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You searched for subject:(Vibration Aerodynamics ). Showing records 1 – 30 of 44 total matches.

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Florida Atlantic University

1. Mohan, Ranjith. Helicopter stability during aggressive maneuvers.

Degree: PhD, 2012, Florida Atlantic University

Summary: The dissertation investigates helicopter trim and stability during level bank-angle and diving bank-angle turns. The level turn is moderate in that sufficient power is… (more)

Subjects/Keywords: Helicopters – Aerodynamics; Helicopters – Control systems; Rotors (Helicopters) – Aerodynamics; Stability of helicopters; Vibration (Aeronautics) – Damping

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APA (6th Edition):

Mohan, R. (2012). Helicopter stability during aggressive maneuvers. (Doctoral Dissertation). Florida Atlantic University. Retrieved from http://purl.flvc.org/FAU/3342237

Chicago Manual of Style (16th Edition):

Mohan, Ranjith. “Helicopter stability during aggressive maneuvers.” 2012. Doctoral Dissertation, Florida Atlantic University. Accessed July 09, 2020. http://purl.flvc.org/FAU/3342237.

MLA Handbook (7th Edition):

Mohan, Ranjith. “Helicopter stability during aggressive maneuvers.” 2012. Web. 09 Jul 2020.

Vancouver:

Mohan R. Helicopter stability during aggressive maneuvers. [Internet] [Doctoral dissertation]. Florida Atlantic University; 2012. [cited 2020 Jul 09]. Available from: http://purl.flvc.org/FAU/3342237.

Council of Science Editors:

Mohan R. Helicopter stability during aggressive maneuvers. [Doctoral Dissertation]. Florida Atlantic University; 2012. Available from: http://purl.flvc.org/FAU/3342237


McGill University

2. Mark, Bill. An experimental study of the vibration response of a single flexibly-mounted cylinder within a rigid array subjected to air cross flow.

Degree: M. Eng., Department of Mechanical Engineering., 1986, McGill University

Subjects/Keywords: Tubes  – Vibration; Cylinders  – Vibration; Vibration  – Research; Tubes  – Aerodynamics

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APA (6th Edition):

Mark, B. (1986). An experimental study of the vibration response of a single flexibly-mounted cylinder within a rigid array subjected to air cross flow. (Masters Thesis). McGill University. Retrieved from http://digitool.library.mcgill.ca/thesisfile65431.pdf

Chicago Manual of Style (16th Edition):

Mark, Bill. “An experimental study of the vibration response of a single flexibly-mounted cylinder within a rigid array subjected to air cross flow.” 1986. Masters Thesis, McGill University. Accessed July 09, 2020. http://digitool.library.mcgill.ca/thesisfile65431.pdf.

MLA Handbook (7th Edition):

Mark, Bill. “An experimental study of the vibration response of a single flexibly-mounted cylinder within a rigid array subjected to air cross flow.” 1986. Web. 09 Jul 2020.

Vancouver:

Mark B. An experimental study of the vibration response of a single flexibly-mounted cylinder within a rigid array subjected to air cross flow. [Internet] [Masters thesis]. McGill University; 1986. [cited 2020 Jul 09]. Available from: http://digitool.library.mcgill.ca/thesisfile65431.pdf.

Council of Science Editors:

Mark B. An experimental study of the vibration response of a single flexibly-mounted cylinder within a rigid array subjected to air cross flow. [Masters Thesis]. McGill University; 1986. Available from: http://digitool.library.mcgill.ca/thesisfile65431.pdf


McGill University

3. Denise, Jean-Paul François. Flutter of cylindrical shells conveying fluid.

Degree: M. Eng., Department of Mechanical Engineering, 1971, McGill University

Subjects/Keywords: Shells (Engineering); Vibration.; Flutter (Aerodynamics)

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APA (6th Edition):

Denise, J. F. (1971). Flutter of cylindrical shells conveying fluid. (Masters Thesis). McGill University. Retrieved from http://digitool.library.mcgill.ca/thesisfile50212.pdf

Chicago Manual of Style (16th Edition):

Denise, Jean-Paul François. “Flutter of cylindrical shells conveying fluid.” 1971. Masters Thesis, McGill University. Accessed July 09, 2020. http://digitool.library.mcgill.ca/thesisfile50212.pdf.

MLA Handbook (7th Edition):

Denise, Jean-Paul François. “Flutter of cylindrical shells conveying fluid.” 1971. Web. 09 Jul 2020.

Vancouver:

Denise JF. Flutter of cylindrical shells conveying fluid. [Internet] [Masters thesis]. McGill University; 1971. [cited 2020 Jul 09]. Available from: http://digitool.library.mcgill.ca/thesisfile50212.pdf.

Council of Science Editors:

Denise JF. Flutter of cylindrical shells conveying fluid. [Masters Thesis]. McGill University; 1971. Available from: http://digitool.library.mcgill.ca/thesisfile50212.pdf


McGill University

4. Suen, Hon-ching. Ovalling vibration of cylindrical shells in cross flow.

Degree: Masters of Engineering., Department of Mechanical Engineering., 1980, McGill University

Note:

This thesis deals with flow-induced ovalling oscillation and the mechanical characteristics of cylindrical shells. The experiments were conducted with epoxy shells which were either… (more)

Subjects/Keywords: Cylinders  – Aerodynamics.; Cylinders  – Vibration.

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APA (6th Edition):

Suen, H. (1980). Ovalling vibration of cylindrical shells in cross flow. (Masters Thesis). McGill University. Retrieved from http://digitool.library.mcgill.ca/thesisfile119287.pdf

Chicago Manual of Style (16th Edition):

Suen, Hon-ching. “Ovalling vibration of cylindrical shells in cross flow.” 1980. Masters Thesis, McGill University. Accessed July 09, 2020. http://digitool.library.mcgill.ca/thesisfile119287.pdf.

MLA Handbook (7th Edition):

Suen, Hon-ching. “Ovalling vibration of cylindrical shells in cross flow.” 1980. Web. 09 Jul 2020.

Vancouver:

Suen H. Ovalling vibration of cylindrical shells in cross flow. [Internet] [Masters thesis]. McGill University; 1980. [cited 2020 Jul 09]. Available from: http://digitool.library.mcgill.ca/thesisfile119287.pdf.

Council of Science Editors:

Suen H. Ovalling vibration of cylindrical shells in cross flow. [Masters Thesis]. McGill University; 1980. Available from: http://digitool.library.mcgill.ca/thesisfile119287.pdf


Hong Kong University of Science and Technology

5. Song, Jie. Structural and aerodynamic couplings of wind-excited linked tall buildings.

Degree: 2015, Hong Kong University of Science and Technology

 There is a growing trend to link tall buildings in close proximity by connecting through horizontal structural links such as skybridges, skygardens, and even skypools.… (more)

Subjects/Keywords: Tall buildings ; Aerodynamics ; Testing ; Mathematical models ; Vibration ; Wind tunnels

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APA (6th Edition):

Song, J. (2015). Structural and aerodynamic couplings of wind-excited linked tall buildings. (Thesis). Hong Kong University of Science and Technology. Retrieved from http://repository.ust.hk/ir/Record/1783.1-78866 ; https://doi.org/10.14711/thesis-b1514636 ; http://repository.ust.hk/ir/bitstream/1783.1-78866/1/th_redirect.html

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):

Song, Jie. “Structural and aerodynamic couplings of wind-excited linked tall buildings.” 2015. Thesis, Hong Kong University of Science and Technology. Accessed July 09, 2020. http://repository.ust.hk/ir/Record/1783.1-78866 ; https://doi.org/10.14711/thesis-b1514636 ; http://repository.ust.hk/ir/bitstream/1783.1-78866/1/th_redirect.html.

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

MLA Handbook (7th Edition):

Song, Jie. “Structural and aerodynamic couplings of wind-excited linked tall buildings.” 2015. Web. 09 Jul 2020.

Vancouver:

Song J. Structural and aerodynamic couplings of wind-excited linked tall buildings. [Internet] [Thesis]. Hong Kong University of Science and Technology; 2015. [cited 2020 Jul 09]. Available from: http://repository.ust.hk/ir/Record/1783.1-78866 ; https://doi.org/10.14711/thesis-b1514636 ; http://repository.ust.hk/ir/bitstream/1783.1-78866/1/th_redirect.html.

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

Council of Science Editors:

Song J. Structural and aerodynamic couplings of wind-excited linked tall buildings. [Thesis]. Hong Kong University of Science and Technology; 2015. Available from: http://repository.ust.hk/ir/Record/1783.1-78866 ; https://doi.org/10.14711/thesis-b1514636 ; http://repository.ust.hk/ir/bitstream/1783.1-78866/1/th_redirect.html

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


Georgia Tech

6. Bartlett, Felton Drew. The development of a controlled lateral gust facility for determining the transfer function of a lifting surface.

Degree: PhD, Aeronautical Engineering, 1972, Georgia Tech

Subjects/Keywords: Aeroelasticity; Vibration (Aeronautics); Lift (Aerodynamics)

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APA (6th Edition):

Bartlett, F. D. (1972). The development of a controlled lateral gust facility for determining the transfer function of a lifting surface. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/12533

Chicago Manual of Style (16th Edition):

Bartlett, Felton Drew. “The development of a controlled lateral gust facility for determining the transfer function of a lifting surface.” 1972. Doctoral Dissertation, Georgia Tech. Accessed July 09, 2020. http://hdl.handle.net/1853/12533.

MLA Handbook (7th Edition):

Bartlett, Felton Drew. “The development of a controlled lateral gust facility for determining the transfer function of a lifting surface.” 1972. Web. 09 Jul 2020.

Vancouver:

Bartlett FD. The development of a controlled lateral gust facility for determining the transfer function of a lifting surface. [Internet] [Doctoral dissertation]. Georgia Tech; 1972. [cited 2020 Jul 09]. Available from: http://hdl.handle.net/1853/12533.

Council of Science Editors:

Bartlett FD. The development of a controlled lateral gust facility for determining the transfer function of a lifting surface. [Doctoral Dissertation]. Georgia Tech; 1972. Available from: http://hdl.handle.net/1853/12533


Georgia Tech

7. Griffin, Steven F. Acoustic replication in smart structure using active structural/acoustic control.

Degree: PhD, Aeronautical Engineering, 1995, Georgia Tech

Subjects/Keywords: Noise control; Vibration; Aerodynamics

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APA (6th Edition):

Griffin, S. F. (1995). Acoustic replication in smart structure using active structural/acoustic control. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/13085

Chicago Manual of Style (16th Edition):

Griffin, Steven F. “Acoustic replication in smart structure using active structural/acoustic control.” 1995. Doctoral Dissertation, Georgia Tech. Accessed July 09, 2020. http://hdl.handle.net/1853/13085.

MLA Handbook (7th Edition):

Griffin, Steven F. “Acoustic replication in smart structure using active structural/acoustic control.” 1995. Web. 09 Jul 2020.

Vancouver:

Griffin SF. Acoustic replication in smart structure using active structural/acoustic control. [Internet] [Doctoral dissertation]. Georgia Tech; 1995. [cited 2020 Jul 09]. Available from: http://hdl.handle.net/1853/13085.

Council of Science Editors:

Griffin SF. Acoustic replication in smart structure using active structural/acoustic control. [Doctoral Dissertation]. Georgia Tech; 1995. Available from: http://hdl.handle.net/1853/13085


University of KwaZulu-Natal

8. [No author]. Determination of dynamic loads caused by aeolian vibration on composite insulator : experimental approach.

Degree: Mechanical engineering, 2015, University of KwaZulu-Natal

 High voltage insulators have to fulfil high reliability criteria by being one of the main components for the operational safety and operating efficiency of the… (more)

Subjects/Keywords: Electric insulators and insulation – Vibration.; Flutter (Aerodynamics); Electric conductors.; Electric conductors – Vibration.; Overhead electric lines – Vibration.; Mechanical engineering.; Aeolian vibration.; Composite insulator.

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APA (6th Edition):

author], [. (2015). Determination of dynamic loads caused by aeolian vibration on composite insulator : experimental approach. (Thesis). University of KwaZulu-Natal. Retrieved from http://hdl.handle.net/10413/13276

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

Chicago Manual of Style (16th Edition):

author], [No. “Determination of dynamic loads caused by aeolian vibration on composite insulator : experimental approach. ” 2015. Thesis, University of KwaZulu-Natal. Accessed July 09, 2020. http://hdl.handle.net/10413/13276.

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

MLA Handbook (7th Edition):

author], [No. “Determination of dynamic loads caused by aeolian vibration on composite insulator : experimental approach. ” 2015. Web. 09 Jul 2020.

Vancouver:

author] [. Determination of dynamic loads caused by aeolian vibration on composite insulator : experimental approach. [Internet] [Thesis]. University of KwaZulu-Natal; 2015. [cited 2020 Jul 09]. Available from: http://hdl.handle.net/10413/13276.

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

Council of Science Editors:

author] [. Determination of dynamic loads caused by aeolian vibration on composite insulator : experimental approach. [Thesis]. University of KwaZulu-Natal; 2015. Available from: http://hdl.handle.net/10413/13276

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


Texas Tech University

9. Heo, Hun. Non-linear stochastic flutter of aeroelastic structural systems.

Degree: Mechanical Engineering, 1985, Texas Tech University

 The main objective of t h i s investigation is to examine the linear and non-linear modal interactions of a two-degree-of-freedom aero-elastic structure subjected to… (more)

Subjects/Keywords: Nonlinear theories; Aeroelasticity; Flutter (Aerodynamics); Aerodynamics; Vibration (Aeronautics)

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APA (6th Edition):

Heo, H. (1985). Non-linear stochastic flutter of aeroelastic structural systems. (Thesis). Texas Tech University. Retrieved from http://hdl.handle.net/2346/11127

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):

Heo, Hun. “Non-linear stochastic flutter of aeroelastic structural systems.” 1985. Thesis, Texas Tech University. Accessed July 09, 2020. http://hdl.handle.net/2346/11127.

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

MLA Handbook (7th Edition):

Heo, Hun. “Non-linear stochastic flutter of aeroelastic structural systems.” 1985. Web. 09 Jul 2020.

Vancouver:

Heo H. Non-linear stochastic flutter of aeroelastic structural systems. [Internet] [Thesis]. Texas Tech University; 1985. [cited 2020 Jul 09]. Available from: http://hdl.handle.net/2346/11127.

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

Council of Science Editors:

Heo H. Non-linear stochastic flutter of aeroelastic structural systems. [Thesis]. Texas Tech University; 1985. Available from: http://hdl.handle.net/2346/11127

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


Georgia Tech

10. Viswanathan, Sathy Padmanaban. An analysis of the flutter and damping characteristics of helicopter rotors.

Degree: PhD, Aeronautical Engineering, 1977, Georgia Tech

Subjects/Keywords: Rotors (Helicopters) Aerodynamics; Flutter (Aerodynamics); Vibration (Aeronautics) Damping

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APA (6th Edition):

Viswanathan, S. P. (1977). An analysis of the flutter and damping characteristics of helicopter rotors. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/12441

Chicago Manual of Style (16th Edition):

Viswanathan, Sathy Padmanaban. “An analysis of the flutter and damping characteristics of helicopter rotors.” 1977. Doctoral Dissertation, Georgia Tech. Accessed July 09, 2020. http://hdl.handle.net/1853/12441.

MLA Handbook (7th Edition):

Viswanathan, Sathy Padmanaban. “An analysis of the flutter and damping characteristics of helicopter rotors.” 1977. Web. 09 Jul 2020.

Vancouver:

Viswanathan SP. An analysis of the flutter and damping characteristics of helicopter rotors. [Internet] [Doctoral dissertation]. Georgia Tech; 1977. [cited 2020 Jul 09]. Available from: http://hdl.handle.net/1853/12441.

Council of Science Editors:

Viswanathan SP. An analysis of the flutter and damping characteristics of helicopter rotors. [Doctoral Dissertation]. Georgia Tech; 1977. Available from: http://hdl.handle.net/1853/12441


Indian Institute of Science

11. Narla, Subrahmanya Prasad. Vibration And Impact Induced Sound.

Degree: 2009, Indian Institute of Science

 Sound generated by impacting structures is of considerable importance in noise control. Sound is generated by a vibrating structure by inducing pressure fluctuations in the… (more)

Subjects/Keywords: Vibration; Sound Vibrations; Oscillators - Vibration Analysis; Acoustic Field Dynamics; Impact Mechanics; Impact Oscillator; Impact Induced Sound; Aerodynamics

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APA (6th Edition):

Narla, S. P. (2009). Vibration And Impact Induced Sound. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/928

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):

Narla, Subrahmanya Prasad. “Vibration And Impact Induced Sound.” 2009. Thesis, Indian Institute of Science. Accessed July 09, 2020. http://hdl.handle.net/2005/928.

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

MLA Handbook (7th Edition):

Narla, Subrahmanya Prasad. “Vibration And Impact Induced Sound.” 2009. Web. 09 Jul 2020.

Vancouver:

Narla SP. Vibration And Impact Induced Sound. [Internet] [Thesis]. Indian Institute of Science; 2009. [cited 2020 Jul 09]. Available from: http://hdl.handle.net/2005/928.

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

Council of Science Editors:

Narla SP. Vibration And Impact Induced Sound. [Thesis]. Indian Institute of Science; 2009. Available from: http://hdl.handle.net/2005/928

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


Virginia Tech

12. Yan, Zhimiao. Modeling of Nonlinear Unsteady Aerodynamics, Dynamics and Fluid Structure Interactions.

Degree: PhD, Engineering Science and Mechanics, 2015, Virginia Tech

 We model different nonlinear systems, analyze their nonlinear aspects and discuss their applications. First, we present a semi-analytical, geometrically-exact, unsteady potential flow model is developed… (more)

Subjects/Keywords: Nonlinear Dynamics; Unsteady Aerodynamics; Vibration; Energy Harvesting; Galloping; Autoparametric Vibration Absorber; Method of Multiple Scale; Bifurcation; Saturation; Quenching; Chaos

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APA (6th Edition):

Yan, Z. (2015). Modeling of Nonlinear Unsteady Aerodynamics, Dynamics and Fluid Structure Interactions. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/71824

Chicago Manual of Style (16th Edition):

Yan, Zhimiao. “Modeling of Nonlinear Unsteady Aerodynamics, Dynamics and Fluid Structure Interactions.” 2015. Doctoral Dissertation, Virginia Tech. Accessed July 09, 2020. http://hdl.handle.net/10919/71824.

MLA Handbook (7th Edition):

Yan, Zhimiao. “Modeling of Nonlinear Unsteady Aerodynamics, Dynamics and Fluid Structure Interactions.” 2015. Web. 09 Jul 2020.

Vancouver:

Yan Z. Modeling of Nonlinear Unsteady Aerodynamics, Dynamics and Fluid Structure Interactions. [Internet] [Doctoral dissertation]. Virginia Tech; 2015. [cited 2020 Jul 09]. Available from: http://hdl.handle.net/10919/71824.

Council of Science Editors:

Yan Z. Modeling of Nonlinear Unsteady Aerodynamics, Dynamics and Fluid Structure Interactions. [Doctoral Dissertation]. Virginia Tech; 2015. Available from: http://hdl.handle.net/10919/71824


Florida Atlantic University

13. Calle, Oscar F. Rain-wind-induced cable vibrations in cable-stayed bridges.

Degree: MS, 2014, Florida Atlantic University

Summary: This research is aimed at investigating and analyzing the rain-windinduced cable vibration phenomena experienced in cables of cable-stayed bridges and also the countermeasures employed… (more)

Subjects/Keywords: Bridges  – Aerodynamics; Bridges  – Vibration  – Prevention; Cable stayed bridges  – Maintenance and repair; Damping (Mechanics); Structural dynamics; Vibration  – Mathematical models; Wind resistant design

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APA (6th Edition):

Calle, O. F. (2014). Rain-wind-induced cable vibrations in cable-stayed bridges. (Masters Thesis). Florida Atlantic University. Retrieved from http://purl.flvc.org/fau/fd/FA00004271 ; (URL) http://purl.flvc.org/fau/fd/FA00004271

Chicago Manual of Style (16th Edition):

Calle, Oscar F. “Rain-wind-induced cable vibrations in cable-stayed bridges.” 2014. Masters Thesis, Florida Atlantic University. Accessed July 09, 2020. http://purl.flvc.org/fau/fd/FA00004271 ; (URL) http://purl.flvc.org/fau/fd/FA00004271.

MLA Handbook (7th Edition):

Calle, Oscar F. “Rain-wind-induced cable vibrations in cable-stayed bridges.” 2014. Web. 09 Jul 2020.

Vancouver:

Calle OF. Rain-wind-induced cable vibrations in cable-stayed bridges. [Internet] [Masters thesis]. Florida Atlantic University; 2014. [cited 2020 Jul 09]. Available from: http://purl.flvc.org/fau/fd/FA00004271 ; (URL) http://purl.flvc.org/fau/fd/FA00004271.

Council of Science Editors:

Calle OF. Rain-wind-induced cable vibrations in cable-stayed bridges. [Masters Thesis]. Florida Atlantic University; 2014. Available from: http://purl.flvc.org/fau/fd/FA00004271 ; (URL) http://purl.flvc.org/fau/fd/FA00004271


Delft University of Technology

14. Derksen, Adriaan (author). Numerical simulation of a forced and freely-vibrating cylinder at supercritical Reynolds numbers.

Degree: 2019, Delft University of Technology

Recent innovations in the off-shore wind industry have lead to bigger wind turbines and taller support structures. These towers can suffer from vortex-induced vibrations (VIV).… (more)

Subjects/Keywords: Vortex-induced vibrations; supercritical Reynolds number; Forced-vibration; Frree-vibration; numerical simulation; OpenFOAM; URANS; fluid-structure interaction; Cylinder aerodynamics

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APA (6th Edition):

Derksen, A. (. (2019). Numerical simulation of a forced and freely-vibrating cylinder at supercritical Reynolds numbers. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:4c92eee4-8378-4a40-9180-bcb72f751076

Chicago Manual of Style (16th Edition):

Derksen, Adriaan (author). “Numerical simulation of a forced and freely-vibrating cylinder at supercritical Reynolds numbers.” 2019. Masters Thesis, Delft University of Technology. Accessed July 09, 2020. http://resolver.tudelft.nl/uuid:4c92eee4-8378-4a40-9180-bcb72f751076.

MLA Handbook (7th Edition):

Derksen, Adriaan (author). “Numerical simulation of a forced and freely-vibrating cylinder at supercritical Reynolds numbers.” 2019. Web. 09 Jul 2020.

Vancouver:

Derksen A(. Numerical simulation of a forced and freely-vibrating cylinder at supercritical Reynolds numbers. [Internet] [Masters thesis]. Delft University of Technology; 2019. [cited 2020 Jul 09]. Available from: http://resolver.tudelft.nl/uuid:4c92eee4-8378-4a40-9180-bcb72f751076.

Council of Science Editors:

Derksen A(. Numerical simulation of a forced and freely-vibrating cylinder at supercritical Reynolds numbers. [Masters Thesis]. Delft University of Technology; 2019. Available from: http://resolver.tudelft.nl/uuid:4c92eee4-8378-4a40-9180-bcb72f751076


McMaster University

15. McLaren, Kevin W. A NUMERICAL AND EXPERIMENTAL STUDY OF UNSTEADY LOADING OF HIGH SOLIDITY VERTICAL AXIS WIND TURBINES.

Degree: PhD, 2011, McMaster University

This thesis reports on a numerical and experimental investigation of the unsteady loading of high solidity vertical axis wind turbines (VAWTs). Two-dimensional, unsteady Reynolds… (more)

Subjects/Keywords: Vertical Axis Wind Turbine; Dynamic Stall; Vibration Response; Three-dimensional Flow Effects; URANS Simulation; Vibration Mitigation Methodologies; Aerodynamics and Fluid Mechanics; Aerodynamics and Fluid Mechanics

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APA (6th Edition):

McLaren, K. W. (2011). A NUMERICAL AND EXPERIMENTAL STUDY OF UNSTEADY LOADING OF HIGH SOLIDITY VERTICAL AXIS WIND TURBINES. (Doctoral Dissertation). McMaster University. Retrieved from http://hdl.handle.net/11375/11096

Chicago Manual of Style (16th Edition):

McLaren, Kevin W. “A NUMERICAL AND EXPERIMENTAL STUDY OF UNSTEADY LOADING OF HIGH SOLIDITY VERTICAL AXIS WIND TURBINES.” 2011. Doctoral Dissertation, McMaster University. Accessed July 09, 2020. http://hdl.handle.net/11375/11096.

MLA Handbook (7th Edition):

McLaren, Kevin W. “A NUMERICAL AND EXPERIMENTAL STUDY OF UNSTEADY LOADING OF HIGH SOLIDITY VERTICAL AXIS WIND TURBINES.” 2011. Web. 09 Jul 2020.

Vancouver:

McLaren KW. A NUMERICAL AND EXPERIMENTAL STUDY OF UNSTEADY LOADING OF HIGH SOLIDITY VERTICAL AXIS WIND TURBINES. [Internet] [Doctoral dissertation]. McMaster University; 2011. [cited 2020 Jul 09]. Available from: http://hdl.handle.net/11375/11096.

Council of Science Editors:

McLaren KW. A NUMERICAL AND EXPERIMENTAL STUDY OF UNSTEADY LOADING OF HIGH SOLIDITY VERTICAL AXIS WIND TURBINES. [Doctoral Dissertation]. McMaster University; 2011. Available from: http://hdl.handle.net/11375/11096


University of Colorado

16. Kucala, Alec. Control of Transitional and Turbulent Flows Using Direct Numerical Simulation.

Degree: PhD, Aerospace Engineering Sciences, 2015, University of Colorado

  Efficient methods of drag reduction in wall-bounded shear flows remains an important, yet elusive problem in fluid mechanics. There are two potential avenues for… (more)

Subjects/Keywords: direct numerical simulation; flow control; phononics; transition; turbulence; vibration; Aerodynamics and Fluid Mechanics

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

APA (6th Edition):

Kucala, A. (2015). Control of Transitional and Turbulent Flows Using Direct Numerical Simulation. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/107

Chicago Manual of Style (16th Edition):

Kucala, Alec. “Control of Transitional and Turbulent Flows Using Direct Numerical Simulation.” 2015. Doctoral Dissertation, University of Colorado. Accessed July 09, 2020. https://scholar.colorado.edu/asen_gradetds/107.

MLA Handbook (7th Edition):

Kucala, Alec. “Control of Transitional and Turbulent Flows Using Direct Numerical Simulation.” 2015. Web. 09 Jul 2020.

Vancouver:

Kucala A. Control of Transitional and Turbulent Flows Using Direct Numerical Simulation. [Internet] [Doctoral dissertation]. University of Colorado; 2015. [cited 2020 Jul 09]. Available from: https://scholar.colorado.edu/asen_gradetds/107.

Council of Science Editors:

Kucala A. Control of Transitional and Turbulent Flows Using Direct Numerical Simulation. [Doctoral Dissertation]. University of Colorado; 2015. Available from: https://scholar.colorado.edu/asen_gradetds/107


Hong Kong University of Science and Technology

17. Tang, Un Fong. Interference effects of wind-excited tall buildings.

Degree: 2002, Hong Kong University of Science and Technology

 This thesis presents the results of a study of interference effects and excitation mechanisms on wind-excited tall buildings through wind tunnel model tests on a… (more)

Subjects/Keywords: Tall buildings  – Aerodynamics ; Tall buildings  – Vibration

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

APA (6th Edition):

Tang, U. F. (2002). Interference effects of wind-excited tall buildings. (Thesis). Hong Kong University of Science and Technology. Retrieved from http://repository.ust.hk/ir/Record/1783.1-4142 ; https://doi.org/10.14711/thesis-b779379 ; http://repository.ust.hk/ir/bitstream/1783.1-4142/1/th_redirect.html

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):

Tang, Un Fong. “Interference effects of wind-excited tall buildings.” 2002. Thesis, Hong Kong University of Science and Technology. Accessed July 09, 2020. http://repository.ust.hk/ir/Record/1783.1-4142 ; https://doi.org/10.14711/thesis-b779379 ; http://repository.ust.hk/ir/bitstream/1783.1-4142/1/th_redirect.html.

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

MLA Handbook (7th Edition):

Tang, Un Fong. “Interference effects of wind-excited tall buildings.” 2002. Web. 09 Jul 2020.

Vancouver:

Tang UF. Interference effects of wind-excited tall buildings. [Internet] [Thesis]. Hong Kong University of Science and Technology; 2002. [cited 2020 Jul 09]. Available from: http://repository.ust.hk/ir/Record/1783.1-4142 ; https://doi.org/10.14711/thesis-b779379 ; http://repository.ust.hk/ir/bitstream/1783.1-4142/1/th_redirect.html.

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

Council of Science Editors:

Tang UF. Interference effects of wind-excited tall buildings. [Thesis]. Hong Kong University of Science and Technology; 2002. Available from: http://repository.ust.hk/ir/Record/1783.1-4142 ; https://doi.org/10.14711/thesis-b779379 ; http://repository.ust.hk/ir/bitstream/1783.1-4142/1/th_redirect.html

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


Florida Atlantic University

18. Sargsyan, Armen. Simulation and modeling of flow field around a horizontal axis wind turbine (HAWT) using RANS method.

Degree: M.S.C.S., 2010, Florida Atlantic University

Summary: The principal objective of the proposed CFD analysis is to investigate the flow field around a horizontal axis wind turbine rotor and calculate the… (more)

Subjects/Keywords: Wind turbines – Aerodynamics – Computer simulation; Fluid dynamics – Computational methods; Vibration (Aerodynamics)

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

APA (6th Edition):

Sargsyan, A. (2010). Simulation and modeling of flow field around a horizontal axis wind turbine (HAWT) using RANS method. (Masters Thesis). Florida Atlantic University. Retrieved from http://purl.flvc.org/FAU/2979383

Chicago Manual of Style (16th Edition):

Sargsyan, Armen. “Simulation and modeling of flow field around a horizontal axis wind turbine (HAWT) using RANS method.” 2010. Masters Thesis, Florida Atlantic University. Accessed July 09, 2020. http://purl.flvc.org/FAU/2979383.

MLA Handbook (7th Edition):

Sargsyan, Armen. “Simulation and modeling of flow field around a horizontal axis wind turbine (HAWT) using RANS method.” 2010. Web. 09 Jul 2020.

Vancouver:

Sargsyan A. Simulation and modeling of flow field around a horizontal axis wind turbine (HAWT) using RANS method. [Internet] [Masters thesis]. Florida Atlantic University; 2010. [cited 2020 Jul 09]. Available from: http://purl.flvc.org/FAU/2979383.

Council of Science Editors:

Sargsyan A. Simulation and modeling of flow field around a horizontal axis wind turbine (HAWT) using RANS method. [Masters Thesis]. Florida Atlantic University; 2010. Available from: http://purl.flvc.org/FAU/2979383


University of Alabama

19. Zhang, Zheng. Static and dynamic characteristics of membrane wings at low Reynolds number.

Degree: 2014, University of Alabama

 To lessen the deterioration of fixed-wing aerodynamic performance associated with Reynolds numbers (Re) below 100,000, flexible membrane wing designs have been studied and proposed as… (more)

Subjects/Keywords: Electronic Thesis or Dissertation;  – thesis; Aerospace engineering; Mechanics; flow-induced vibration; fluid-structure interaction; low Re aerodynamics; MAV; wind tunnel testing

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APA (6th Edition):

Zhang, Z. (2014). Static and dynamic characteristics of membrane wings at low Reynolds number. (Thesis). University of Alabama. Retrieved from http://purl.lib.ua.edu/120446

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

Chicago Manual of Style (16th Edition):

Zhang, Zheng. “Static and dynamic characteristics of membrane wings at low Reynolds number.” 2014. Thesis, University of Alabama. Accessed July 09, 2020. http://purl.lib.ua.edu/120446.

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

MLA Handbook (7th Edition):

Zhang, Zheng. “Static and dynamic characteristics of membrane wings at low Reynolds number.” 2014. Web. 09 Jul 2020.

Vancouver:

Zhang Z. Static and dynamic characteristics of membrane wings at low Reynolds number. [Internet] [Thesis]. University of Alabama; 2014. [cited 2020 Jul 09]. Available from: http://purl.lib.ua.edu/120446.

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

Council of Science Editors:

Zhang Z. Static and dynamic characteristics of membrane wings at low Reynolds number. [Thesis]. University of Alabama; 2014. Available from: http://purl.lib.ua.edu/120446

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


Michigan Technological University

20. Sun, Xiao. SMART AERODYNAMIC CONTROL DEVICES DESIGN AND VIBRATION REDUCTION ANALYSIS FOR WIND TURBINE BLADES.

Degree: PhD, Department of Civil and Environmental Engineering, 2016, Michigan Technological University

  This study aims to design several types of aerodynamic control devices using smart material actuators to reduce the vibration fatigue load of wind turbine… (more)

Subjects/Keywords: Smart Material; Trailing Edge Flap; Wind Turbine; Vibration Fatigue; Modal Analysis; Acoustics, Dynamics, and Controls; Aerodynamics and Fluid Mechanics; Civil Engineering

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

APA (6th Edition):

Sun, X. (2016). SMART AERODYNAMIC CONTROL DEVICES DESIGN AND VIBRATION REDUCTION ANALYSIS FOR WIND TURBINE BLADES. (Doctoral Dissertation). Michigan Technological University. Retrieved from http://digitalcommons.mtu.edu/etdr/298

Chicago Manual of Style (16th Edition):

Sun, Xiao. “SMART AERODYNAMIC CONTROL DEVICES DESIGN AND VIBRATION REDUCTION ANALYSIS FOR WIND TURBINE BLADES.” 2016. Doctoral Dissertation, Michigan Technological University. Accessed July 09, 2020. http://digitalcommons.mtu.edu/etdr/298.

MLA Handbook (7th Edition):

Sun, Xiao. “SMART AERODYNAMIC CONTROL DEVICES DESIGN AND VIBRATION REDUCTION ANALYSIS FOR WIND TURBINE BLADES.” 2016. Web. 09 Jul 2020.

Vancouver:

Sun X. SMART AERODYNAMIC CONTROL DEVICES DESIGN AND VIBRATION REDUCTION ANALYSIS FOR WIND TURBINE BLADES. [Internet] [Doctoral dissertation]. Michigan Technological University; 2016. [cited 2020 Jul 09]. Available from: http://digitalcommons.mtu.edu/etdr/298.

Council of Science Editors:

Sun X. SMART AERODYNAMIC CONTROL DEVICES DESIGN AND VIBRATION REDUCTION ANALYSIS FOR WIND TURBINE BLADES. [Doctoral Dissertation]. Michigan Technological University; 2016. Available from: http://digitalcommons.mtu.edu/etdr/298


Virginia Tech

21. Chandiramani, Naresh K. Nonlinear flutter of composite shear-deformable panels in a high-supersonic flow.

Degree: PhD, Engineering Mechanics, 1993, Virginia Tech

Subjects/Keywords: Flutter (Aerodynamics); Plates (Engineering) Vibration.; LD5655.V856 1993.C538

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APA (6th Edition):

Chandiramani, N. K. (1993). Nonlinear flutter of composite shear-deformable panels in a high-supersonic flow. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/40149

Chicago Manual of Style (16th Edition):

Chandiramani, Naresh K. “Nonlinear flutter of composite shear-deformable panels in a high-supersonic flow.” 1993. Doctoral Dissertation, Virginia Tech. Accessed July 09, 2020. http://hdl.handle.net/10919/40149.

MLA Handbook (7th Edition):

Chandiramani, Naresh K. “Nonlinear flutter of composite shear-deformable panels in a high-supersonic flow.” 1993. Web. 09 Jul 2020.

Vancouver:

Chandiramani NK. Nonlinear flutter of composite shear-deformable panels in a high-supersonic flow. [Internet] [Doctoral dissertation]. Virginia Tech; 1993. [cited 2020 Jul 09]. Available from: http://hdl.handle.net/10919/40149.

Council of Science Editors:

Chandiramani NK. Nonlinear flutter of composite shear-deformable panels in a high-supersonic flow. [Doctoral Dissertation]. Virginia Tech; 1993. Available from: http://hdl.handle.net/10919/40149


University of Sydney

22. Xu, Y. L. (You Lin), 1952-. Vibration control of wind-excited tall/slender structures .

Degree: 1991, University of Sydney

Subjects/Keywords: Buildings  – Vibration; Damping (Mechanics); Tall buildings  – Aerodynamics; Wind-pressure

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APA (6th Edition):

Xu, Y. L. (You Lin), 1. (1991). Vibration control of wind-excited tall/slender structures . (Thesis). University of Sydney. Retrieved from http://hdl.handle.net/2123/9458

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):

Xu, Y. L. (You Lin), 1952-. “Vibration control of wind-excited tall/slender structures .” 1991. Thesis, University of Sydney. Accessed July 09, 2020. http://hdl.handle.net/2123/9458.

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

MLA Handbook (7th Edition):

Xu, Y. L. (You Lin), 1952-. “Vibration control of wind-excited tall/slender structures .” 1991. Web. 09 Jul 2020.

Vancouver:

Xu, Y. L. (You Lin) 1. Vibration control of wind-excited tall/slender structures . [Internet] [Thesis]. University of Sydney; 1991. [cited 2020 Jul 09]. Available from: http://hdl.handle.net/2123/9458.

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

Council of Science Editors:

Xu, Y. L. (You Lin) 1. Vibration control of wind-excited tall/slender structures . [Thesis]. University of Sydney; 1991. Available from: http://hdl.handle.net/2123/9458

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


Hong Kong University of Science and Technology

23. Hui, Kenny Tsz Kin. Stiffness optimization to limit wind-induced vibrations of tall buildings.

Degree: 2000, Hong Kong University of Science and Technology

 The trend towards constructing taller and slender buildings with higher strength materials has contributed to a new generation of wind sensitive structures. Modern tall buildings… (more)

Subjects/Keywords: Tall buildings  – Aerodynamics ; Damping (Mechanics) ; Vibration ; Dynamics, Rigid

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

APA (6th Edition):

Hui, K. T. K. (2000). Stiffness optimization to limit wind-induced vibrations of tall buildings. (Thesis). Hong Kong University of Science and Technology. Retrieved from http://repository.ust.hk/ir/Record/1783.1-4106 ; https://doi.org/10.14711/thesis-b681105 ; http://repository.ust.hk/ir/bitstream/1783.1-4106/1/th_redirect.html

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):

Hui, Kenny Tsz Kin. “Stiffness optimization to limit wind-induced vibrations of tall buildings.” 2000. Thesis, Hong Kong University of Science and Technology. Accessed July 09, 2020. http://repository.ust.hk/ir/Record/1783.1-4106 ; https://doi.org/10.14711/thesis-b681105 ; http://repository.ust.hk/ir/bitstream/1783.1-4106/1/th_redirect.html.

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

MLA Handbook (7th Edition):

Hui, Kenny Tsz Kin. “Stiffness optimization to limit wind-induced vibrations of tall buildings.” 2000. Web. 09 Jul 2020.

Vancouver:

Hui KTK. Stiffness optimization to limit wind-induced vibrations of tall buildings. [Internet] [Thesis]. Hong Kong University of Science and Technology; 2000. [cited 2020 Jul 09]. Available from: http://repository.ust.hk/ir/Record/1783.1-4106 ; https://doi.org/10.14711/thesis-b681105 ; http://repository.ust.hk/ir/bitstream/1783.1-4106/1/th_redirect.html.

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

Council of Science Editors:

Hui KTK. Stiffness optimization to limit wind-induced vibrations of tall buildings. [Thesis]. Hong Kong University of Science and Technology; 2000. Available from: http://repository.ust.hk/ir/Record/1783.1-4106 ; https://doi.org/10.14711/thesis-b681105 ; http://repository.ust.hk/ir/bitstream/1783.1-4106/1/th_redirect.html

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


Hong Kong University of Science and Technology

24. Wong, Kwok Shing. Wind-induced interference effects on eccentric tall buildings.

Degree: 2007, Hong Kong University of Science and Technology

 This thesis presents the results of a study of interference effects and excitation mechanisms on wind-excited centric and eccentric tall buildings through wind tunnel test… (more)

Subjects/Keywords: Tall buildings  – Aerodynamics ; Tall buildings  – Vibration ; Wind tunnels

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APA (6th Edition):

Wong, K. S. (2007). Wind-induced interference effects on eccentric tall buildings. (Thesis). Hong Kong University of Science and Technology. Retrieved from http://repository.ust.hk/ir/Record/1783.1-4214 ; https://doi.org/10.14711/thesis-b943689 ; http://repository.ust.hk/ir/bitstream/1783.1-4214/1/th_redirect.html

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):

Wong, Kwok Shing. “Wind-induced interference effects on eccentric tall buildings.” 2007. Thesis, Hong Kong University of Science and Technology. Accessed July 09, 2020. http://repository.ust.hk/ir/Record/1783.1-4214 ; https://doi.org/10.14711/thesis-b943689 ; http://repository.ust.hk/ir/bitstream/1783.1-4214/1/th_redirect.html.

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

MLA Handbook (7th Edition):

Wong, Kwok Shing. “Wind-induced interference effects on eccentric tall buildings.” 2007. Web. 09 Jul 2020.

Vancouver:

Wong KS. Wind-induced interference effects on eccentric tall buildings. [Internet] [Thesis]. Hong Kong University of Science and Technology; 2007. [cited 2020 Jul 09]. Available from: http://repository.ust.hk/ir/Record/1783.1-4214 ; https://doi.org/10.14711/thesis-b943689 ; http://repository.ust.hk/ir/bitstream/1783.1-4214/1/th_redirect.html.

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

Council of Science Editors:

Wong KS. Wind-induced interference effects on eccentric tall buildings. [Thesis]. Hong Kong University of Science and Technology; 2007. Available from: http://repository.ust.hk/ir/Record/1783.1-4214 ; https://doi.org/10.14711/thesis-b943689 ; http://repository.ust.hk/ir/bitstream/1783.1-4214/1/th_redirect.html

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


Texas Tech University

25. Hedayati, Zhian. Random modal interaction of a non-linear aeroelastic structure.

Degree: Mechanical Engineering, 1985, Texas Tech University

 The modal interaction of an aeroelastic structure subjected to random wide band excitation is investigated. An analytical model, represented by three degrees of freedom, is… (more)

Subjects/Keywords: Aeroelasticity  – Mathematical models; Random vibration; Flutter (Aerodynamics); Degree of freedom; Resonant vibration

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APA (6th Edition):

Hedayati, Z. (1985). Random modal interaction of a non-linear aeroelastic structure. (Thesis). Texas Tech University. Retrieved from http://hdl.handle.net/2346/17729

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):

Hedayati, Zhian. “Random modal interaction of a non-linear aeroelastic structure.” 1985. Thesis, Texas Tech University. Accessed July 09, 2020. http://hdl.handle.net/2346/17729.

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

MLA Handbook (7th Edition):

Hedayati, Zhian. “Random modal interaction of a non-linear aeroelastic structure.” 1985. Web. 09 Jul 2020.

Vancouver:

Hedayati Z. Random modal interaction of a non-linear aeroelastic structure. [Internet] [Thesis]. Texas Tech University; 1985. [cited 2020 Jul 09]. Available from: http://hdl.handle.net/2346/17729.

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

Council of Science Editors:

Hedayati Z. Random modal interaction of a non-linear aeroelastic structure. [Thesis]. Texas Tech University; 1985. Available from: http://hdl.handle.net/2346/17729

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


McMaster University

26. Abdou, Sherif. Synthetic Jet Actuator for Active Flow Control.

Degree: MASc, 2014, McMaster University

This thesis investigates the characteristics of a long aspect ratio synthetic jet actuator and its application for the active control of the vibrations of… (more)

Subjects/Keywords: Synthetic Jet; Flow Control; Flow Induced Vibration; Actuator; Tandem Cylinder; Acoustics; Acoustics, Dynamics, and Controls; Aerodynamics and Fluid Mechanics; Other Mechanical Engineering; Acoustics, Dynamics, and Controls

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APA (6th Edition):

Abdou, S. (2014). Synthetic Jet Actuator for Active Flow Control. (Masters Thesis). McMaster University. Retrieved from http://hdl.handle.net/11375/13984

Chicago Manual of Style (16th Edition):

Abdou, Sherif. “Synthetic Jet Actuator for Active Flow Control.” 2014. Masters Thesis, McMaster University. Accessed July 09, 2020. http://hdl.handle.net/11375/13984.

MLA Handbook (7th Edition):

Abdou, Sherif. “Synthetic Jet Actuator for Active Flow Control.” 2014. Web. 09 Jul 2020.

Vancouver:

Abdou S. Synthetic Jet Actuator for Active Flow Control. [Internet] [Masters thesis]. McMaster University; 2014. [cited 2020 Jul 09]. Available from: http://hdl.handle.net/11375/13984.

Council of Science Editors:

Abdou S. Synthetic Jet Actuator for Active Flow Control. [Masters Thesis]. McMaster University; 2014. Available from: http://hdl.handle.net/11375/13984


Hong Kong University of Science and Technology

27. Tse, Kam Tim. Cost and benefits of response mitigation techniques for wind-excited tall buildings.

Degree: 2009, Hong Kong University of Science and Technology

 The advances in height of building structures have magnified their susceptibility to wind-induced vibrations, particularly in typhoon-prone cities. Consequently, considerable efforts have been devoted to… (more)

Subjects/Keywords: Tall buildings  – Aerodynamics ; Tall buildings  – Vibration ; Tall buildings  – Design and construction  – Economic aspects

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APA (6th Edition):

Tse, K. T. (2009). Cost and benefits of response mitigation techniques for wind-excited tall buildings. (Thesis). Hong Kong University of Science and Technology. Retrieved from http://repository.ust.hk/ir/Record/1783.1-5950 ; https://doi.org/10.14711/thesis-b1041199 ; http://repository.ust.hk/ir/bitstream/1783.1-5950/1/th_redirect.html

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):

Tse, Kam Tim. “Cost and benefits of response mitigation techniques for wind-excited tall buildings.” 2009. Thesis, Hong Kong University of Science and Technology. Accessed July 09, 2020. http://repository.ust.hk/ir/Record/1783.1-5950 ; https://doi.org/10.14711/thesis-b1041199 ; http://repository.ust.hk/ir/bitstream/1783.1-5950/1/th_redirect.html.

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

MLA Handbook (7th Edition):

Tse, Kam Tim. “Cost and benefits of response mitigation techniques for wind-excited tall buildings.” 2009. Web. 09 Jul 2020.

Vancouver:

Tse KT. Cost and benefits of response mitigation techniques for wind-excited tall buildings. [Internet] [Thesis]. Hong Kong University of Science and Technology; 2009. [cited 2020 Jul 09]. Available from: http://repository.ust.hk/ir/Record/1783.1-5950 ; https://doi.org/10.14711/thesis-b1041199 ; http://repository.ust.hk/ir/bitstream/1783.1-5950/1/th_redirect.html.

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

Council of Science Editors:

Tse KT. Cost and benefits of response mitigation techniques for wind-excited tall buildings. [Thesis]. Hong Kong University of Science and Technology; 2009. Available from: http://repository.ust.hk/ir/Record/1783.1-5950 ; https://doi.org/10.14711/thesis-b1041199 ; http://repository.ust.hk/ir/bitstream/1783.1-5950/1/th_redirect.html

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


University of Florida

28. Timpe, Amory W. Flow and Structure Interactions of Membrane Wings at Low Reynolds Number.

Degree: MS, Aerospace Engineering - Mechanical and Aerospace Engineering, 2012, University of Florida

 The inherent challenges associated with low Reynolds number flight have stemmed biologically inspired wing designs incorporating highly flexible membranes. Natural membrane wing flyers demonstrate advantages… (more)

Subjects/Keywords: Aerodynamics; Aircraft wings; Modeling; Momentum; Near wakes; Pixels; Shear layers; Velocity; Vibration; Vorticity; compliant  – dic  – flexible  – fluid-structure  – fsi  – mav  – membrane  – piv  – reynolds  – wing

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

APA (6th Edition):

Timpe, A. W. (2012). Flow and Structure Interactions of Membrane Wings at Low Reynolds Number. (Masters Thesis). University of Florida. Retrieved from https://ufdc.ufl.edu/UFE0044220

Chicago Manual of Style (16th Edition):

Timpe, Amory W. “Flow and Structure Interactions of Membrane Wings at Low Reynolds Number.” 2012. Masters Thesis, University of Florida. Accessed July 09, 2020. https://ufdc.ufl.edu/UFE0044220.

MLA Handbook (7th Edition):

Timpe, Amory W. “Flow and Structure Interactions of Membrane Wings at Low Reynolds Number.” 2012. Web. 09 Jul 2020.

Vancouver:

Timpe AW. Flow and Structure Interactions of Membrane Wings at Low Reynolds Number. [Internet] [Masters thesis]. University of Florida; 2012. [cited 2020 Jul 09]. Available from: https://ufdc.ufl.edu/UFE0044220.

Council of Science Editors:

Timpe AW. Flow and Structure Interactions of Membrane Wings at Low Reynolds Number. [Masters Thesis]. University of Florida; 2012. Available from: https://ufdc.ufl.edu/UFE0044220


Georgia Tech

29. Rajmohan, Nischint. Application of hybrid methodology to rotors in steady and maneuvering flight.

Degree: PhD, Aerospace Engineering, 2010, Georgia Tech

 Helicopters are versatile flying machines that have capabilities that are unparalleled by fixed wing aircraft, such as operating in hover, performing vertical take-off and landing… (more)

Subjects/Keywords: Aeroelasticity; Rotorcraft; CFD; Helicopters; Helicopters Aerodynamics; Vibration (Aeronautics) Damping; Computational fluid dynamics

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

APA (6th Edition):

Rajmohan, N. (2010). Application of hybrid methodology to rotors in steady and maneuvering flight. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/34756

Chicago Manual of Style (16th Edition):

Rajmohan, Nischint. “Application of hybrid methodology to rotors in steady and maneuvering flight.” 2010. Doctoral Dissertation, Georgia Tech. Accessed July 09, 2020. http://hdl.handle.net/1853/34756.

MLA Handbook (7th Edition):

Rajmohan, Nischint. “Application of hybrid methodology to rotors in steady and maneuvering flight.” 2010. Web. 09 Jul 2020.

Vancouver:

Rajmohan N. Application of hybrid methodology to rotors in steady and maneuvering flight. [Internet] [Doctoral dissertation]. Georgia Tech; 2010. [cited 2020 Jul 09]. Available from: http://hdl.handle.net/1853/34756.

Council of Science Editors:

Rajmohan N. Application of hybrid methodology to rotors in steady and maneuvering flight. [Doctoral Dissertation]. Georgia Tech; 2010. Available from: http://hdl.handle.net/1853/34756


Ryerson University

30. Bomeman, Stephen R. A New Dynamic Finite Element Formulation with Applications to Composite Aircraft Wings.

Degree: 2004, Ryerson University

 This thesis presents a new dynamic finite element (DFE) formulation for the free vibration of composite wings modelled as beam assemblies. Implementing Euler-Bernoulli beam theory,… (more)

Subjects/Keywords: Airplanes  – Wings  – Design and construction; Vibration (Aeronautics) Airplanes  – Wings  – Vibration  – Measurement; Airplanes  – Wings  – Mathematical models; Aerodynamics  – Technological innovations.

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

APA (6th Edition):

Bomeman, S. R. (2004). A New Dynamic Finite Element Formulation with Applications to Composite Aircraft Wings. (Thesis). Ryerson University. Retrieved from https://digital.library.ryerson.ca/islandora/object/RULA%3A2143

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):

Bomeman, Stephen R. “A New Dynamic Finite Element Formulation with Applications to Composite Aircraft Wings.” 2004. Thesis, Ryerson University. Accessed July 09, 2020. https://digital.library.ryerson.ca/islandora/object/RULA%3A2143.

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

MLA Handbook (7th Edition):

Bomeman, Stephen R. “A New Dynamic Finite Element Formulation with Applications to Composite Aircraft Wings.” 2004. Web. 09 Jul 2020.

Vancouver:

Bomeman SR. A New Dynamic Finite Element Formulation with Applications to Composite Aircraft Wings. [Internet] [Thesis]. Ryerson University; 2004. [cited 2020 Jul 09]. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A2143.

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

Council of Science Editors:

Bomeman SR. A New Dynamic Finite Element Formulation with Applications to Composite Aircraft Wings. [Thesis]. Ryerson University; 2004. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A2143

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

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