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You searched for subject:(Aeroelasticity). Showing records 1 – 30 of 286 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 September 18, 2020. 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. 18 Sep 2020.

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 2020 Sep 18]. 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


KTH

2. 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 September 18, 2020. 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. 18 Sep 2020.

Vancouver:

Bernardi G. Feasibility Study of a 3D CFD Solution for FSI Investigations on NREL 5MW Wind Turbine Blade. [Internet] [Thesis]. KTH; 2015. [cited 2020 Sep 18]. 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

3. 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 September 18, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=osu1486634509114617.

MLA Handbook (7th Edition):

Swaim, Robert Lee. “Active control of booster elasticity.” 1966. Web. 18 Sep 2020.

Vancouver:

Swaim RL. Active control of booster elasticity. [Internet] [Doctoral dissertation]. The Ohio State University; 1966. [cited 2020 Sep 18]. 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

4. 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 September 18, 2020. 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. 18 Sep 2020.

Vancouver:

Mellquist EC. Computational Transonic Flutter Solutions for Cranked Wings by the Direct Eulerian-Lagrangian Method. [Internet] [Thesis]. UCLA; 2014. [cited 2020 Sep 18]. 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


Texas A&M University

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

Degree: PhD, Aerospace Engineering, 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. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1219

Chicago Manual of Style (16th Edition):

Gargoloff, Joaquin Ivan. “A numerical method for fully nonlinear aeroelastic analysis.” 2009. Doctoral Dissertation, Texas A&M University. Accessed September 18, 2020. http://hdl.handle.net/1969.1/ETD-TAMU-1219.

MLA Handbook (7th Edition):

Gargoloff, Joaquin Ivan. “A numerical method for fully nonlinear aeroelastic analysis.” 2009. Web. 18 Sep 2020.

Vancouver:

Gargoloff JI. A numerical method for fully nonlinear aeroelastic analysis. [Internet] [Doctoral dissertation]. Texas A&M University; 2009. [cited 2020 Sep 18]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1219.

Council of Science Editors:

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


Duke University

6. McHugh, Kevin Andrew. Large Deflection Inextensible Beams and Plates and their Responses to Nonconservative Forces: Theory and Computations .

Degree: 2020, Duke University

  There is a growing interest among aeroelasticity researchers for insight into large deflection oscillations of aerospace structures. Here, a new beam and plate model… (more)

Subjects/Keywords: Mechanical engineering; Aeroelasticity; Nonlinear Dynamics

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APA (6th Edition):

McHugh, K. A. (2020). Large Deflection Inextensible Beams and Plates and their Responses to Nonconservative Forces: Theory and Computations . (Thesis). Duke University. Retrieved from http://hdl.handle.net/10161/20858

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):

McHugh, Kevin Andrew. “Large Deflection Inextensible Beams and Plates and their Responses to Nonconservative Forces: Theory and Computations .” 2020. Thesis, Duke University. Accessed September 18, 2020. http://hdl.handle.net/10161/20858.

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

MLA Handbook (7th Edition):

McHugh, Kevin Andrew. “Large Deflection Inextensible Beams and Plates and their Responses to Nonconservative Forces: Theory and Computations .” 2020. Web. 18 Sep 2020.

Vancouver:

McHugh KA. Large Deflection Inextensible Beams and Plates and their Responses to Nonconservative Forces: Theory and Computations . [Internet] [Thesis]. Duke University; 2020. [cited 2020 Sep 18]. Available from: http://hdl.handle.net/10161/20858.

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

Council of Science Editors:

McHugh KA. Large Deflection Inextensible Beams and Plates and their Responses to Nonconservative Forces: Theory and Computations . [Thesis]. Duke University; 2020. Available from: http://hdl.handle.net/10161/20858

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


Virginia Tech

7. 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 September 18, 2020. 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. 18 Sep 2020.

Vancouver:

Ricciardi AP. Utility of Quasi-Static Gust Loads Certification Methods for Novel Configurations. [Internet] [Masters thesis]. Virginia Tech; 2011. [cited 2020 Sep 18]. 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

8. 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 September 18, 2020. 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. 18 Sep 2020.

Vancouver:

Butt LM. Design Optimization of a High Aspect Ratio Rigid/Inflatable Wing. [Internet] [Masters thesis]. Virginia Tech; 2011. [cited 2020 Sep 18]. 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


Virginia Tech

9. 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 September 18, 2020. http://hdl.handle.net/10919/24913.

MLA Handbook (7th Edition):

Ricciardi, Anthony Pasquale. “Geometrically Nonlinear Aeroelastic Scaling.” 2014. Web. 18 Sep 2020.

Vancouver:

Ricciardi AP. Geometrically Nonlinear Aeroelastic Scaling. [Internet] [Doctoral dissertation]. Virginia Tech; 2014. [cited 2020 Sep 18]. 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

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

Degree: MS, Aerospace 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 September 18, 2020. 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. 18 Sep 2020.

Vancouver:

Eger CAG. Design of a Scaled Flight Test Vehicle Including Linear Aeroelastic Effects. [Internet] [Masters thesis]. Virginia Tech; 2013. [cited 2020 Sep 18]. 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


Delft University of Technology

11. Verdonck, Hendrik (author). Improvements on the application of direct-CFD in unsteady aeroelastic simulations.

Degree: 2019, Delft University of Technology

 Aircraft manufacturers have to prove a flutter free design for all operational cases within the complete flight envelope plus a safety margin. This certification process… (more)

Subjects/Keywords: Aeroelasticity; Flutter; Direct-CFD

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APA (6th Edition):

Verdonck, H. (. (2019). Improvements on the application of direct-CFD in unsteady aeroelastic simulations. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:b65e68ed-933e-4f6c-9e4a-305c44166569

Chicago Manual of Style (16th Edition):

Verdonck, Hendrik (author). “Improvements on the application of direct-CFD in unsteady aeroelastic simulations.” 2019. Masters Thesis, Delft University of Technology. Accessed September 18, 2020. http://resolver.tudelft.nl/uuid:b65e68ed-933e-4f6c-9e4a-305c44166569.

MLA Handbook (7th Edition):

Verdonck, Hendrik (author). “Improvements on the application of direct-CFD in unsteady aeroelastic simulations.” 2019. Web. 18 Sep 2020.

Vancouver:

Verdonck H(. Improvements on the application of direct-CFD in unsteady aeroelastic simulations. [Internet] [Masters thesis]. Delft University of Technology; 2019. [cited 2020 Sep 18]. Available from: http://resolver.tudelft.nl/uuid:b65e68ed-933e-4f6c-9e4a-305c44166569.

Council of Science Editors:

Verdonck H(. Improvements on the application of direct-CFD in unsteady aeroelastic simulations. [Masters Thesis]. Delft University of Technology; 2019. Available from: http://resolver.tudelft.nl/uuid:b65e68ed-933e-4f6c-9e4a-305c44166569


University of New Mexico

12. 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 September 18, 2020. http://hdl.handle.net/1928/12833.

MLA Handbook (7th Edition):

Carter, Melissa. “Effect of an aeroelastic film on confined subsonic cavity resonance.” 2011. Web. 18 Sep 2020.

Vancouver:

Carter M. Effect of an aeroelastic film on confined subsonic cavity resonance. [Internet] [Masters thesis]. University of New Mexico; 2011. [cited 2020 Sep 18]. 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


University of Minnesota

13. Gupta, Abhineet. Flight Dynamics Model of A Small Flexible Aircraft.

Degree: PhD, Aerospace Engineering and Mechanics, 2019, University of Minnesota

 The presence of aeroservoelastic effects in the flight dynamics of flexible aircraft presents significant challenges in terms of performance degradation and instability. In order to… (more)

Subjects/Keywords: Aeroelasticity; Flexible Aircraft; Flight Dynamics

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APA (6th Edition):

Gupta, A. (2019). Flight Dynamics Model of A Small Flexible Aircraft. (Doctoral Dissertation). University of Minnesota. Retrieved from http://hdl.handle.net/11299/211757

Chicago Manual of Style (16th Edition):

Gupta, Abhineet. “Flight Dynamics Model of A Small Flexible Aircraft.” 2019. Doctoral Dissertation, University of Minnesota. Accessed September 18, 2020. http://hdl.handle.net/11299/211757.

MLA Handbook (7th Edition):

Gupta, Abhineet. “Flight Dynamics Model of A Small Flexible Aircraft.” 2019. Web. 18 Sep 2020.

Vancouver:

Gupta A. Flight Dynamics Model of A Small Flexible Aircraft. [Internet] [Doctoral dissertation]. University of Minnesota; 2019. [cited 2020 Sep 18]. Available from: http://hdl.handle.net/11299/211757.

Council of Science Editors:

Gupta A. Flight Dynamics Model of A Small Flexible Aircraft. [Doctoral Dissertation]. University of Minnesota; 2019. Available from: http://hdl.handle.net/11299/211757


Texas A&M University

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

Degree: MS, Aerospace Engineering, 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. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-8039

Chicago Manual of Style (16th Edition):

Freno, Brian Andrew. “An Efficient Nonlinear Structural Dynamics Solver for Use in Computational Aeroelastic Analysis.” 2011. Masters Thesis, Texas A&M University. Accessed September 18, 2020. http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-8039.

MLA Handbook (7th Edition):

Freno, Brian Andrew. “An Efficient Nonlinear Structural Dynamics Solver for Use in Computational Aeroelastic Analysis.” 2011. Web. 18 Sep 2020.

Vancouver:

Freno BA. An Efficient Nonlinear Structural Dynamics Solver for Use in Computational Aeroelastic Analysis. [Internet] [Masters thesis]. Texas A&M University; 2011. [cited 2020 Sep 18]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-2010-05-8039.

Council of Science Editors:

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


University of Manchester

15. 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 September 18, 2020. 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. 18 Sep 2020.

Vancouver:

Miller SJ. Adaptive wing structures for aeroelastic drag reduction and loadsalleviation. [Internet] [Doctoral dissertation]. University of Manchester; 2011. [cited 2020 Sep 18]. 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

16. Szczyglowski, Christopher Patrick. Passive aeroelastic control in truss-braced wings using vibration suppression.

Degree: PhD, 2020, University of Bristol

 In recent years a significant effort has been devoted to the study of more energy efficient aircraft that will meet the environmental goals set out… (more)

Subjects/Keywords: aeroelasticity; vibration suppression; truss-braced wing; inerter

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APA (6th Edition):

Szczyglowski, C. P. (2020). Passive aeroelastic control in truss-braced wings using vibration suppression. (Doctoral Dissertation). University of Bristol. Retrieved from http://hdl.handle.net/1983/6ad0363f-1519-411e-aa97-bab798d53637

Chicago Manual of Style (16th Edition):

Szczyglowski, Christopher Patrick. “Passive aeroelastic control in truss-braced wings using vibration suppression.” 2020. Doctoral Dissertation, University of Bristol. Accessed September 18, 2020. http://hdl.handle.net/1983/6ad0363f-1519-411e-aa97-bab798d53637.

MLA Handbook (7th Edition):

Szczyglowski, Christopher Patrick. “Passive aeroelastic control in truss-braced wings using vibration suppression.” 2020. Web. 18 Sep 2020.

Vancouver:

Szczyglowski CP. Passive aeroelastic control in truss-braced wings using vibration suppression. [Internet] [Doctoral dissertation]. University of Bristol; 2020. [cited 2020 Sep 18]. Available from: http://hdl.handle.net/1983/6ad0363f-1519-411e-aa97-bab798d53637.

Council of Science Editors:

Szczyglowski CP. Passive aeroelastic control in truss-braced wings using vibration suppression. [Doctoral Dissertation]. University of Bristol; 2020. Available from: http://hdl.handle.net/1983/6ad0363f-1519-411e-aa97-bab798d53637


Texas A&M University

17. Long, Robert Raymond. Experiments on Dynamic Aeroelastic Response of Wind Turbine Blades.

Degree: PhD, Aerospace Engineering, 2017, Texas A&M University

 Wind turbine blades are growing progressively larger and lighter relative to their size, and these trends can lead to early failure due to fatigue. Effort… (more)

Subjects/Keywords: wind turbine; aeroelasticity; wind tunnel; experimental

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APA (6th Edition):

Long, R. R. (2017). Experiments on Dynamic Aeroelastic Response of Wind Turbine Blades. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/173080

Chicago Manual of Style (16th Edition):

Long, Robert Raymond. “Experiments on Dynamic Aeroelastic Response of Wind Turbine Blades.” 2017. Doctoral Dissertation, Texas A&M University. Accessed September 18, 2020. http://hdl.handle.net/1969.1/173080.

MLA Handbook (7th Edition):

Long, Robert Raymond. “Experiments on Dynamic Aeroelastic Response of Wind Turbine Blades.” 2017. Web. 18 Sep 2020.

Vancouver:

Long RR. Experiments on Dynamic Aeroelastic Response of Wind Turbine Blades. [Internet] [Doctoral dissertation]. Texas A&M University; 2017. [cited 2020 Sep 18]. Available from: http://hdl.handle.net/1969.1/173080.

Council of Science Editors:

Long RR. Experiments on Dynamic Aeroelastic Response of Wind Turbine Blades. [Doctoral Dissertation]. Texas A&M University; 2017. Available from: http://hdl.handle.net/1969.1/173080


Delft University of Technology

18. Prins, H.C. (author). Static Aeroelastic Scaling: Design of a static aeroelastically scaled strut-braced wing wind tunnel test model.

Degree: 2020, Delft University of Technology

 Classical aerodynamic wind tunnel tests are performed with stiff or rigid wind tunnel models. Over the years wing structures have become more flexible, and with… (more)

Subjects/Keywords: Aeroelasticity; Scaling; Composite Optimization; Wind tunnel testing

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APA (6th Edition):

Prins, H. C. (. (2020). Static Aeroelastic Scaling: Design of a static aeroelastically scaled strut-braced wing wind tunnel test model. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:13121f47-6481-405d-add7-0e110dacc0a4

Chicago Manual of Style (16th Edition):

Prins, H C (author). “Static Aeroelastic Scaling: Design of a static aeroelastically scaled strut-braced wing wind tunnel test model.” 2020. Masters Thesis, Delft University of Technology. Accessed September 18, 2020. http://resolver.tudelft.nl/uuid:13121f47-6481-405d-add7-0e110dacc0a4.

MLA Handbook (7th Edition):

Prins, H C (author). “Static Aeroelastic Scaling: Design of a static aeroelastically scaled strut-braced wing wind tunnel test model.” 2020. Web. 18 Sep 2020.

Vancouver:

Prins HC(. Static Aeroelastic Scaling: Design of a static aeroelastically scaled strut-braced wing wind tunnel test model. [Internet] [Masters thesis]. Delft University of Technology; 2020. [cited 2020 Sep 18]. Available from: http://resolver.tudelft.nl/uuid:13121f47-6481-405d-add7-0e110dacc0a4.

Council of Science Editors:

Prins HC(. Static Aeroelastic Scaling: Design of a static aeroelastically scaled strut-braced wing wind tunnel test model. [Masters Thesis]. Delft University of Technology; 2020. Available from: http://resolver.tudelft.nl/uuid:13121f47-6481-405d-add7-0e110dacc0a4


Delft University of Technology

19. Christison Gray, Alasdair (author). Geometrically Nonlinear High Fidelity Aerostructural Optimisation for Highly Flexible Wings.

Degree: 2020, Delft University of Technology

In the past decade, MDO researchers have developed capabilities to simultaneously optimise the shape and internal structure of aircraft based on coupled high fidelity Computational… (more)

Subjects/Keywords: MDO; Aeroelasticity; Aeroelastic tailoring; geometrically nonlinear structures

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APA (6th Edition):

Christison Gray, A. (. (2020). Geometrically Nonlinear High Fidelity Aerostructural Optimisation for Highly Flexible Wings. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:1a6b5001-d213-40d9-bc2c-5e831eda527d

Chicago Manual of Style (16th Edition):

Christison Gray, Alasdair (author). “Geometrically Nonlinear High Fidelity Aerostructural Optimisation for Highly Flexible Wings.” 2020. Masters Thesis, Delft University of Technology. Accessed September 18, 2020. http://resolver.tudelft.nl/uuid:1a6b5001-d213-40d9-bc2c-5e831eda527d.

MLA Handbook (7th Edition):

Christison Gray, Alasdair (author). “Geometrically Nonlinear High Fidelity Aerostructural Optimisation for Highly Flexible Wings.” 2020. Web. 18 Sep 2020.

Vancouver:

Christison Gray A(. Geometrically Nonlinear High Fidelity Aerostructural Optimisation for Highly Flexible Wings. [Internet] [Masters thesis]. Delft University of Technology; 2020. [cited 2020 Sep 18]. Available from: http://resolver.tudelft.nl/uuid:1a6b5001-d213-40d9-bc2c-5e831eda527d.

Council of Science Editors:

Christison Gray A(. Geometrically Nonlinear High Fidelity Aerostructural Optimisation for Highly Flexible Wings. [Masters Thesis]. Delft University of Technology; 2020. Available from: http://resolver.tudelft.nl/uuid:1a6b5001-d213-40d9-bc2c-5e831eda527d


University of Manchester

20. 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 September 18, 2020. 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. 18 Sep 2020.

Vancouver:

Miller SJ. Adaptive wing structures for aeroelastic drag reduction and loads alleviation. [Internet] [Doctoral dissertation]. University of Manchester; 2011. [cited 2020 Sep 18]. 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 Pretoria

21. Meijer, Marius-Corne. Development of an Aeroprediction Method for Slender Bodies Including Aeroelastic Effects Using Euler-Based Local Piston Theory.

Degree: PhD, Mechanical and Aeronautical Engineering, 2019, University of Pretoria

 Euler-based local piston theory (LPT) has received significant interest in recent literature. The method utilizes a simple, algebraic relation to predict between perturbation pressures directly… (more)

Subjects/Keywords: Aerodynamics; UCTD; Aeroelasticity

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APA (6th Edition):

Meijer, M. (2019). Development of an Aeroprediction Method for Slender Bodies Including Aeroelastic Effects Using Euler-Based Local Piston Theory. (Doctoral Dissertation). University of Pretoria. Retrieved from http://hdl.handle.net/2263/68727

Chicago Manual of Style (16th Edition):

Meijer, Marius-Corne. “Development of an Aeroprediction Method for Slender Bodies Including Aeroelastic Effects Using Euler-Based Local Piston Theory.” 2019. Doctoral Dissertation, University of Pretoria. Accessed September 18, 2020. http://hdl.handle.net/2263/68727.

MLA Handbook (7th Edition):

Meijer, Marius-Corne. “Development of an Aeroprediction Method for Slender Bodies Including Aeroelastic Effects Using Euler-Based Local Piston Theory.” 2019. Web. 18 Sep 2020.

Vancouver:

Meijer M. Development of an Aeroprediction Method for Slender Bodies Including Aeroelastic Effects Using Euler-Based Local Piston Theory. [Internet] [Doctoral dissertation]. University of Pretoria; 2019. [cited 2020 Sep 18]. Available from: http://hdl.handle.net/2263/68727.

Council of Science Editors:

Meijer M. Development of an Aeroprediction Method for Slender Bodies Including Aeroelastic Effects Using Euler-Based Local Piston Theory. [Doctoral Dissertation]. University of Pretoria; 2019. Available from: http://hdl.handle.net/2263/68727


Delft University of Technology

22. Kalthof, R.L.C. (author). 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 (author). “Multibody Dynamics Modeling of Flexible Aircraft Flight Dynamics.” 2014. Masters Thesis, Delft University of Technology. Accessed September 18, 2020. http://resolver.tudelft.nl/uuid:6aa1d6a0-0601-4595-97b3-047117fc6a97.

MLA Handbook (7th Edition):

Kalthof, R L C (author). “Multibody Dynamics Modeling of Flexible Aircraft Flight Dynamics.” 2014. Web. 18 Sep 2020.

Vancouver:

Kalthof RLC(. Multibody Dynamics Modeling of Flexible Aircraft Flight Dynamics. [Internet] [Masters thesis]. Delft University of Technology; 2014. [cited 2020 Sep 18]. 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


Delft University of Technology

23. Van Dooren, R.M. (author). The controllability of a winged hypersonic vehicle under aeroelastic effects.

Degree: 2016, Delft University of Technology

Aerospace Engineering

Space Engineering

Space Flight

Advisors/Committee Members: Mooij, E. (mentor).

Subjects/Keywords: Aeroelasticity; Controllability; hypersonic

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APA (6th Edition):

Van Dooren, R. M. (. (2016). The controllability of a winged hypersonic vehicle under aeroelastic effects. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:e8527460-df6c-4a08-838d-247566fa4c44

Chicago Manual of Style (16th Edition):

Van Dooren, R M (author). “The controllability of a winged hypersonic vehicle under aeroelastic effects.” 2016. Masters Thesis, Delft University of Technology. Accessed September 18, 2020. http://resolver.tudelft.nl/uuid:e8527460-df6c-4a08-838d-247566fa4c44.

MLA Handbook (7th Edition):

Van Dooren, R M (author). “The controllability of a winged hypersonic vehicle under aeroelastic effects.” 2016. Web. 18 Sep 2020.

Vancouver:

Van Dooren RM(. The controllability of a winged hypersonic vehicle under aeroelastic effects. [Internet] [Masters thesis]. Delft University of Technology; 2016. [cited 2020 Sep 18]. Available from: http://resolver.tudelft.nl/uuid:e8527460-df6c-4a08-838d-247566fa4c44.

Council of Science Editors:

Van Dooren RM(. The controllability of a winged hypersonic vehicle under aeroelastic effects. [Masters Thesis]. Delft University of Technology; 2016. Available from: http://resolver.tudelft.nl/uuid:e8527460-df6c-4a08-838d-247566fa4c44


Delft University of Technology

24. Anand, Himanshu (author). Nonlinear Aeroelastic Analysis of a High Aspect Ratio Wing in NASTRAN.

Degree: 2019, Delft University of Technology

Recent decades have seen the range of applications for aircraft expand to niches like weather monitoring, reconnaissance and satellite launch (Air Launch to Orbit, ALO).… (more)

Subjects/Keywords: Aeroelasticity; Geometric non-linear; high aspect ratio

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APA (6th Edition):

Anand, H. (. (2019). Nonlinear Aeroelastic Analysis of a High Aspect Ratio Wing in NASTRAN. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:e2e602da-857a-4786-855e-dfed3164bea8

Chicago Manual of Style (16th Edition):

Anand, Himanshu (author). “Nonlinear Aeroelastic Analysis of a High Aspect Ratio Wing in NASTRAN.” 2019. Masters Thesis, Delft University of Technology. Accessed September 18, 2020. http://resolver.tudelft.nl/uuid:e2e602da-857a-4786-855e-dfed3164bea8.

MLA Handbook (7th Edition):

Anand, Himanshu (author). “Nonlinear Aeroelastic Analysis of a High Aspect Ratio Wing in NASTRAN.” 2019. Web. 18 Sep 2020.

Vancouver:

Anand H(. Nonlinear Aeroelastic Analysis of a High Aspect Ratio Wing in NASTRAN. [Internet] [Masters thesis]. Delft University of Technology; 2019. [cited 2020 Sep 18]. Available from: http://resolver.tudelft.nl/uuid:e2e602da-857a-4786-855e-dfed3164bea8.

Council of Science Editors:

Anand H(. Nonlinear Aeroelastic Analysis of a High Aspect Ratio Wing in NASTRAN. [Masters Thesis]. Delft University of Technology; 2019. Available from: http://resolver.tudelft.nl/uuid:e2e602da-857a-4786-855e-dfed3164bea8


Delft University of Technology

25. Boatto, Umberto (author). A fluid-multibody coupling for aeroelastic applications to rotorcraft and wind turbines.

Degree: 2020, Delft University of Technology

 Accurate aerodynamic and aeroacoustic simulations of helicopters and wind turbines require the inclusion of the blade elasticity into the computational setup. If low-order aerodynamic models… (more)

Subjects/Keywords: Fluid Structure Interaction; Aeroelasticity; CFD; Unsteady Aerodynamics

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APA (6th Edition):

Boatto, U. (. (2020). A fluid-multibody coupling for aeroelastic applications to rotorcraft and wind turbines. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:170ea7f8-7c21-447b-93b5-e9a88112c4a3

Chicago Manual of Style (16th Edition):

Boatto, Umberto (author). “A fluid-multibody coupling for aeroelastic applications to rotorcraft and wind turbines.” 2020. Masters Thesis, Delft University of Technology. Accessed September 18, 2020. http://resolver.tudelft.nl/uuid:170ea7f8-7c21-447b-93b5-e9a88112c4a3.

MLA Handbook (7th Edition):

Boatto, Umberto (author). “A fluid-multibody coupling for aeroelastic applications to rotorcraft and wind turbines.” 2020. Web. 18 Sep 2020.

Vancouver:

Boatto U(. A fluid-multibody coupling for aeroelastic applications to rotorcraft and wind turbines. [Internet] [Masters thesis]. Delft University of Technology; 2020. [cited 2020 Sep 18]. Available from: http://resolver.tudelft.nl/uuid:170ea7f8-7c21-447b-93b5-e9a88112c4a3.

Council of Science Editors:

Boatto U(. A fluid-multibody coupling for aeroelastic applications to rotorcraft and wind turbines. [Masters Thesis]. Delft University of Technology; 2020. Available from: http://resolver.tudelft.nl/uuid:170ea7f8-7c21-447b-93b5-e9a88112c4a3


Delft University of Technology

26. Natella, M. (author). 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 (author). “Coupled Nonlinear Aeroelasticity and Flight Dynamics for Stability Analysis of Flexible Wing Structures.” 2015. Masters Thesis, Delft University of Technology. Accessed September 18, 2020. http://resolver.tudelft.nl/uuid:39984220-1d55-43fb-b42c-8a692a979211.

MLA Handbook (7th Edition):

Natella, M (author). “Coupled Nonlinear Aeroelasticity and Flight Dynamics for Stability Analysis of Flexible Wing Structures.” 2015. Web. 18 Sep 2020.

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 2020 Sep 18]. 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


University of Minnesota

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

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

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Alfifi, Salman. “An Experimental Study of Wing Flutter.” 2017. Doctoral Dissertation, University of Minnesota. Accessed September 18, 2020. http://hdl.handle.net/11299/206344.

MLA Handbook (7th Edition):

Alfifi, Salman. “An Experimental Study of Wing Flutter.” 2017. Web. 18 Sep 2020.

Vancouver:

Alfifi S. An Experimental Study of Wing Flutter. [Internet] [Doctoral dissertation]. University of Minnesota; 2017. [cited 2020 Sep 18]. Available from: http://hdl.handle.net/11299/206344.

Council of Science Editors:

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


Georgia Tech

28. 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 September 18, 2020. http://hdl.handle.net/1853/5037.

MLA Handbook (7th Edition):

Chae, Seungmook. “Effect of Follower Forces on Aeroelastic Stability of Flexible Structures.” 2004. Web. 18 Sep 2020.

Vancouver:

Chae S. Effect of Follower Forces on Aeroelastic Stability of Flexible Structures. [Internet] [Doctoral dissertation]. Georgia Tech; 2004. [cited 2020 Sep 18]. 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


Georgia Tech

29. Nagaraja, Kanivenahalli Sreenivasa. Analytical and experimental studies of a helicopter rotor in vertical flight.

Degree: PhD, Aerospace Engineering, 1975, Georgia Tech

Subjects/Keywords: Rotors (Helicopters); Aeroelasticity

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APA (6th Edition):

Nagaraja, K. S. (1975). Analytical and experimental studies of a helicopter rotor in vertical flight. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/12107

Chicago Manual of Style (16th Edition):

Nagaraja, Kanivenahalli Sreenivasa. “Analytical and experimental studies of a helicopter rotor in vertical flight.” 1975. Doctoral Dissertation, Georgia Tech. Accessed September 18, 2020. http://hdl.handle.net/1853/12107.

MLA Handbook (7th Edition):

Nagaraja, Kanivenahalli Sreenivasa. “Analytical and experimental studies of a helicopter rotor in vertical flight.” 1975. Web. 18 Sep 2020.

Vancouver:

Nagaraja KS. Analytical and experimental studies of a helicopter rotor in vertical flight. [Internet] [Doctoral dissertation]. Georgia Tech; 1975. [cited 2020 Sep 18]. Available from: http://hdl.handle.net/1853/12107.

Council of Science Editors:

Nagaraja KS. Analytical and experimental studies of a helicopter rotor in vertical flight. [Doctoral Dissertation]. Georgia Tech; 1975. Available from: http://hdl.handle.net/1853/12107


University of Florida

30. Armanious, George J. Distributed Control of a Flexible Air Vehicle Using an Adaptive Multi-Rate Distributed Kalman Filtering Framework.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2018, University of Florida

 In flexible aircraft, the structural dynamics and flight dynamics of the aircraft have the potential to couple. Controllers for these aircraft must be designed to… (more)

Subjects/Keywords: aeroelasticity  – controls  – distributed  – filter  – kalman  – multi-rate

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APA (6th Edition):

Armanious, G. J. (2018). Distributed Control of a Flexible Air Vehicle Using an Adaptive Multi-Rate Distributed Kalman Filtering Framework. (Doctoral Dissertation). University of Florida. Retrieved from https://ufdc.ufl.edu/UFE0051711

Chicago Manual of Style (16th Edition):

Armanious, George J. “Distributed Control of a Flexible Air Vehicle Using an Adaptive Multi-Rate Distributed Kalman Filtering Framework.” 2018. Doctoral Dissertation, University of Florida. Accessed September 18, 2020. https://ufdc.ufl.edu/UFE0051711.

MLA Handbook (7th Edition):

Armanious, George J. “Distributed Control of a Flexible Air Vehicle Using an Adaptive Multi-Rate Distributed Kalman Filtering Framework.” 2018. Web. 18 Sep 2020.

Vancouver:

Armanious GJ. Distributed Control of a Flexible Air Vehicle Using an Adaptive Multi-Rate Distributed Kalman Filtering Framework. [Internet] [Doctoral dissertation]. University of Florida; 2018. [cited 2020 Sep 18]. Available from: https://ufdc.ufl.edu/UFE0051711.

Council of Science Editors:

Armanious GJ. Distributed Control of a Flexible Air Vehicle Using an Adaptive Multi-Rate Distributed Kalman Filtering Framework. [Doctoral Dissertation]. University of Florida; 2018. Available from: https://ufdc.ufl.edu/UFE0051711

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