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You searched for subject:( Aeroelasticity). Showing records 1 – 30 of 216 total matches.

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1. Peristy, Luke H. EXAMINATION OF SMALL AND LARGE AMPLITUDE AEROELASTIC OSCILLATIONS IN PITCH OF A NACA0012 AIRFOIL.

Degree: MASc (Master of Applied Science/Ma??trise ??s sciences appliqu??es), Mechanical Engineering/G??nie m??canique, 2016, Royal Military College of Canada

One degree of freedom aeroelastic oscillations in pitch of a NACA0012 airfoil at transitional Reynolds numbers were examined experimentally in a wind tunnel using a… (more)

Subjects/Keywords: Aeroelasticity

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

APA (6th Edition):

Peristy, L. H. (2016). EXAMINATION OF SMALL AND LARGE AMPLITUDE AEROELASTIC OSCILLATIONS IN PITCH OF A NACA0012 AIRFOIL. (Masters Thesis). Royal Military College of Canada. Retrieved from http://hdl.handle.net/11264/882

Chicago Manual of Style (16th Edition):

Peristy, Luke H. “EXAMINATION OF SMALL AND LARGE AMPLITUDE AEROELASTIC OSCILLATIONS IN PITCH OF A NACA0012 AIRFOIL.” 2016. Masters Thesis, Royal Military College of Canada. Accessed March 24, 2019. http://hdl.handle.net/11264/882.

MLA Handbook (7th Edition):

Peristy, Luke H. “EXAMINATION OF SMALL AND LARGE AMPLITUDE AEROELASTIC OSCILLATIONS IN PITCH OF A NACA0012 AIRFOIL.” 2016. Web. 24 Mar 2019.

Vancouver:

Peristy LH. EXAMINATION OF SMALL AND LARGE AMPLITUDE AEROELASTIC OSCILLATIONS IN PITCH OF A NACA0012 AIRFOIL. [Internet] [Masters thesis]. Royal Military College of Canada; 2016. [cited 2019 Mar 24]. Available from: http://hdl.handle.net/11264/882.

Council of Science Editors:

Peristy LH. EXAMINATION OF SMALL AND LARGE AMPLITUDE AEROELASTIC OSCILLATIONS IN PITCH OF A NACA0012 AIRFOIL. [Masters Thesis]. Royal Military College of Canada; 2016. Available from: http://hdl.handle.net/11264/882


Texas A&M University

2. Gargoloff, Joaquin Ivan. A numerical method for fully nonlinear aeroelastic analysis.

Degree: 2009, Texas A&M University

 This work presents a numerical method for the analysis of fully nonlinear aeroelastic problems. The aeroelastic model consisted of a Navier-Stokes flow solver, a nonlinear… (more)

Subjects/Keywords: aeroelasticity; cfd

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APA (6th Edition):

Gargoloff, J. I. (2009). A numerical method for fully nonlinear aeroelastic analysis. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1219

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):

Gargoloff, Joaquin Ivan. “A numerical method for fully nonlinear aeroelastic analysis.” 2009. Thesis, Texas A&M University. Accessed March 24, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-1219.

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

MLA Handbook (7th Edition):

Gargoloff, Joaquin Ivan. “A numerical method for fully nonlinear aeroelastic analysis.” 2009. Web. 24 Mar 2019.

Vancouver:

Gargoloff JI. A numerical method for fully nonlinear aeroelastic analysis. [Internet] [Thesis]. Texas A&M University; 2009. [cited 2019 Mar 24]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1219.

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

Council of Science Editors:

Gargoloff JI. A numerical method for fully nonlinear aeroelastic analysis. [Thesis]. Texas A&M University; 2009. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1219

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


KTH

3. Bernardi, Giacomo. Feasibility Study of a 3D CFD Solution for FSI Investigations on NREL 5MW Wind Turbine Blade.

Degree: Heat and Power Technology, 2015, KTH

  With the increase in length of wind turbine blades flutter is becoming a potential design constrain, hence the interest in computational tools for fluid-structure… (more)

Subjects/Keywords: HAWT; CFD; Aeroelasticity

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APA (6th Edition):

Bernardi, G. (2015). Feasibility Study of a 3D CFD Solution for FSI Investigations on NREL 5MW Wind Turbine Blade. (Thesis). KTH. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-159690

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):

Bernardi, Giacomo. “Feasibility Study of a 3D CFD Solution for FSI Investigations on NREL 5MW Wind Turbine Blade.” 2015. Thesis, KTH. Accessed March 24, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-159690.

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

MLA Handbook (7th Edition):

Bernardi, Giacomo. “Feasibility Study of a 3D CFD Solution for FSI Investigations on NREL 5MW Wind Turbine Blade.” 2015. Web. 24 Mar 2019.

Vancouver:

Bernardi G. Feasibility Study of a 3D CFD Solution for FSI Investigations on NREL 5MW Wind Turbine Blade. [Internet] [Thesis]. KTH; 2015. [cited 2019 Mar 24]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-159690.

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

Council of Science Editors:

Bernardi G. Feasibility Study of a 3D CFD Solution for FSI Investigations on NREL 5MW Wind Turbine Blade. [Thesis]. KTH; 2015. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-159690

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


The Ohio State University

4. Swaim, Robert Lee. Active control of booster elasticity.

Degree: PhD, Graduate School, 1966, The Ohio State University

Subjects/Keywords: Engineering; Aeroelasticity

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APA (6th Edition):

Swaim, R. L. (1966). Active control of booster elasticity. (Doctoral Dissertation). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1486634509114617

Chicago Manual of Style (16th Edition):

Swaim, Robert Lee. “Active control of booster elasticity.” 1966. Doctoral Dissertation, The Ohio State University. Accessed March 24, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=osu1486634509114617.

MLA Handbook (7th Edition):

Swaim, Robert Lee. “Active control of booster elasticity.” 1966. Web. 24 Mar 2019.

Vancouver:

Swaim RL. Active control of booster elasticity. [Internet] [Doctoral dissertation]. The Ohio State University; 1966. [cited 2019 Mar 24]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1486634509114617.

Council of Science Editors:

Swaim RL. Active control of booster elasticity. [Doctoral Dissertation]. The Ohio State University; 1966. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1486634509114617


UCLA

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

Degree: Aerospace Engineering, 2014, UCLA

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

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

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APA (6th Edition):

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

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

Chicago Manual of Style (16th Edition):

Mellquist, Erik Charles. “Computational Transonic Flutter Solutions for Cranked Wings by the Direct Eulerian-Lagrangian Method.” 2014. Thesis, UCLA. Accessed March 24, 2019. http://www.escholarship.org/uc/item/9rk54186.

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

MLA Handbook (7th Edition):

Mellquist, Erik Charles. “Computational Transonic Flutter Solutions for Cranked Wings by the Direct Eulerian-Lagrangian Method.” 2014. Web. 24 Mar 2019.

Vancouver:

Mellquist EC. Computational Transonic Flutter Solutions for Cranked Wings by the Direct Eulerian-Lagrangian Method. [Internet] [Thesis]. UCLA; 2014. [cited 2019 Mar 24]. Available from: http://www.escholarship.org/uc/item/9rk54186.

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

Council of Science Editors:

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

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


Delft University of Technology

6. Janssen, M. Aeroelastic Modelling of Composite Rotor Blades:.

Degree: 2015, Delft University of Technology

 This thesis was conducted at KVE Composites Group (The Hague, The Netherlands). The aim of this thesis is to create an aeroelastic model that can… (more)

Subjects/Keywords: rotor; blade; aeroelastic; modelling; aeroelasticity

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APA (6th Edition):

Janssen, M. (2015). Aeroelastic Modelling of Composite Rotor Blades:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:316904df-d86b-415c-803a-9a94df225b21

Chicago Manual of Style (16th Edition):

Janssen, M. “Aeroelastic Modelling of Composite Rotor Blades:.” 2015. Masters Thesis, Delft University of Technology. Accessed March 24, 2019. http://resolver.tudelft.nl/uuid:316904df-d86b-415c-803a-9a94df225b21.

MLA Handbook (7th Edition):

Janssen, M. “Aeroelastic Modelling of Composite Rotor Blades:.” 2015. Web. 24 Mar 2019.

Vancouver:

Janssen M. Aeroelastic Modelling of Composite Rotor Blades:. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2019 Mar 24]. Available from: http://resolver.tudelft.nl/uuid:316904df-d86b-415c-803a-9a94df225b21.

Council of Science Editors:

Janssen M. Aeroelastic Modelling of Composite Rotor Blades:. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:316904df-d86b-415c-803a-9a94df225b21


University of New Mexico

7. Carter, Melissa. Effect of an aeroelastic film on confined subsonic cavity resonance.

Degree: Mechanical Engineering, 2011, University of New Mexico

 EFFECT OF AN AEROELASTIC FILM ON CONFINED SUBSONIC CAVITY RESONANCE by Melissa Carter B.S., Mechanical Engineering, University of New Mexico, 2001 M.S., Mechanical Engineering, University… (more)

Subjects/Keywords: Thin films; Aeroelasticity; Resonators; Cavity.

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APA (6th Edition):

Carter, M. (2011). Effect of an aeroelastic film on confined subsonic cavity resonance. (Masters Thesis). University of New Mexico. Retrieved from http://hdl.handle.net/1928/12833

Chicago Manual of Style (16th Edition):

Carter, Melissa. “Effect of an aeroelastic film on confined subsonic cavity resonance.” 2011. Masters Thesis, University of New Mexico. Accessed March 24, 2019. http://hdl.handle.net/1928/12833.

MLA Handbook (7th Edition):

Carter, Melissa. “Effect of an aeroelastic film on confined subsonic cavity resonance.” 2011. Web. 24 Mar 2019.

Vancouver:

Carter M. Effect of an aeroelastic film on confined subsonic cavity resonance. [Internet] [Masters thesis]. University of New Mexico; 2011. [cited 2019 Mar 24]. Available from: http://hdl.handle.net/1928/12833.

Council of Science Editors:

Carter M. Effect of an aeroelastic film on confined subsonic cavity resonance. [Masters Thesis]. University of New Mexico; 2011. Available from: http://hdl.handle.net/1928/12833


Virginia Tech

8. Ricciardi, Anthony Pasquale. Geometrically Nonlinear Aeroelastic Scaling.

Degree: PhD, Aerospace and Ocean Engineering, 2014, Virginia Tech

 Aeroelastic scaling methodologies are developed for geometrically nonlinear applications. The new methods are demonstrated by designing an aeroelastically scaled model of a suitably nonlinear full-scale… (more)

Subjects/Keywords: Nonlinear; Aeroelasticity; Scaling; SensorCraft

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APA (6th Edition):

Ricciardi, A. P. (2014). Geometrically Nonlinear Aeroelastic Scaling. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/24913

Chicago Manual of Style (16th Edition):

Ricciardi, Anthony Pasquale. “Geometrically Nonlinear Aeroelastic Scaling.” 2014. Doctoral Dissertation, Virginia Tech. Accessed March 24, 2019. http://hdl.handle.net/10919/24913.

MLA Handbook (7th Edition):

Ricciardi, Anthony Pasquale. “Geometrically Nonlinear Aeroelastic Scaling.” 2014. Web. 24 Mar 2019.

Vancouver:

Ricciardi AP. Geometrically Nonlinear Aeroelastic Scaling. [Internet] [Doctoral dissertation]. Virginia Tech; 2014. [cited 2019 Mar 24]. Available from: http://hdl.handle.net/10919/24913.

Council of Science Editors:

Ricciardi AP. Geometrically Nonlinear Aeroelastic Scaling. [Doctoral Dissertation]. Virginia Tech; 2014. Available from: http://hdl.handle.net/10919/24913


Virginia Tech

9. Ricciardi, Anthony Pasquale. Utility of Quasi-Static Gust Loads Certification Methods for Novel Configurations.

Degree: MS, Aerospace and Ocean Engineering, 2011, Virginia Tech

 Aeroelastic gust and maneuver loads have driven the sizing of primary aircraft structures since the beginning of aviation. Methodologies for determining the gust loads on… (more)

Subjects/Keywords: SensorCraft; Aeroelasticity; Gust Loads

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APA (6th Edition):

Ricciardi, A. P. (2011). Utility of Quasi-Static Gust Loads Certification Methods for Novel Configurations. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/35359

Chicago Manual of Style (16th Edition):

Ricciardi, Anthony Pasquale. “Utility of Quasi-Static Gust Loads Certification Methods for Novel Configurations.” 2011. Masters Thesis, Virginia Tech. Accessed March 24, 2019. http://hdl.handle.net/10919/35359.

MLA Handbook (7th Edition):

Ricciardi, Anthony Pasquale. “Utility of Quasi-Static Gust Loads Certification Methods for Novel Configurations.” 2011. Web. 24 Mar 2019.

Vancouver:

Ricciardi AP. Utility of Quasi-Static Gust Loads Certification Methods for Novel Configurations. [Internet] [Masters thesis]. Virginia Tech; 2011. [cited 2019 Mar 24]. Available from: http://hdl.handle.net/10919/35359.

Council of Science Editors:

Ricciardi AP. Utility of Quasi-Static Gust Loads Certification Methods for Novel Configurations. [Masters Thesis]. Virginia Tech; 2011. Available from: http://hdl.handle.net/10919/35359


Virginia Tech

10. Eger, Charles Alfred Gaitan. Design of a Scaled Flight Test Vehicle Including Linear Aeroelastic Effects.

Degree: MS, Aerospace and Ocean Engineering, 2013, Virginia Tech

 A procedure for the design of a scaled aircraft using linear aeroelastic scaling is developed and demonstrated. Previous work has shown the viability in matching… (more)

Subjects/Keywords: Aeroelasticity; Scaling; Joined-wing

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APA (6th Edition):

Eger, C. A. G. (2013). Design of a Scaled Flight Test Vehicle Including Linear Aeroelastic Effects. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/23088

Chicago Manual of Style (16th Edition):

Eger, Charles Alfred Gaitan. “Design of a Scaled Flight Test Vehicle Including Linear Aeroelastic Effects.” 2013. Masters Thesis, Virginia Tech. Accessed March 24, 2019. http://hdl.handle.net/10919/23088.

MLA Handbook (7th Edition):

Eger, Charles Alfred Gaitan. “Design of a Scaled Flight Test Vehicle Including Linear Aeroelastic Effects.” 2013. Web. 24 Mar 2019.

Vancouver:

Eger CAG. Design of a Scaled Flight Test Vehicle Including Linear Aeroelastic Effects. [Internet] [Masters thesis]. Virginia Tech; 2013. [cited 2019 Mar 24]. Available from: http://hdl.handle.net/10919/23088.

Council of Science Editors:

Eger CAG. Design of a Scaled Flight Test Vehicle Including Linear Aeroelastic Effects. [Masters Thesis]. Virginia Tech; 2013. Available from: http://hdl.handle.net/10919/23088


Virginia Tech

11. Butt, Lauren Marie. Design Optimization of a High Aspect Ratio Rigid/Inflatable Wing.

Degree: MS, Aerospace and Ocean Engineering, 2011, Virginia Tech

 High aspect-ratio, long-endurance aircraft require different design modeling from those with traditional moderate aspect ratios. High aspect-ratio, long endurance aircraft are generally more flexible structures… (more)

Subjects/Keywords: Design Optimization; Aeroelasticity; Inflatable Wings

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APA (6th Edition):

Butt, L. M. (2011). Design Optimization of a High Aspect Ratio Rigid/Inflatable Wing. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/42641

Chicago Manual of Style (16th Edition):

Butt, Lauren Marie. “Design Optimization of a High Aspect Ratio Rigid/Inflatable Wing.” 2011. Masters Thesis, Virginia Tech. Accessed March 24, 2019. http://hdl.handle.net/10919/42641.

MLA Handbook (7th Edition):

Butt, Lauren Marie. “Design Optimization of a High Aspect Ratio Rigid/Inflatable Wing.” 2011. Web. 24 Mar 2019.

Vancouver:

Butt LM. Design Optimization of a High Aspect Ratio Rigid/Inflatable Wing. [Internet] [Masters thesis]. Virginia Tech; 2011. [cited 2019 Mar 24]. Available from: http://hdl.handle.net/10919/42641.

Council of Science Editors:

Butt LM. Design Optimization of a High Aspect Ratio Rigid/Inflatable Wing. [Masters Thesis]. Virginia Tech; 2011. Available from: http://hdl.handle.net/10919/42641


Texas A&M University

12. Freno, Brian Andrew. An Efficient Nonlinear Structural Dynamics Solver for Use in Computational Aeroelastic Analysis.

Degree: 2011, Texas A&M University

 Aerospace structures with large aspect ratio, such as airplane wings, rotorcraft blades, wind turbine blades, and jet engine fan and compressor blades, are particularly susceptible… (more)

Subjects/Keywords: aeroelasticity; nonlinear structural dynamics; computational aeroelasticity; elasticity; aerodynamics

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APA (6th Edition):

Freno, B. A. (2011). An Efficient Nonlinear Structural Dynamics Solver for Use in Computational Aeroelastic Analysis. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-8039

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):

Freno, Brian Andrew. “An Efficient Nonlinear Structural Dynamics Solver for Use in Computational Aeroelastic Analysis.” 2011. Thesis, Texas A&M University. Accessed March 24, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-8039.

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

MLA Handbook (7th Edition):

Freno, Brian Andrew. “An Efficient Nonlinear Structural Dynamics Solver for Use in Computational Aeroelastic Analysis.” 2011. Web. 24 Mar 2019.

Vancouver:

Freno BA. An Efficient Nonlinear Structural Dynamics Solver for Use in Computational Aeroelastic Analysis. [Internet] [Thesis]. Texas A&M University; 2011. [cited 2019 Mar 24]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-8039.

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

Council of Science Editors:

Freno BA. An Efficient Nonlinear Structural Dynamics Solver for Use in Computational Aeroelastic Analysis. [Thesis]. Texas A&M University; 2011. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-8039

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


University of Canterbury

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

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

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

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

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APA (6th Edition):

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

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

Chicago Manual of Style (16th Edition):

Pons, Arion Douglas. “Aeroelastic flutter as a multiparameter eigenvalue problem.” 2015. Thesis, University of Canterbury. Accessed March 24, 2019. http://hdl.handle.net/10092/11265.

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

MLA Handbook (7th Edition):

Pons, Arion Douglas. “Aeroelastic flutter as a multiparameter eigenvalue problem.” 2015. Web. 24 Mar 2019.

Vancouver:

Pons AD. Aeroelastic flutter as a multiparameter eigenvalue problem. [Internet] [Thesis]. University of Canterbury; 2015. [cited 2019 Mar 24]. Available from: http://hdl.handle.net/10092/11265.

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

Council of Science Editors:

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

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


Georgia Tech

14. Chae, Seungmook. Effect of Follower Forces on Aeroelastic Stability of Flexible Structures.

Degree: PhD, Aerospace Engineering, 2004, Georgia Tech

 Missile bodies and wings are typical examples of structures that can be represented by beam models. Such structures, loaded by follower forces along with aerodynamics,… (more)

Subjects/Keywords: Aeroelasticity; Follower force

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APA (6th Edition):

Chae, S. (2004). Effect of Follower Forces on Aeroelastic Stability of Flexible Structures. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/5037

Chicago Manual of Style (16th Edition):

Chae, Seungmook. “Effect of Follower Forces on Aeroelastic Stability of Flexible Structures.” 2004. Doctoral Dissertation, Georgia Tech. Accessed March 24, 2019. http://hdl.handle.net/1853/5037.

MLA Handbook (7th Edition):

Chae, Seungmook. “Effect of Follower Forces on Aeroelastic Stability of Flexible Structures.” 2004. Web. 24 Mar 2019.

Vancouver:

Chae S. Effect of Follower Forces on Aeroelastic Stability of Flexible Structures. [Internet] [Doctoral dissertation]. Georgia Tech; 2004. [cited 2019 Mar 24]. Available from: http://hdl.handle.net/1853/5037.

Council of Science Editors:

Chae S. Effect of Follower Forces on Aeroelastic Stability of Flexible Structures. [Doctoral Dissertation]. Georgia Tech; 2004. Available from: http://hdl.handle.net/1853/5037


University of Manchester

15. Miller, Simon James. Adaptive wing structures for aeroelastic drag reduction and loads alleviation.

Degree: PhD, 2011, University of Manchester

 An investigation into two distinct novel adaptive structures concepts is performed with a view to improving the aerodynamic efficiency of aircraft wings.The main focus of… (more)

Subjects/Keywords: 629.13; Aeroelasticity; Aircraft morphing; Adaptive wing structures

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APA (6th Edition):

Miller, S. J. (2011). Adaptive wing structures for aeroelastic drag reduction and loads alleviation. (Doctoral Dissertation). University of Manchester. Retrieved from https://www.research.manchester.ac.uk/portal/en/theses/adaptive-wing-structures-for-aeroelastic-drag-reduction-and-loadsalleviation(562181ed-7153-44cb-b0c7-9bfe1f79ae0f).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.542701

Chicago Manual of Style (16th Edition):

Miller, Simon James. “Adaptive wing structures for aeroelastic drag reduction and loads alleviation.” 2011. Doctoral Dissertation, University of Manchester. Accessed March 24, 2019. https://www.research.manchester.ac.uk/portal/en/theses/adaptive-wing-structures-for-aeroelastic-drag-reduction-and-loadsalleviation(562181ed-7153-44cb-b0c7-9bfe1f79ae0f).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.542701.

MLA Handbook (7th Edition):

Miller, Simon James. “Adaptive wing structures for aeroelastic drag reduction and loads alleviation.” 2011. Web. 24 Mar 2019.

Vancouver:

Miller SJ. Adaptive wing structures for aeroelastic drag reduction and loads alleviation. [Internet] [Doctoral dissertation]. University of Manchester; 2011. [cited 2019 Mar 24]. Available from: https://www.research.manchester.ac.uk/portal/en/theses/adaptive-wing-structures-for-aeroelastic-drag-reduction-and-loadsalleviation(562181ed-7153-44cb-b0c7-9bfe1f79ae0f).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.542701.

Council of Science Editors:

Miller SJ. Adaptive wing structures for aeroelastic drag reduction and loads alleviation. [Doctoral Dissertation]. University of Manchester; 2011. Available from: https://www.research.manchester.ac.uk/portal/en/theses/adaptive-wing-structures-for-aeroelastic-drag-reduction-and-loadsalleviation(562181ed-7153-44cb-b0c7-9bfe1f79ae0f).html ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.542701


University of Manchester

16. Miller, Simon James. Adaptive wing structures for aeroelastic drag reduction and loadsalleviation.

Degree: 2011, University of Manchester

 An investigation into two distinct novel adaptive structures concepts is performed with a view to improving the aerodynamic efficiency of aircraft wings.The main focus of… (more)

Subjects/Keywords: Aeroelasticity; Aircraft morphing; Adaptive wing structures

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APA (6th Edition):

Miller, S. J. (2011). Adaptive wing structures for aeroelastic drag reduction and loadsalleviation. (Doctoral Dissertation). University of Manchester. Retrieved from http://www.manchester.ac.uk/escholar/uk-ac-man-scw:120148

Chicago Manual of Style (16th Edition):

Miller, Simon James. “Adaptive wing structures for aeroelastic drag reduction and loadsalleviation.” 2011. Doctoral Dissertation, University of Manchester. Accessed March 24, 2019. http://www.manchester.ac.uk/escholar/uk-ac-man-scw:120148.

MLA Handbook (7th Edition):

Miller, Simon James. “Adaptive wing structures for aeroelastic drag reduction and loadsalleviation.” 2011. Web. 24 Mar 2019.

Vancouver:

Miller SJ. Adaptive wing structures for aeroelastic drag reduction and loadsalleviation. [Internet] [Doctoral dissertation]. University of Manchester; 2011. [cited 2019 Mar 24]. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:120148.

Council of Science Editors:

Miller SJ. Adaptive wing structures for aeroelastic drag reduction and loadsalleviation. [Doctoral Dissertation]. University of Manchester; 2011. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:120148


University of British Columbia

17. Slater, Jonathan Ernest. Aeroelastic instability of a structural angle section .

Degree: 1969, University of British Columbia

 Angle section members, used in open engineering structures, have been known to experience large amplitude oscillations when exposed to normal atmospheric winds, and in a… (more)

Subjects/Keywords: Aeroelasticity; Angles  – Vibration

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APA (6th Edition):

Slater, J. E. (1969). Aeroelastic instability of a structural angle section . (Thesis). University of British Columbia. Retrieved from http://hdl.handle.net/2429/35618

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):

Slater, Jonathan Ernest. “Aeroelastic instability of a structural angle section .” 1969. Thesis, University of British Columbia. Accessed March 24, 2019. http://hdl.handle.net/2429/35618.

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

MLA Handbook (7th Edition):

Slater, Jonathan Ernest. “Aeroelastic instability of a structural angle section .” 1969. Web. 24 Mar 2019.

Vancouver:

Slater JE. Aeroelastic instability of a structural angle section . [Internet] [Thesis]. University of British Columbia; 1969. [cited 2019 Mar 24]. Available from: http://hdl.handle.net/2429/35618.

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

Council of Science Editors:

Slater JE. Aeroelastic instability of a structural angle section . [Thesis]. University of British Columbia; 1969. Available from: http://hdl.handle.net/2429/35618

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


Delft University of Technology

18. Natella, M. Coupled Nonlinear Aeroelasticity and Flight Dynamics for Stability Analysis of Flexible Wing Structures:.

Degree: 2015, Delft University of Technology

 The present work thus develops a low-fidelity formulation to investigate the flight dynamic stability of a flexible wing structure. The model is verified against other… (more)

Subjects/Keywords: aeroelasticity; flight dynamics; flexible wings; stability analysis

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APA (6th Edition):

Natella, M. (2015). Coupled Nonlinear Aeroelasticity and Flight Dynamics for Stability Analysis of Flexible Wing Structures:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:39984220-1d55-43fb-b42c-8a692a979211

Chicago Manual of Style (16th Edition):

Natella, M. “Coupled Nonlinear Aeroelasticity and Flight Dynamics for Stability Analysis of Flexible Wing Structures:.” 2015. Masters Thesis, Delft University of Technology. Accessed March 24, 2019. http://resolver.tudelft.nl/uuid:39984220-1d55-43fb-b42c-8a692a979211.

MLA Handbook (7th Edition):

Natella, M. “Coupled Nonlinear Aeroelasticity and Flight Dynamics for Stability Analysis of Flexible Wing Structures:.” 2015. Web. 24 Mar 2019.

Vancouver:

Natella M. Coupled Nonlinear Aeroelasticity and Flight Dynamics for Stability Analysis of Flexible Wing Structures:. [Internet] [Masters thesis]. Delft University of Technology; 2015. [cited 2019 Mar 24]. Available from: http://resolver.tudelft.nl/uuid:39984220-1d55-43fb-b42c-8a692a979211.

Council of Science Editors:

Natella M. Coupled Nonlinear Aeroelasticity and Flight Dynamics for Stability Analysis of Flexible Wing Structures:. [Masters Thesis]. Delft University of Technology; 2015. Available from: http://resolver.tudelft.nl/uuid:39984220-1d55-43fb-b42c-8a692a979211


Delft University of Technology

19. Kalthof, R.L.C. Multibody Dynamics Modeling of Flexible Aircraft Flight Dynamics:.

Degree: 2014, Delft University of Technology

 Because of the focus on weight minimization, aircraft are becoming more and more flexible. Therefore, the frequency separation between flight mechanics motion and structural vibration… (more)

Subjects/Keywords: multibody dynamics; aeroelasticity; SimMechanics; flight dynamics

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APA (6th Edition):

Kalthof, R. L. C. (2014). Multibody Dynamics Modeling of Flexible Aircraft Flight Dynamics:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:6aa1d6a0-0601-4595-97b3-047117fc6a97

Chicago Manual of Style (16th Edition):

Kalthof, R L C. “Multibody Dynamics Modeling of Flexible Aircraft Flight Dynamics:.” 2014. Masters Thesis, Delft University of Technology. Accessed March 24, 2019. http://resolver.tudelft.nl/uuid:6aa1d6a0-0601-4595-97b3-047117fc6a97.

MLA Handbook (7th Edition):

Kalthof, R L C. “Multibody Dynamics Modeling of Flexible Aircraft Flight Dynamics:.” 2014. Web. 24 Mar 2019.

Vancouver:

Kalthof RLC. Multibody Dynamics Modeling of Flexible Aircraft Flight Dynamics:. [Internet] [Masters thesis]. Delft University of Technology; 2014. [cited 2019 Mar 24]. Available from: http://resolver.tudelft.nl/uuid:6aa1d6a0-0601-4595-97b3-047117fc6a97.

Council of Science Editors:

Kalthof RLC. Multibody Dynamics Modeling of Flexible Aircraft Flight Dynamics:. [Masters Thesis]. Delft University of Technology; 2014. Available from: http://resolver.tudelft.nl/uuid:6aa1d6a0-0601-4595-97b3-047117fc6a97

20. Král Radomil. Numerical and experimental solutions of self-induced instability of bridge .

Degree: 2011, Czech University of Technology

 The thesis is focused on a solution of self-induced oscillations and instabilities of slender beams in the wind. It uses a combination of appropriately selected… (more)

Subjects/Keywords: bridge aeroelasticity; flutter instability; wind-structure interaction; bluff body.

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APA (6th Edition):

Radomil, K. (2011). Numerical and experimental solutions of self-induced instability of bridge . (Thesis). Czech University of Technology. Retrieved from http://hdl.handle.net/10467/8083

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):

Radomil, Král. “Numerical and experimental solutions of self-induced instability of bridge .” 2011. Thesis, Czech University of Technology. Accessed March 24, 2019. http://hdl.handle.net/10467/8083.

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

MLA Handbook (7th Edition):

Radomil, Král. “Numerical and experimental solutions of self-induced instability of bridge .” 2011. Web. 24 Mar 2019.

Vancouver:

Radomil K. Numerical and experimental solutions of self-induced instability of bridge . [Internet] [Thesis]. Czech University of Technology; 2011. [cited 2019 Mar 24]. Available from: http://hdl.handle.net/10467/8083.

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

Council of Science Editors:

Radomil K. Numerical and experimental solutions of self-induced instability of bridge . [Thesis]. Czech University of Technology; 2011. Available from: http://hdl.handle.net/10467/8083

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

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

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

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Bidinotto, Jorge Henrique. “Proposta conceitual de excitador de \"flutter\" alternativo para ensaios em vôo.” 2007. Masters Thesis, University of São Paulo. Accessed March 24, 2019. http://www.teses.usp.br/teses/disponiveis/18/18148/tde-27052009-142508/ ;.

MLA Handbook (7th Edition):

Bidinotto, Jorge Henrique. “Proposta conceitual de excitador de \"flutter\" alternativo para ensaios em vôo.” 2007. Web. 24 Mar 2019.

Vancouver:

Bidinotto JH. Proposta conceitual de excitador de \"flutter\" alternativo para ensaios em vôo. [Internet] [Masters thesis]. University of São Paulo; 2007. [cited 2019 Mar 24]. Available from: http://www.teses.usp.br/teses/disponiveis/18/18148/tde-27052009-142508/ ;.

Council of Science Editors:

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


Texas A&M University

22. Nichkawde, Chetan. Nonlinear aeroelastic analysis of high aspect-ratio wings using the method of numerical continuation.

Degree: 2006, Texas A&M University

 This research explores the impact of kinematic structural nonlinearities on the dynamics of a highly deformable cantilevered wing. Two different theoretical formulations are presented and… (more)

Subjects/Keywords: Aeroelasticity; Nonlinear; Continuation; Bifurcation

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APA (6th Edition):

Nichkawde, C. (2006). Nonlinear aeroelastic analysis of high aspect-ratio wings using the method of numerical continuation. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/3846

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):

Nichkawde, Chetan. “Nonlinear aeroelastic analysis of high aspect-ratio wings using the method of numerical continuation.” 2006. Thesis, Texas A&M University. Accessed March 24, 2019. http://hdl.handle.net/1969.1/3846.

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

MLA Handbook (7th Edition):

Nichkawde, Chetan. “Nonlinear aeroelastic analysis of high aspect-ratio wings using the method of numerical continuation.” 2006. Web. 24 Mar 2019.

Vancouver:

Nichkawde C. Nonlinear aeroelastic analysis of high aspect-ratio wings using the method of numerical continuation. [Internet] [Thesis]. Texas A&M University; 2006. [cited 2019 Mar 24]. Available from: http://hdl.handle.net/1969.1/3846.

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

Council of Science Editors:

Nichkawde C. Nonlinear aeroelastic analysis of high aspect-ratio wings using the method of numerical continuation. [Thesis]. Texas A&M University; 2006. Available from: http://hdl.handle.net/1969.1/3846

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


Texas A&M University

23. Lucas, Amy Marie. Gust Load Alleviation for an Aeroelastic System Using Nonlinear Control.

Degree: 2010, Texas A&M University

 The author develops a nonlinear longitudinal model of an aircraft modeled by rigid fuselage, tail, and wing, where the wing is attached to the fuselage… (more)

Subjects/Keywords: Lyapunov Control; Aeroelasticity; Nonlinear Response; Limit Cycle Oscillation; LCO; nonlinear control

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APA (6th Edition):

Lucas, A. M. (2010). Gust Load Alleviation for an Aeroelastic System Using Nonlinear Control. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2009-08-1504

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):

Lucas, Amy Marie. “Gust Load Alleviation for an Aeroelastic System Using Nonlinear Control.” 2010. Thesis, Texas A&M University. Accessed March 24, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2009-08-1504.

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

MLA Handbook (7th Edition):

Lucas, Amy Marie. “Gust Load Alleviation for an Aeroelastic System Using Nonlinear Control.” 2010. Web. 24 Mar 2019.

Vancouver:

Lucas AM. Gust Load Alleviation for an Aeroelastic System Using Nonlinear Control. [Internet] [Thesis]. Texas A&M University; 2010. [cited 2019 Mar 24]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2009-08-1504.

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

Council of Science Editors:

Lucas AM. Gust Load Alleviation for an Aeroelastic System Using Nonlinear Control. [Thesis]. Texas A&M University; 2010. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2009-08-1504

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

24. Elgohary, Tarek Adel Abdelsalam. Nonlinear Analysis of a Two DOF Piecewise Linear Aeroelastic System.

Degree: 2011, Texas A&M University

 The nonlinear dynamic analysis of aeroelastic systems is a topic that has been covered extensively in the literature. The two main sources of nonlinearities in… (more)

Subjects/Keywords: Aeroelasticity; piecewise linear

…for the problem discussing nonlinear aeroelasticity and its effects on flight and its… 

Page 1 Page 2 Page 3 Page 4 Page 5 Page 6 Page 7

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APA (6th Edition):

Elgohary, T. A. A. (2011). Nonlinear Analysis of a Two DOF Piecewise Linear Aeroelastic System. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2010-08-8012

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):

Elgohary, Tarek Adel Abdelsalam. “Nonlinear Analysis of a Two DOF Piecewise Linear Aeroelastic System.” 2011. Thesis, Texas A&M University. Accessed March 24, 2019. http://hdl.handle.net/1969.1/ETD-TAMU-2010-08-8012.

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

MLA Handbook (7th Edition):

Elgohary, Tarek Adel Abdelsalam. “Nonlinear Analysis of a Two DOF Piecewise Linear Aeroelastic System.” 2011. Web. 24 Mar 2019.

Vancouver:

Elgohary TAA. Nonlinear Analysis of a Two DOF Piecewise Linear Aeroelastic System. [Internet] [Thesis]. Texas A&M University; 2011. [cited 2019 Mar 24]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-08-8012.

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

Council of Science Editors:

Elgohary TAA. Nonlinear Analysis of a Two DOF Piecewise Linear Aeroelastic System. [Thesis]. Texas A&M University; 2011. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-08-8012

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


University of Adelaide

25. Prime, Zebb David. Robust scheduling control of aeroelasticity.

Degree: 2010, University of Adelaide

Aeroelasticity is a broad term describing the often complex interactions between structural mechanics and aerodynamics. Aeroelastic phenomena such as divergence and flutter are potentially destructive,… (more)

Subjects/Keywords: aeroelasticity; aeroservo elasticity; robust control; linear parameter; varying control; LPV control

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APA (6th Edition):

Prime, Z. D. (2010). Robust scheduling control of aeroelasticity. (Thesis). University of Adelaide. Retrieved from http://hdl.handle.net/2440/67016

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):

Prime, Zebb David. “Robust scheduling control of aeroelasticity.” 2010. Thesis, University of Adelaide. Accessed March 24, 2019. http://hdl.handle.net/2440/67016.

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

MLA Handbook (7th Edition):

Prime, Zebb David. “Robust scheduling control of aeroelasticity.” 2010. Web. 24 Mar 2019.

Vancouver:

Prime ZD. Robust scheduling control of aeroelasticity. [Internet] [Thesis]. University of Adelaide; 2010. [cited 2019 Mar 24]. Available from: http://hdl.handle.net/2440/67016.

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

Council of Science Editors:

Prime ZD. Robust scheduling control of aeroelasticity. [Thesis]. University of Adelaide; 2010. Available from: http://hdl.handle.net/2440/67016

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


Cal Poly

26. Chin, Alexander Wong. Integration of Aeroservoelastic Properties into the NASA Dryden F/A-18 Simulator Using Flight Data from the Active Aeroelastic Wing Program.

Degree: MS, Aerospace Engineering, 2011, Cal Poly

  Aircraft structures have varying stiffness levels making them flexible. Consequently, this elastic property becomes increasingly important at high speeds affecting the flight dynamics of… (more)

Subjects/Keywords: aeroservoelasticity; aeroelasticity; simulation; aaw; interpolation; discretize; Navigation, Guidance, Control and Dynamics

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APA (6th Edition):

Chin, A. W. (2011). Integration of Aeroservoelastic Properties into the NASA Dryden F/A-18 Simulator Using Flight Data from the Active Aeroelastic Wing Program. (Masters Thesis). Cal Poly. Retrieved from http://digitalcommons.calpoly.edu/theses/489 ; 10.15368/theses.2011.43

Chicago Manual of Style (16th Edition):

Chin, Alexander Wong. “Integration of Aeroservoelastic Properties into the NASA Dryden F/A-18 Simulator Using Flight Data from the Active Aeroelastic Wing Program.” 2011. Masters Thesis, Cal Poly. Accessed March 24, 2019. http://digitalcommons.calpoly.edu/theses/489 ; 10.15368/theses.2011.43.

MLA Handbook (7th Edition):

Chin, Alexander Wong. “Integration of Aeroservoelastic Properties into the NASA Dryden F/A-18 Simulator Using Flight Data from the Active Aeroelastic Wing Program.” 2011. Web. 24 Mar 2019.

Vancouver:

Chin AW. Integration of Aeroservoelastic Properties into the NASA Dryden F/A-18 Simulator Using Flight Data from the Active Aeroelastic Wing Program. [Internet] [Masters thesis]. Cal Poly; 2011. [cited 2019 Mar 24]. Available from: http://digitalcommons.calpoly.edu/theses/489 ; 10.15368/theses.2011.43.

Council of Science Editors:

Chin AW. Integration of Aeroservoelastic Properties into the NASA Dryden F/A-18 Simulator Using Flight Data from the Active Aeroelastic Wing Program. [Masters Thesis]. Cal Poly; 2011. Available from: http://digitalcommons.calpoly.edu/theses/489 ; 10.15368/theses.2011.43


Miami University

27. Fellows, Mark T. Aeroelastic Stability and Control of Rectangular Plates with Compliant Boundary Supports.

Degree: MS, Computational Science and Engineering, 2014, Miami University

 A proposed design to reduce airframe noise emissions by attaching a flexible fairing between the flap and trailing edge of airplane wings has inspired new… (more)

Subjects/Keywords: Aerospace Engineering; Mechanical Engineering; aeroelasticity; rectangular plate; control; flutter; buckling

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APA (6th Edition):

Fellows, M. T. (2014). Aeroelastic Stability and Control of Rectangular Plates with Compliant Boundary Supports. (Masters Thesis). Miami University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=miami1407440336

Chicago Manual of Style (16th Edition):

Fellows, Mark T. “Aeroelastic Stability and Control of Rectangular Plates with Compliant Boundary Supports.” 2014. Masters Thesis, Miami University. Accessed March 24, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=miami1407440336.

MLA Handbook (7th Edition):

Fellows, Mark T. “Aeroelastic Stability and Control of Rectangular Plates with Compliant Boundary Supports.” 2014. Web. 24 Mar 2019.

Vancouver:

Fellows MT. Aeroelastic Stability and Control of Rectangular Plates with Compliant Boundary Supports. [Internet] [Masters thesis]. Miami University; 2014. [cited 2019 Mar 24]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=miami1407440336.

Council of Science Editors:

Fellows MT. Aeroelastic Stability and Control of Rectangular Plates with Compliant Boundary Supports. [Masters Thesis]. Miami University; 2014. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=miami1407440336


University of Kentucky

28. Simpson, Andrew D. DESIGN AND EVALUATION OF INFLATABLE WINGS FOR UAVs.

Degree: 2008, University of Kentucky

 Performance of inflatable wings was investigated through laboratory, wind tunnel and flight-testing. Three airfoils were investigated, an inflatable-rigidazable wing, an inflatable polyurethane wing and a… (more)

Subjects/Keywords: Inflatable Wings; Aerodynamics; Aeroelasticity; Flight Testing; Unmanned Aerial Vehicle (UAV)

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APA (6th Edition):

Simpson, A. D. (2008). DESIGN AND EVALUATION OF INFLATABLE WINGS FOR UAVs. (Doctoral Dissertation). University of Kentucky. Retrieved from http://uknowledge.uky.edu/gradschool_diss/589

Chicago Manual of Style (16th Edition):

Simpson, Andrew D. “DESIGN AND EVALUATION OF INFLATABLE WINGS FOR UAVs.” 2008. Doctoral Dissertation, University of Kentucky. Accessed March 24, 2019. http://uknowledge.uky.edu/gradschool_diss/589.

MLA Handbook (7th Edition):

Simpson, Andrew D. “DESIGN AND EVALUATION OF INFLATABLE WINGS FOR UAVs.” 2008. Web. 24 Mar 2019.

Vancouver:

Simpson AD. DESIGN AND EVALUATION OF INFLATABLE WINGS FOR UAVs. [Internet] [Doctoral dissertation]. University of Kentucky; 2008. [cited 2019 Mar 24]. Available from: http://uknowledge.uky.edu/gradschool_diss/589.

Council of Science Editors:

Simpson AD. DESIGN AND EVALUATION OF INFLATABLE WINGS FOR UAVs. [Doctoral Dissertation]. University of Kentucky; 2008. Available from: http://uknowledge.uky.edu/gradschool_diss/589


Cornell University

29. Bryant, Matthew. Aeroelastic Flutter Vibration Energy Harvesting: Modeling, Testing, And System Design .

Degree: 2012, Cornell University

 The rapid proliferation of wireless sensors and microelectronics has spurred considerable interest in developing small scale devices that convert ambient energy sources to electrical power.… (more)

Subjects/Keywords: Energy Harvesting; Piezoelectric; Aeroelasticity; Flutter; Flapping; Wind Power; Self Powered

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APA (6th Edition):

Bryant, M. (2012). Aeroelastic Flutter Vibration Energy Harvesting: Modeling, Testing, And System Design . (Thesis). Cornell University. Retrieved from http://hdl.handle.net/1813/31459

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):

Bryant, Matthew. “Aeroelastic Flutter Vibration Energy Harvesting: Modeling, Testing, And System Design .” 2012. Thesis, Cornell University. Accessed March 24, 2019. http://hdl.handle.net/1813/31459.

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

MLA Handbook (7th Edition):

Bryant, Matthew. “Aeroelastic Flutter Vibration Energy Harvesting: Modeling, Testing, And System Design .” 2012. Web. 24 Mar 2019.

Vancouver:

Bryant M. Aeroelastic Flutter Vibration Energy Harvesting: Modeling, Testing, And System Design . [Internet] [Thesis]. Cornell University; 2012. [cited 2019 Mar 24]. Available from: http://hdl.handle.net/1813/31459.

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

Council of Science Editors:

Bryant M. Aeroelastic Flutter Vibration Energy Harvesting: Modeling, Testing, And System Design . [Thesis]. Cornell University; 2012. Available from: http://hdl.handle.net/1813/31459

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


UCLA

30. Gariffo, James Michael. Generalized Reduced Order Modeling of Aeroservoelastic Systems.

Degree: Mechanical Engineering, 2013, UCLA

 Transonic aeroelastic and aeroservoelastic (ASE) modeling presents a significant technical and computational challenge. Flow fields with a mixture of subsonic and supersonic flow, as well… (more)

Subjects/Keywords: Mechanical engineering; Aerospace engineering; aeroelasticity; aeroservoelasticity; flutter; reduced-order modeling; transonic

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

APA (6th Edition):

Gariffo, J. M. (2013). Generalized Reduced Order Modeling of Aeroservoelastic Systems. (Thesis). UCLA. Retrieved from http://www.escholarship.org/uc/item/0rc0c11t

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):

Gariffo, James Michael. “Generalized Reduced Order Modeling of Aeroservoelastic Systems.” 2013. Thesis, UCLA. Accessed March 24, 2019. http://www.escholarship.org/uc/item/0rc0c11t.

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

MLA Handbook (7th Edition):

Gariffo, James Michael. “Generalized Reduced Order Modeling of Aeroservoelastic Systems.” 2013. Web. 24 Mar 2019.

Vancouver:

Gariffo JM. Generalized Reduced Order Modeling of Aeroservoelastic Systems. [Internet] [Thesis]. UCLA; 2013. [cited 2019 Mar 24]. Available from: http://www.escholarship.org/uc/item/0rc0c11t.

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

Council of Science Editors:

Gariffo JM. Generalized Reduced Order Modeling of Aeroservoelastic Systems. [Thesis]. UCLA; 2013. Available from: http://www.escholarship.org/uc/item/0rc0c11t

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

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