Parametric Shape Aircraft Optimization.” 2019. Web. 05 Jul 2020.

Vancouver:

Dofek I. Parametrická tvarová optimalizace letounu z aerodynamického hlediska: Aerodynamics Parametric Shape Aircraft Optimization. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2020 Jul 05]. Available from: http://hdl.handle.net/11012/36292.

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

Council of Science Editors:

Dofek I. Parametrická tvarová optimalizace letounu z aerodynamického hlediska: Aerodynamics Parametric Shape Aircraft Optimization. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/36292

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

20. Rao, Arjun. Measurement of aerodynamic characteristics of MAVs using motion tracking.

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

 Aerodynamic characteristics of Micro Air Vehicles (MAVs) is not well addressed in aeronautics literature, and more experimental data are required to help better understand the… (more)

Subjects/Keywords: Micro air vehicle (MAV); Reynolds number; remote controlled (RC); aircraft; airplane; model; Lift; drag; thrust; moment; stability; control; pitch; roll; yaw; weathercock; weathervane; motion tracking; motion capture; VICON; camera; wand; Re; lift curve; drag polar; propeller; Advanced Precision Composites (APC); sport; E-flite; sideslip; static margin (SM); axis; axes; PropellerScanner; airfoil; wing; lifting line theory; theory; experimental; Aerodynamics; calibration; noise; markers; camera; Euler angles; longitudinal; lateral; advance ratio; density; data points; Extra 260; Extra 300 3D; glider; frequency; revolutions per minute (RPM); body-fixed; Earth-fixed; transformation; rotation; matrix; filter; low-pass; finite difference; robust; lineqar; least-squares; parabolic; Uhlig; Selig; Rao

…acquisition capability, low radar cross section, and low noise. The primary missions of interest for… …that the span efficiency factors for an airfoil and wing at low Reynolds numbers deviated… …an airfoil. Experiments were conducted using an E387 airfoil and a wing with an aspect… …order to validate the motion tracking system. The noise levels and accuracy of the… …measurement rate to 50 or 100 Hz decreased the noise in the differentiated data. While tracking the… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Rao, A. (2012). Measurement of aerodynamic characteristics of MAVs using motion tracking. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/30943

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):

Rao, Arjun. “Measurement of aerodynamic characteristics of MAVs using motion tracking.” 2012. Thesis, University of Illinois – Urbana-Champaign. Accessed July 05, 2020. http://hdl.handle.net/2142/30943.

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

MLA Handbook (7th Edition):

Rao, Arjun. “Measurement of aerodynamic characteristics of MAVs using motion tracking.” 2012. Web. 05 Jul 2020.

Vancouver:

Rao A. Measurement of aerodynamic characteristics of MAVs using motion tracking. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2012. [cited 2020 Jul 05]. Available from: http://hdl.handle.net/2142/30943.

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

Council of Science Editors:

Rao A. Measurement of aerodynamic characteristics of MAVs using motion tracking. [Thesis]. University of Illinois – Urbana-Champaign; 2012. Available from: http://hdl.handle.net/2142/30943

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

.