Advanced search options

Advanced Search Options 🞨

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

Find ETDs with:

in
/  
in
/  
in
/  
in

Written in Published in Earliest date Latest date

Sorted by

Results per page:

Sorted by: relevance · author · university · dateNew search

Dept: Aerospace Engineering

You searched for subject:( Coupling). Showing records 1 – 19 of 19 total matches.

Search Limiters

Last 2 Years | English Only

No search limiters apply to these results.

▼ Search Limiters


Georgia Tech

1. Haynes, Robert Andrew. Hygrothermally stable laminated composites with optimal coupling.

Degree: PhD, Aerospace Engineering, 2010, Georgia Tech

 This work begins by establishing the necessary and sufficient conditions for hygrothermal stability of composite laminates. An investigation is performed into the range of coupling(more)

Subjects/Keywords: Composite laminates; Hygrothermal stability; Extension-twist coupling; Bending-twist coupling; Optimization; Hygrothermoelasticity; Stability; Continuum mechanics

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Haynes, R. A. (2010). Hygrothermally stable laminated composites with optimal coupling. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/34671

Chicago Manual of Style (16th Edition):

Haynes, Robert Andrew. “Hygrothermally stable laminated composites with optimal coupling.” 2010. Doctoral Dissertation, Georgia Tech. Accessed March 18, 2019. http://hdl.handle.net/1853/34671.

MLA Handbook (7th Edition):

Haynes, Robert Andrew. “Hygrothermally stable laminated composites with optimal coupling.” 2010. Web. 18 Mar 2019.

Vancouver:

Haynes RA. Hygrothermally stable laminated composites with optimal coupling. [Internet] [Doctoral dissertation]. Georgia Tech; 2010. [cited 2019 Mar 18]. Available from: http://hdl.handle.net/1853/34671.

Council of Science Editors:

Haynes RA. Hygrothermally stable laminated composites with optimal coupling. [Doctoral Dissertation]. Georgia Tech; 2010. Available from: http://hdl.handle.net/1853/34671


Arizona State University

2. Larsson, Daniel. Dynamics, Modeling, Simulation and Control of Mid-Flight Coupling of Quadrotors.

Degree: Aerospace Engineering, 2016, Arizona State University

 Unmanned aerial vehicles have received increased attention in the last decade due to their versatility, as well as the availability of inexpensive sensors (e.g. GPS,… (more)

Subjects/Keywords: Aerospace engineering; Mechanical engineering; Control; Coupling; Dynamics; Quadrotors

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Larsson, D. (2016). Dynamics, Modeling, Simulation and Control of Mid-Flight Coupling of Quadrotors. (Masters Thesis). Arizona State University. Retrieved from http://repository.asu.edu/items/38761

Chicago Manual of Style (16th Edition):

Larsson, Daniel. “Dynamics, Modeling, Simulation and Control of Mid-Flight Coupling of Quadrotors.” 2016. Masters Thesis, Arizona State University. Accessed March 18, 2019. http://repository.asu.edu/items/38761.

MLA Handbook (7th Edition):

Larsson, Daniel. “Dynamics, Modeling, Simulation and Control of Mid-Flight Coupling of Quadrotors.” 2016. Web. 18 Mar 2019.

Vancouver:

Larsson D. Dynamics, Modeling, Simulation and Control of Mid-Flight Coupling of Quadrotors. [Internet] [Masters thesis]. Arizona State University; 2016. [cited 2019 Mar 18]. Available from: http://repository.asu.edu/items/38761.

Council of Science Editors:

Larsson D. Dynamics, Modeling, Simulation and Control of Mid-Flight Coupling of Quadrotors. [Masters Thesis]. Arizona State University; 2016. Available from: http://repository.asu.edu/items/38761

3. Doane, Stargel R. A Wind Tunnel Technique for the Identification of Ship Airwake/Rotor Downwash Coupling.

Degree: PhD, Aerospace Engineering, 2011, Old Dominion University

  A wind tunnel study is performed to analyze the interaction between ship airwakes and helicopter rotor downwash. This interaction is of interest to naval… (more)

Subjects/Keywords: Coupling; Interactions; Rotor downwash; Ship airwake; Wind tunnel; Aerospace Engineering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Doane, S. R. (2011). A Wind Tunnel Technique for the Identification of Ship Airwake/Rotor Downwash Coupling. (Doctoral Dissertation). Old Dominion University. Retrieved from 9781124973074 ; https://digitalcommons.odu.edu/mae_etds/56

Chicago Manual of Style (16th Edition):

Doane, Stargel R. “A Wind Tunnel Technique for the Identification of Ship Airwake/Rotor Downwash Coupling.” 2011. Doctoral Dissertation, Old Dominion University. Accessed March 18, 2019. 9781124973074 ; https://digitalcommons.odu.edu/mae_etds/56.

MLA Handbook (7th Edition):

Doane, Stargel R. “A Wind Tunnel Technique for the Identification of Ship Airwake/Rotor Downwash Coupling.” 2011. Web. 18 Mar 2019.

Vancouver:

Doane SR. A Wind Tunnel Technique for the Identification of Ship Airwake/Rotor Downwash Coupling. [Internet] [Doctoral dissertation]. Old Dominion University; 2011. [cited 2019 Mar 18]. Available from: 9781124973074 ; https://digitalcommons.odu.edu/mae_etds/56.

Council of Science Editors:

Doane SR. A Wind Tunnel Technique for the Identification of Ship Airwake/Rotor Downwash Coupling. [Doctoral Dissertation]. Old Dominion University; 2011. Available from: 9781124973074 ; https://digitalcommons.odu.edu/mae_etds/56


Cal Poly

4. Brown, John. A SPACE BASED PARTICLE DAMPER DEMONSTRATOR.

Degree: MS, Aerospace Engineering, 2011, Cal Poly

  The structure and payload of a CubeSat flight experiment that investigates the performance of particle dampers in a micro-gravity environment was designed, built, and… (more)

Subjects/Keywords: Harmonic Coupling; Space Qualified; Orbit; Phases of Design; Precision; Structures and Materials

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Brown, J. (2011). A SPACE BASED PARTICLE DAMPER DEMONSTRATOR. (Masters Thesis). Cal Poly. Retrieved from http://digitalcommons.calpoly.edu/theses/501 ; 10.15368/theses.2011.63

Chicago Manual of Style (16th Edition):

Brown, John. “A SPACE BASED PARTICLE DAMPER DEMONSTRATOR.” 2011. Masters Thesis, Cal Poly. Accessed March 18, 2019. http://digitalcommons.calpoly.edu/theses/501 ; 10.15368/theses.2011.63.

MLA Handbook (7th Edition):

Brown, John. “A SPACE BASED PARTICLE DAMPER DEMONSTRATOR.” 2011. Web. 18 Mar 2019.

Vancouver:

Brown J. A SPACE BASED PARTICLE DAMPER DEMONSTRATOR. [Internet] [Masters thesis]. Cal Poly; 2011. [cited 2019 Mar 18]. Available from: http://digitalcommons.calpoly.edu/theses/501 ; 10.15368/theses.2011.63.

Council of Science Editors:

Brown J. A SPACE BASED PARTICLE DAMPER DEMONSTRATOR. [Masters Thesis]. Cal Poly; 2011. Available from: http://digitalcommons.calpoly.edu/theses/501 ; 10.15368/theses.2011.63


Georgia Tech

5. Zaki, Afifa Adel. Using tightly-coupled CFD/CSD simulation for rotorcraft stability analysis.

Degree: PhD, Aerospace Engineering, 2012, Georgia Tech

 Dynamic stall deeply affects the response of helicopter rotor blades, making its modeling accuracy very important. Two commonly used dynamic stall models were implemented in… (more)

Subjects/Keywords: CFD/CSD coupling; Rotorcraft stability analysis; Rotors (Helicopters); Rotors (Helicopters) Aerodynamics; Aerodynamics

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Zaki, A. A. (2012). Using tightly-coupled CFD/CSD simulation for rotorcraft stability analysis. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/43579

Chicago Manual of Style (16th Edition):

Zaki, Afifa Adel. “Using tightly-coupled CFD/CSD simulation for rotorcraft stability analysis.” 2012. Doctoral Dissertation, Georgia Tech. Accessed March 18, 2019. http://hdl.handle.net/1853/43579.

MLA Handbook (7th Edition):

Zaki, Afifa Adel. “Using tightly-coupled CFD/CSD simulation for rotorcraft stability analysis.” 2012. Web. 18 Mar 2019.

Vancouver:

Zaki AA. Using tightly-coupled CFD/CSD simulation for rotorcraft stability analysis. [Internet] [Doctoral dissertation]. Georgia Tech; 2012. [cited 2019 Mar 18]. Available from: http://hdl.handle.net/1853/43579.

Council of Science Editors:

Zaki AA. Using tightly-coupled CFD/CSD simulation for rotorcraft stability analysis. [Doctoral Dissertation]. Georgia Tech; 2012. Available from: http://hdl.handle.net/1853/43579


Georgia Tech

6. Bopp, Matthew Scott. A time accurate fluid-structure interaction framework using a Cartesian grid CFD solver.

Degree: PhD, Aerospace Engineering, 2017, Georgia Tech

 The landing of the Mars Science Laboratory (MSL) in 2012 demonstrated the limits of supersonic planetary entry technology through the use of a disk-gap-band parachute… (more)

Subjects/Keywords: CFD; FSI; Cartesian; EDL; Aerodynamic decelerator; Fluid dynamics; Structural dynamics; Coupling; C++; Immersed boundary method

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Bopp, M. S. (2017). A time accurate fluid-structure interaction framework using a Cartesian grid CFD solver. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/59257

Chicago Manual of Style (16th Edition):

Bopp, Matthew Scott. “A time accurate fluid-structure interaction framework using a Cartesian grid CFD solver.” 2017. Doctoral Dissertation, Georgia Tech. Accessed March 18, 2019. http://hdl.handle.net/1853/59257.

MLA Handbook (7th Edition):

Bopp, Matthew Scott. “A time accurate fluid-structure interaction framework using a Cartesian grid CFD solver.” 2017. Web. 18 Mar 2019.

Vancouver:

Bopp MS. A time accurate fluid-structure interaction framework using a Cartesian grid CFD solver. [Internet] [Doctoral dissertation]. Georgia Tech; 2017. [cited 2019 Mar 18]. Available from: http://hdl.handle.net/1853/59257.

Council of Science Editors:

Bopp MS. A time accurate fluid-structure interaction framework using a Cartesian grid CFD solver. [Doctoral Dissertation]. Georgia Tech; 2017. Available from: http://hdl.handle.net/1853/59257


University of Kansas

7. Mendoza Strilchuk, Pedro. Structural-Electromagnetic Simulation Coupling and Conformal Antenna Design Tool.

Degree: MS, Aerospace Engineering, 2018, University of Kansas

 Airborne and spaceborne radar has long been an effective tool for remote sensing, surveillance, and reconnaissance. Most airborne systems utilize antenna arrays that are installed… (more)

Subjects/Keywords: Remote sensing; Aerospace engineering; antenna; B-splines; confromal; remote sensing; simulation coupling

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Mendoza Strilchuk, P. (2018). Structural-Electromagnetic Simulation Coupling and Conformal Antenna Design Tool. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/27597

Chicago Manual of Style (16th Edition):

Mendoza Strilchuk, Pedro. “Structural-Electromagnetic Simulation Coupling and Conformal Antenna Design Tool.” 2018. Masters Thesis, University of Kansas. Accessed March 18, 2019. http://hdl.handle.net/1808/27597.

MLA Handbook (7th Edition):

Mendoza Strilchuk, Pedro. “Structural-Electromagnetic Simulation Coupling and Conformal Antenna Design Tool.” 2018. Web. 18 Mar 2019.

Vancouver:

Mendoza Strilchuk P. Structural-Electromagnetic Simulation Coupling and Conformal Antenna Design Tool. [Internet] [Masters thesis]. University of Kansas; 2018. [cited 2019 Mar 18]. Available from: http://hdl.handle.net/1808/27597.

Council of Science Editors:

Mendoza Strilchuk P. Structural-Electromagnetic Simulation Coupling and Conformal Antenna Design Tool. [Masters Thesis]. University of Kansas; 2018. Available from: http://hdl.handle.net/1808/27597


University of Illinois – Urbana-Champaign

8. Kroeker, Erik Ian. Magnetic attitude control of LAICE satellite with aerodynamic stabilization.

Degree: PhD, Aerospace Engineering, 2017, University of Illinois – Urbana-Champaign

 The Lower Atmosphere Ionosphere Coupling Experiment (LAICE) is a NanoSatellite which will be performing in-situ measurements of neutral and ion densities in the mesosphere, lower… (more)

Subjects/Keywords: CubeSat; NanoSatellite; Magnetic; Attitude; Determination; Control; Lower Atmosphere Ionosphere Coupling Experiment (LAICE)

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Kroeker, E. I. (2017). Magnetic attitude control of LAICE satellite with aerodynamic stabilization. (Doctoral Dissertation). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/97249

Chicago Manual of Style (16th Edition):

Kroeker, Erik Ian. “Magnetic attitude control of LAICE satellite with aerodynamic stabilization.” 2017. Doctoral Dissertation, University of Illinois – Urbana-Champaign. Accessed March 18, 2019. http://hdl.handle.net/2142/97249.

MLA Handbook (7th Edition):

Kroeker, Erik Ian. “Magnetic attitude control of LAICE satellite with aerodynamic stabilization.” 2017. Web. 18 Mar 2019.

Vancouver:

Kroeker EI. Magnetic attitude control of LAICE satellite with aerodynamic stabilization. [Internet] [Doctoral dissertation]. University of Illinois – Urbana-Champaign; 2017. [cited 2019 Mar 18]. Available from: http://hdl.handle.net/2142/97249.

Council of Science Editors:

Kroeker EI. Magnetic attitude control of LAICE satellite with aerodynamic stabilization. [Doctoral Dissertation]. University of Illinois – Urbana-Champaign; 2017. Available from: http://hdl.handle.net/2142/97249


Georgia Tech

9. Abras, Jennifer N. Enhancement of aeroelastic rotor airload prediction methods.

Degree: PhD, Aerospace Engineering, 2009, Georgia Tech

 The accurate prediction of rotor air loads is a current topic of interest in the rotorcraft community. The complex nature of this loading makes this… (more)

Subjects/Keywords: Coupling; CFD-CSD; Comprehensive code; Free wake; CFD; Rotor; Aeroelasticity; Rotors (Helicopters) Aerodynamics; Structural dynamics; Prediction theory

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Abras, J. N. (2009). Enhancement of aeroelastic rotor airload prediction methods. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/28182

Chicago Manual of Style (16th Edition):

Abras, Jennifer N. “Enhancement of aeroelastic rotor airload prediction methods.” 2009. Doctoral Dissertation, Georgia Tech. Accessed March 18, 2019. http://hdl.handle.net/1853/28182.

MLA Handbook (7th Edition):

Abras, Jennifer N. “Enhancement of aeroelastic rotor airload prediction methods.” 2009. Web. 18 Mar 2019.

Vancouver:

Abras JN. Enhancement of aeroelastic rotor airload prediction methods. [Internet] [Doctoral dissertation]. Georgia Tech; 2009. [cited 2019 Mar 18]. Available from: http://hdl.handle.net/1853/28182.

Council of Science Editors:

Abras JN. Enhancement of aeroelastic rotor airload prediction methods. [Doctoral Dissertation]. Georgia Tech; 2009. Available from: http://hdl.handle.net/1853/28182


UCLA

10. Tran, Phuoc Hai Nguyen. Acoustically Coupled Droplet Combustion and Local Extinction under High Amplitude Excitation.

Degree: Aerospace Engineering, 2014, UCLA

 The present experimental study examined the characteristics of liquid ethanol fuel droplet combustion in the presence of high amplitude acoustic excitation, with focus on conditions… (more)

Subjects/Keywords: Aerospace engineering; Acoustics; Engineering; alternative fuels; droplet combustion; high amplitude acoustic excitation; OH* chemiluminescence; partial extinction; thermoacoustic coupling

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Tran, P. H. N. (2014). Acoustically Coupled Droplet Combustion and Local Extinction under High Amplitude Excitation. (Thesis). UCLA. Retrieved from http://www.escholarship.org/uc/item/125455dw

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):

Tran, Phuoc Hai Nguyen. “Acoustically Coupled Droplet Combustion and Local Extinction under High Amplitude Excitation.” 2014. Thesis, UCLA. Accessed March 18, 2019. http://www.escholarship.org/uc/item/125455dw.

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

MLA Handbook (7th Edition):

Tran, Phuoc Hai Nguyen. “Acoustically Coupled Droplet Combustion and Local Extinction under High Amplitude Excitation.” 2014. Web. 18 Mar 2019.

Vancouver:

Tran PHN. Acoustically Coupled Droplet Combustion and Local Extinction under High Amplitude Excitation. [Internet] [Thesis]. UCLA; 2014. [cited 2019 Mar 18]. Available from: http://www.escholarship.org/uc/item/125455dw.

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

Council of Science Editors:

Tran PHN. Acoustically Coupled Droplet Combustion and Local Extinction under High Amplitude Excitation. [Thesis]. UCLA; 2014. Available from: http://www.escholarship.org/uc/item/125455dw

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


Georgia Tech

11. Cook, James Richard. Development of an aeroelastic methodology for surface morphing rotors.

Degree: PhD, Aerospace Engineering, 2014, Georgia Tech

 A Computational Fluid Dynamics/Computational Fluid Dynamics (CFD/CSD) coupling interface was developed to obtain aeroelastic solutions of a morphing rotor. The methodology was implemented in Fully… (more)

Subjects/Keywords: Aeroelasticity; Test facility; Recirculation; Turbulence model; Hrles; Rotorcraft; Rotor; CFD/CSD; Coupling; CFD; Camber; Actuation; Morphing; Rotors; Aeroelasticity; Structural dynamics; Computational fluid dynamics

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Cook, J. R. (2014). Development of an aeroelastic methodology for surface morphing rotors. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/51807

Chicago Manual of Style (16th Edition):

Cook, James Richard. “Development of an aeroelastic methodology for surface morphing rotors.” 2014. Doctoral Dissertation, Georgia Tech. Accessed March 18, 2019. http://hdl.handle.net/1853/51807.

MLA Handbook (7th Edition):

Cook, James Richard. “Development of an aeroelastic methodology for surface morphing rotors.” 2014. Web. 18 Mar 2019.

Vancouver:

Cook JR. Development of an aeroelastic methodology for surface morphing rotors. [Internet] [Doctoral dissertation]. Georgia Tech; 2014. [cited 2019 Mar 18]. Available from: http://hdl.handle.net/1853/51807.

Council of Science Editors:

Cook JR. Development of an aeroelastic methodology for surface morphing rotors. [Doctoral Dissertation]. Georgia Tech; 2014. Available from: http://hdl.handle.net/1853/51807


Georgia Tech

12. Min, Byung-Young. A physics based investigation of gurney flaps for enhancement of rotorcraft flight characteristics.

Degree: PhD, Aerospace Engineering, 2010, Georgia Tech

 Helicopters are versatile vehicles that can vertically take off and land, hover, and perform maneuver at very low forward speeds. These characteristics make them unique… (more)

Subjects/Keywords: On-Board Control (OBC); Active control; CFD-CSD coupling; BVI; Vibration reduction; Autorotation; Gurney flap; Rotorcraft; Hybrid Navier-Stokes/Free wake method; Rotors Vibration; Aerofoils; Rotors (Helicopters)

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Min, B. (2010). A physics based investigation of gurney flaps for enhancement of rotorcraft flight characteristics. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/33851

Chicago Manual of Style (16th Edition):

Min, Byung-Young. “A physics based investigation of gurney flaps for enhancement of rotorcraft flight characteristics.” 2010. Doctoral Dissertation, Georgia Tech. Accessed March 18, 2019. http://hdl.handle.net/1853/33851.

MLA Handbook (7th Edition):

Min, Byung-Young. “A physics based investigation of gurney flaps for enhancement of rotorcraft flight characteristics.” 2010. Web. 18 Mar 2019.

Vancouver:

Min B. A physics based investigation of gurney flaps for enhancement of rotorcraft flight characteristics. [Internet] [Doctoral dissertation]. Georgia Tech; 2010. [cited 2019 Mar 18]. Available from: http://hdl.handle.net/1853/33851.

Council of Science Editors:

Min B. A physics based investigation of gurney flaps for enhancement of rotorcraft flight characteristics. [Doctoral Dissertation]. Georgia Tech; 2010. Available from: http://hdl.handle.net/1853/33851

13. Reveles, Nicolas. Advanced methods for dynamic aeroelastic analysis of rotors.

Degree: PhD, Aerospace Engineering, 2014, Georgia Tech

 Simulations play an integral role in the understanding and development of rotor- craft aeromechanics. Computational Fluid Dynamics coupled with Computational Structural Dynamics (CFD/CSD) offers an… (more)

Subjects/Keywords: Aeroelasticity; Tight coupling; Loose coupling; CFD/CSD; Hybrid; Free-wake; URANS; Trim; Aeroelasticity; Rotors; Computational fluid dynamics; Structural dynamics

…LIST OF FIGURES 1 A generic diagram of tight coupling iterations and data transfer… …coupling trim of the UH-60A C8534 case. . . . . . . . . . . . . . . . . 44 13 Trimming of the… …UH-60A C8534 case in tight coupling from a cold start. . . 45 14 Revolutions needed to… …reach thrust convergence (1% error) based on loose coupling initialization… …49 Trim of UH-60A C8534 using using the optimal trim procedure for tight coupling results… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Reveles, N. (2014). Advanced methods for dynamic aeroelastic analysis of rotors. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/51904

Chicago Manual of Style (16th Edition):

Reveles, Nicolas. “Advanced methods for dynamic aeroelastic analysis of rotors.” 2014. Doctoral Dissertation, Georgia Tech. Accessed March 18, 2019. http://hdl.handle.net/1853/51904.

MLA Handbook (7th Edition):

Reveles, Nicolas. “Advanced methods for dynamic aeroelastic analysis of rotors.” 2014. Web. 18 Mar 2019.

Vancouver:

Reveles N. Advanced methods for dynamic aeroelastic analysis of rotors. [Internet] [Doctoral dissertation]. Georgia Tech; 2014. [cited 2019 Mar 18]. Available from: http://hdl.handle.net/1853/51904.

Council of Science Editors:

Reveles N. Advanced methods for dynamic aeroelastic analysis of rotors. [Doctoral Dissertation]. Georgia Tech; 2014. Available from: http://hdl.handle.net/1853/51904


Penn State University

14. Howard, Anna Kathleen Tyler. The Aeromechanical Stability of Soft-Inplane Tiltrotors.

Degree: PhD, Aerospace Engineering, 2001, Penn State University

 A soft-inplane tiltrotor can be subject to the aeromechanical instabilities of ground and air resonance in addition to whirl flutter. While whirl flutter has been… (more)

Subjects/Keywords: full-span; whirl flutter; semi-span; civil tiltrotor; aeromechanical stability; rotorcraft; helicopter; pitch-lag coupling; ground resonance; pitch-flap coupling; air resonance; aeroelastic couplings; stability; tiltrotor

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Howard, A. K. T. (2001). The Aeromechanical Stability of Soft-Inplane Tiltrotors. (Doctoral Dissertation). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/5861

Chicago Manual of Style (16th Edition):

Howard, Anna Kathleen Tyler. “The Aeromechanical Stability of Soft-Inplane Tiltrotors.” 2001. Doctoral Dissertation, Penn State University. Accessed March 18, 2019. https://etda.libraries.psu.edu/catalog/5861.

MLA Handbook (7th Edition):

Howard, Anna Kathleen Tyler. “The Aeromechanical Stability of Soft-Inplane Tiltrotors.” 2001. Web. 18 Mar 2019.

Vancouver:

Howard AKT. The Aeromechanical Stability of Soft-Inplane Tiltrotors. [Internet] [Doctoral dissertation]. Penn State University; 2001. [cited 2019 Mar 18]. Available from: https://etda.libraries.psu.edu/catalog/5861.

Council of Science Editors:

Howard AKT. The Aeromechanical Stability of Soft-Inplane Tiltrotors. [Doctoral Dissertation]. Penn State University; 2001. Available from: https://etda.libraries.psu.edu/catalog/5861


Georgia Tech

15. Ozbay, Serkan. Extension-Twist Coupling Optimization in Composite Rotor Blades.

Degree: PhD, Aerospace Engineering, 2005, Georgia Tech

 For optimal rotor performance in a tiltrotor aircraft the difference in the inflow and the rotor speeds between the hover and cruise flight modes suggests… (more)

Subjects/Keywords: Composite rotor blades; Elastic tailoring; Extension-twist coupling; Structural optimization; Rotors Dynamics; Rotors (Helicopters) Aerodynamics

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Ozbay, S. (2005). Extension-Twist Coupling Optimization in Composite Rotor Blades. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/10422

Chicago Manual of Style (16th Edition):

Ozbay, Serkan. “Extension-Twist Coupling Optimization in Composite Rotor Blades.” 2005. Doctoral Dissertation, Georgia Tech. Accessed March 18, 2019. http://hdl.handle.net/1853/10422.

MLA Handbook (7th Edition):

Ozbay, Serkan. “Extension-Twist Coupling Optimization in Composite Rotor Blades.” 2005. Web. 18 Mar 2019.

Vancouver:

Ozbay S. Extension-Twist Coupling Optimization in Composite Rotor Blades. [Internet] [Doctoral dissertation]. Georgia Tech; 2005. [cited 2019 Mar 18]. Available from: http://hdl.handle.net/1853/10422.

Council of Science Editors:

Ozbay S. Extension-Twist Coupling Optimization in Composite Rotor Blades. [Doctoral Dissertation]. Georgia Tech; 2005. Available from: http://hdl.handle.net/1853/10422


University of Michigan

16. Chimakurthi, Satish Kumar. A Computational Aeroelasticity Framework for Analyzing Flapping Wings.

Degree: PhD, Aerospace Engineering, 2009, University of Michigan

 Flexible flapping wings have garnered a large amount of attention within the micro aerial vehicle (MAV) community: a critical component of MAV flight is the… (more)

Subjects/Keywords: Aeroelasticity of Flapping Wings; Micro Air Vehicles; Fluid-Structure Interaction; Partitioned Solution; MAV; Fluid-Structure Coupling; Aerospace Engineering; Mechanical Engineering; Engineering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Chimakurthi, S. K. (2009). A Computational Aeroelasticity Framework for Analyzing Flapping Wings. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/64707

Chicago Manual of Style (16th Edition):

Chimakurthi, Satish Kumar. “A Computational Aeroelasticity Framework for Analyzing Flapping Wings.” 2009. Doctoral Dissertation, University of Michigan. Accessed March 18, 2019. http://hdl.handle.net/2027.42/64707.

MLA Handbook (7th Edition):

Chimakurthi, Satish Kumar. “A Computational Aeroelasticity Framework for Analyzing Flapping Wings.” 2009. Web. 18 Mar 2019.

Vancouver:

Chimakurthi SK. A Computational Aeroelasticity Framework for Analyzing Flapping Wings. [Internet] [Doctoral dissertation]. University of Michigan; 2009. [cited 2019 Mar 18]. Available from: http://hdl.handle.net/2027.42/64707.

Council of Science Editors:

Chimakurthi SK. A Computational Aeroelasticity Framework for Analyzing Flapping Wings. [Doctoral Dissertation]. University of Michigan; 2009. Available from: http://hdl.handle.net/2027.42/64707


University of Southern California

17. Gilpin, Matthew R. High temperature latent heat thermal energy storage to augment solar thermal propulsion for microsatellites.

Degree: PhD, Aerospace Engineering, 2015, University of Southern California

 Solar thermal propulsion (STP) offers an unique combination of thrust and efficiency, providing greater total ΔV capability than chemical propulsion systems without the order of… (more)

Subjects/Keywords: solar thermal; latent heat; thermal energy storage; microsatellites; spacecraft propulsion; advanced propulsion; thermal rocket; molten silicon; liquid silicon; solar furnace; solar concentration; phase change material; molten boron; liquid boron; radiation shielding model; convective coupling; thermal battery; thermal capacitor

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Gilpin, M. R. (2015). High temperature latent heat thermal energy storage to augment solar thermal propulsion for microsatellites. (Doctoral Dissertation). University of Southern California. Retrieved from http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll3/id/600904/rec/3175

Chicago Manual of Style (16th Edition):

Gilpin, Matthew R. “High temperature latent heat thermal energy storage to augment solar thermal propulsion for microsatellites.” 2015. Doctoral Dissertation, University of Southern California. Accessed March 18, 2019. http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll3/id/600904/rec/3175.

MLA Handbook (7th Edition):

Gilpin, Matthew R. “High temperature latent heat thermal energy storage to augment solar thermal propulsion for microsatellites.” 2015. Web. 18 Mar 2019.

Vancouver:

Gilpin MR. High temperature latent heat thermal energy storage to augment solar thermal propulsion for microsatellites. [Internet] [Doctoral dissertation]. University of Southern California; 2015. [cited 2019 Mar 18]. Available from: http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll3/id/600904/rec/3175.

Council of Science Editors:

Gilpin MR. High temperature latent heat thermal energy storage to augment solar thermal propulsion for microsatellites. [Doctoral Dissertation]. University of Southern California; 2015. Available from: http://digitallibrary.usc.edu/cdm/compoundobject/collection/p15799coll3/id/600904/rec/3175

18. Sevilla Esparza, Cristhian Israel. Oscillatory Flame Response in Acoustically Coupled Fuel Droplet Combustion.

Degree: Aerospace Engineering, 2013, UCLA

 This experimental study focuses on combustion of liquid fuel droplets subject to external acoustic disturbances in the form of standing waves within an acoustic waveguide.… (more)

Subjects/Keywords: Aerospace engineering; Mechanical engineering; Acoustics; Acoustic Coupling; Combustion Instability; Diffusion Flame; Droplet Combustion; Rayleigh Criterion; Standing Acoustic Wave

…generation. Coupling of large acoustic fluctuations with multiphase combustion in the case of LREs… …oscillation, especially the coupling of heat release and pressure perturbations [1, 2]… …phenomena impacting LREs, such as the POGO instability generated through closed loop coupling of… …concept of the coupling between acoustic disturbances and specific combustion regimes present in… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Sevilla Esparza, C. I. (2013). Oscillatory Flame Response in Acoustically Coupled Fuel Droplet Combustion. (Thesis). UCLA. Retrieved from http://www.escholarship.org/uc/item/9hr0m3k0

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):

Sevilla Esparza, Cristhian Israel. “Oscillatory Flame Response in Acoustically Coupled Fuel Droplet Combustion.” 2013. Thesis, UCLA. Accessed March 18, 2019. http://www.escholarship.org/uc/item/9hr0m3k0.

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

MLA Handbook (7th Edition):

Sevilla Esparza, Cristhian Israel. “Oscillatory Flame Response in Acoustically Coupled Fuel Droplet Combustion.” 2013. Web. 18 Mar 2019.

Vancouver:

Sevilla Esparza CI. Oscillatory Flame Response in Acoustically Coupled Fuel Droplet Combustion. [Internet] [Thesis]. UCLA; 2013. [cited 2019 Mar 18]. Available from: http://www.escholarship.org/uc/item/9hr0m3k0.

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

Council of Science Editors:

Sevilla Esparza CI. Oscillatory Flame Response in Acoustically Coupled Fuel Droplet Combustion. [Thesis]. UCLA; 2013. Available from: http://www.escholarship.org/uc/item/9hr0m3k0

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

19. Tiwari, Chandrashekhar. Innovative Energy Absorbing Devices Based on Composite Tubes.

Degree: PhD, Aerospace Engineering, 2012, Penn State University

 Analytical and experimental study of innovative load limiting and energy absorbing devices are presented here. The devices are based on composite tubes and can be… (more)

Subjects/Keywords: Energy Absorbing; Extension Twist Coupling; Crush Tubes; Sandwich Core Device; Non-linear Model; Rate Effects; Foam Model

…17 Figure 1-18: Extension-twist coupling in an anti-symmetric laminate (left) and… …tailored to result in beneficial elastic couplings. Extension-twist coupling is one such… …characteristic and is explained in the section below. Extension-twist coupling When a composite anti… …characteristic non-classical behavior exhibited by composites is named extension-twist coupling… …Figure 1-18: Extension-twist coupling in an anti-symmetric laminate (left) and in a… 

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Tiwari, C. (2012). Innovative Energy Absorbing Devices Based on Composite Tubes. (Doctoral Dissertation). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/15542

Chicago Manual of Style (16th Edition):

Tiwari, Chandrashekhar. “Innovative Energy Absorbing Devices Based on Composite Tubes.” 2012. Doctoral Dissertation, Penn State University. Accessed March 18, 2019. https://etda.libraries.psu.edu/catalog/15542.

MLA Handbook (7th Edition):

Tiwari, Chandrashekhar. “Innovative Energy Absorbing Devices Based on Composite Tubes.” 2012. Web. 18 Mar 2019.

Vancouver:

Tiwari C. Innovative Energy Absorbing Devices Based on Composite Tubes. [Internet] [Doctoral dissertation]. Penn State University; 2012. [cited 2019 Mar 18]. Available from: https://etda.libraries.psu.edu/catalog/15542.

Council of Science Editors:

Tiwari C. Innovative Energy Absorbing Devices Based on Composite Tubes. [Doctoral Dissertation]. Penn State University; 2012. Available from: https://etda.libraries.psu.edu/catalog/15542

.