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You searched for +publisher:"Old Dominion University" +contributor:("Drew Landman"). Showing records 1 – 29 of 29 total matches.

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1. 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

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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 November 22, 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. 22 Nov 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 Nov 22]. 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

2. Chen, Mau-Kuo. Use of a Rolling Road System in Crosswind Conditions.

Degree: PhD, Aerospace Engineering, 2013, Old Dominion University

  Wind tunnel testing continues to play an important role in vehicle aerodynamic development. Accurate results are strongly associated with whether the wind tunnel can… (more)

Subjects/Keywords: Aerodynamics; Crosswind conditions; Rolling road system; Wind tunnel testing; Aerodynamics and Fluid Mechanics; Aerospace Engineering; Automotive Engineering

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APA (6th Edition):

Chen, M. (2013). Use of a Rolling Road System in Crosswind Conditions. (Doctoral Dissertation). Old Dominion University. Retrieved from 9781303512575 ; https://digitalcommons.odu.edu/mae_etds/126

Chicago Manual of Style (16th Edition):

Chen, Mau-Kuo. “Use of a Rolling Road System in Crosswind Conditions.” 2013. Doctoral Dissertation, Old Dominion University. Accessed November 22, 2019. 9781303512575 ; https://digitalcommons.odu.edu/mae_etds/126.

MLA Handbook (7th Edition):

Chen, Mau-Kuo. “Use of a Rolling Road System in Crosswind Conditions.” 2013. Web. 22 Nov 2019.

Vancouver:

Chen M. Use of a Rolling Road System in Crosswind Conditions. [Internet] [Doctoral dissertation]. Old Dominion University; 2013. [cited 2019 Nov 22]. Available from: 9781303512575 ; https://digitalcommons.odu.edu/mae_etds/126.

Council of Science Editors:

Chen M. Use of a Rolling Road System in Crosswind Conditions. [Doctoral Dissertation]. Old Dominion University; 2013. Available from: 9781303512575 ; https://digitalcommons.odu.edu/mae_etds/126

3. Toro, Kenneth G. Uncertainty Estimates and Prediction Interval Development for Internal Strain Gage Balance Calibration Systems.

Degree: PhD, Aerospace Engineering, 2015, Old Dominion University

  Currently, there is a lack of the use of mathematically rigorous methods to evaluate the performance of multivariate force measurement systems. The specific problem… (more)

Subjects/Keywords: Force measurement; Strain gage balances; Uncertainty; Aerospace Engineering

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APA (6th Edition):

Toro, K. G. (2015). Uncertainty Estimates and Prediction Interval Development for Internal Strain Gage Balance Calibration Systems. (Doctoral Dissertation). Old Dominion University. Retrieved from 9781339868073 ; https://digitalcommons.odu.edu/mae_etds/163

Chicago Manual of Style (16th Edition):

Toro, Kenneth G. “Uncertainty Estimates and Prediction Interval Development for Internal Strain Gage Balance Calibration Systems.” 2015. Doctoral Dissertation, Old Dominion University. Accessed November 22, 2019. 9781339868073 ; https://digitalcommons.odu.edu/mae_etds/163.

MLA Handbook (7th Edition):

Toro, Kenneth G. “Uncertainty Estimates and Prediction Interval Development for Internal Strain Gage Balance Calibration Systems.” 2015. Web. 22 Nov 2019.

Vancouver:

Toro KG. Uncertainty Estimates and Prediction Interval Development for Internal Strain Gage Balance Calibration Systems. [Internet] [Doctoral dissertation]. Old Dominion University; 2015. [cited 2019 Nov 22]. Available from: 9781339868073 ; https://digitalcommons.odu.edu/mae_etds/163.

Council of Science Editors:

Toro KG. Uncertainty Estimates and Prediction Interval Development for Internal Strain Gage Balance Calibration Systems. [Doctoral Dissertation]. Old Dominion University; 2015. Available from: 9781339868073 ; https://digitalcommons.odu.edu/mae_etds/163

4. Zhang, Mingkan. Electrokinetic Transport Phenomena in Nanofluidic Devices.

Degree: PhD, Aerospace Engineering, 2012, Old Dominion University

  Nanofluidic devices have wide potential applications in biology, chemistry and medicine, and have been proven to be very valuable in sensing biological particles (e.g.,… (more)

Subjects/Keywords: DNA sequencing; Electrokinetic transport; Nanofluidic devices; Translocation; Biomechanics and Biotransport; Biomedical Engineering and Bioengineering; Mechanical Engineering

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APA (6th Edition):

Zhang, M. (2012). Electrokinetic Transport Phenomena in Nanofluidic Devices. (Doctoral Dissertation). Old Dominion University. Retrieved from 9781267395955 ; https://digitalcommons.odu.edu/mae_etds/165

Chicago Manual of Style (16th Edition):

Zhang, Mingkan. “Electrokinetic Transport Phenomena in Nanofluidic Devices.” 2012. Doctoral Dissertation, Old Dominion University. Accessed November 22, 2019. 9781267395955 ; https://digitalcommons.odu.edu/mae_etds/165.

MLA Handbook (7th Edition):

Zhang, Mingkan. “Electrokinetic Transport Phenomena in Nanofluidic Devices.” 2012. Web. 22 Nov 2019.

Vancouver:

Zhang M. Electrokinetic Transport Phenomena in Nanofluidic Devices. [Internet] [Doctoral dissertation]. Old Dominion University; 2012. [cited 2019 Nov 22]. Available from: 9781267395955 ; https://digitalcommons.odu.edu/mae_etds/165.

Council of Science Editors:

Zhang M. Electrokinetic Transport Phenomena in Nanofluidic Devices. [Doctoral Dissertation]. Old Dominion University; 2012. Available from: 9781267395955 ; https://digitalcommons.odu.edu/mae_etds/165

5. Ely, Jeffry William. Experimental Investigation of Turbulent Structures and Non-Equilibrium Effects in Axial Wake Vortices Via Particle Image Velocimetry.

Degree: MS, Aerospace Engineering, 2016, Old Dominion University

  Vortices are a common phenomenon in fluid flows that arise as kinetic energy dissipates into heat via viscous interaction. They arise naturally at large… (more)

Subjects/Keywords: Non-equilibrium; Particle image velocimetry (PIV); Turbulent structures; Vortex; Vortices; Aerospace Engineering; Mechanical Engineering

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APA (6th Edition):

Ely, J. W. (2016). Experimental Investigation of Turbulent Structures and Non-Equilibrium Effects in Axial Wake Vortices Via Particle Image Velocimetry. (Thesis). Old Dominion University. Retrieved from 9781339787848 ; https://digitalcommons.odu.edu/mae_etds/9

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):

Ely, Jeffry William. “Experimental Investigation of Turbulent Structures and Non-Equilibrium Effects in Axial Wake Vortices Via Particle Image Velocimetry.” 2016. Thesis, Old Dominion University. Accessed November 22, 2019. 9781339787848 ; https://digitalcommons.odu.edu/mae_etds/9.

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

MLA Handbook (7th Edition):

Ely, Jeffry William. “Experimental Investigation of Turbulent Structures and Non-Equilibrium Effects in Axial Wake Vortices Via Particle Image Velocimetry.” 2016. Web. 22 Nov 2019.

Vancouver:

Ely JW. Experimental Investigation of Turbulent Structures and Non-Equilibrium Effects in Axial Wake Vortices Via Particle Image Velocimetry. [Internet] [Thesis]. Old Dominion University; 2016. [cited 2019 Nov 22]. Available from: 9781339787848 ; https://digitalcommons.odu.edu/mae_etds/9.

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

Council of Science Editors:

Ely JW. Experimental Investigation of Turbulent Structures and Non-Equilibrium Effects in Axial Wake Vortices Via Particle Image Velocimetry. [Thesis]. Old Dominion University; 2016. Available from: 9781339787848 ; https://digitalcommons.odu.edu/mae_etds/9

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

6. Duvall, Brian Edward. Development and Implementation of a Propeller Test Capability for Gl-10 "Greased Lightning" Propeller Design.

Degree: MS, Aerospace Engineering, 2016, Old Dominion University

  Interest in small unmanned aerial vehicles has increased dramatically in recent years. Hybrid vehicles which allow forward flight as a fixed wing aircraft and… (more)

Subjects/Keywords: Acoustic; Performance; Propeller; Aerospace Engineering

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APA (6th Edition):

Duvall, B. E. (2016). Development and Implementation of a Propeller Test Capability for Gl-10 "Greased Lightning" Propeller Design. (Thesis). Old Dominion University. Retrieved from 9781369183771 ; https://digitalcommons.odu.edu/mae_etds/12

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):

Duvall, Brian Edward. “Development and Implementation of a Propeller Test Capability for Gl-10 "Greased Lightning" Propeller Design.” 2016. Thesis, Old Dominion University. Accessed November 22, 2019. 9781369183771 ; https://digitalcommons.odu.edu/mae_etds/12.

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

MLA Handbook (7th Edition):

Duvall, Brian Edward. “Development and Implementation of a Propeller Test Capability for Gl-10 "Greased Lightning" Propeller Design.” 2016. Web. 22 Nov 2019.

Vancouver:

Duvall BE. Development and Implementation of a Propeller Test Capability for Gl-10 "Greased Lightning" Propeller Design. [Internet] [Thesis]. Old Dominion University; 2016. [cited 2019 Nov 22]. Available from: 9781369183771 ; https://digitalcommons.odu.edu/mae_etds/12.

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

Council of Science Editors:

Duvall BE. Development and Implementation of a Propeller Test Capability for Gl-10 "Greased Lightning" Propeller Design. [Thesis]. Old Dominion University; 2016. Available from: 9781369183771 ; https://digitalcommons.odu.edu/mae_etds/12

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

7. Lear, Donald Joseph. Development of a Data Acquisition System for Unmanned Aerial Vehicle (UAV) System Identification.

Degree: MS, Mechanical & Aerospace Engineering, 2017, Old Dominion University

  Aircraft system identification techniques are developed for fixed wing Unmanned Aerial Vehicles (UAV). The use of a designed flight experiment with measured system inputs/outputs… (more)

Subjects/Keywords: Design of experiments; Firmware; PX4; Response surface methodology; UAS; Umanned aerial system; Aerospace Engineering; Applied Mechanics; Computer Engineering

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APA (6th Edition):

Lear, D. J. (2017). Development of a Data Acquisition System for Unmanned Aerial Vehicle (UAV) System Identification. (Thesis). Old Dominion University. Retrieved from 9780355621259 ; https://digitalcommons.odu.edu/mae_etds/30

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):

Lear, Donald Joseph. “Development of a Data Acquisition System for Unmanned Aerial Vehicle (UAV) System Identification.” 2017. Thesis, Old Dominion University. Accessed November 22, 2019. 9780355621259 ; https://digitalcommons.odu.edu/mae_etds/30.

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

MLA Handbook (7th Edition):

Lear, Donald Joseph. “Development of a Data Acquisition System for Unmanned Aerial Vehicle (UAV) System Identification.” 2017. Web. 22 Nov 2019.

Vancouver:

Lear DJ. Development of a Data Acquisition System for Unmanned Aerial Vehicle (UAV) System Identification. [Internet] [Thesis]. Old Dominion University; 2017. [cited 2019 Nov 22]. Available from: 9780355621259 ; https://digitalcommons.odu.edu/mae_etds/30.

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

Council of Science Editors:

Lear DJ. Development of a Data Acquisition System for Unmanned Aerial Vehicle (UAV) System Identification. [Thesis]. Old Dominion University; 2017. Available from: 9780355621259 ; https://digitalcommons.odu.edu/mae_etds/30

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

8. Bernadowski, Timothy Adam. Carbon Deposition During Oxygen Production Using High Temperature Electrolysis and Mitigation Methods.

Degree: MS, Mechanical & Aerospace Engineering, 2016, Old Dominion University

  Carbon dioxide in the Martian atmosphere can be converted to oxygen during high temperature electrolysis for use in life-support and fuel systems on manned… (more)

Subjects/Keywords: Carbon deposition; High temperature electrolysis; Mitigation methods; Oxygen production; Aerospace Engineering; Mechanical Engineering

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APA (6th Edition):

Bernadowski, T. A. (2016). Carbon Deposition During Oxygen Production Using High Temperature Electrolysis and Mitigation Methods. (Thesis). Old Dominion University. Retrieved from 9781369143669 ; https://digitalcommons.odu.edu/mae_etds/10

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):

Bernadowski, Timothy Adam. “Carbon Deposition During Oxygen Production Using High Temperature Electrolysis and Mitigation Methods.” 2016. Thesis, Old Dominion University. Accessed November 22, 2019. 9781369143669 ; https://digitalcommons.odu.edu/mae_etds/10.

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

MLA Handbook (7th Edition):

Bernadowski, Timothy Adam. “Carbon Deposition During Oxygen Production Using High Temperature Electrolysis and Mitigation Methods.” 2016. Web. 22 Nov 2019.

Vancouver:

Bernadowski TA. Carbon Deposition During Oxygen Production Using High Temperature Electrolysis and Mitigation Methods. [Internet] [Thesis]. Old Dominion University; 2016. [cited 2019 Nov 22]. Available from: 9781369143669 ; https://digitalcommons.odu.edu/mae_etds/10.

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

Council of Science Editors:

Bernadowski TA. Carbon Deposition During Oxygen Production Using High Temperature Electrolysis and Mitigation Methods. [Thesis]. Old Dominion University; 2016. Available from: 9781369143669 ; https://digitalcommons.odu.edu/mae_etds/10

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

9. Baris, Engin. An Investigation into the Potential Benefits of Distributed Electric Propulsion on Small UAVS at Low Reynolds Numbers.

Degree: MS, Mechanical & Aerospace Engineering, 2017, Old Dominion University

  Distributed electric propulsion systems benefit from the inherent scale independence of electric propulsion. This property allows the designer to place multiple small electric motors… (more)

Subjects/Keywords: Design of experiments; Distributed; Electric; Low Reynolds; Propulsion; Small UAV; Aerospace Engineering; Propulsion and Power

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APA (6th Edition):

Baris, E. (2017). An Investigation into the Potential Benefits of Distributed Electric Propulsion on Small UAVS at Low Reynolds Numbers. (Thesis). Old Dominion University. Retrieved from 9780355081923 ; https://digitalcommons.odu.edu/mae_etds/24

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):

Baris, Engin. “An Investigation into the Potential Benefits of Distributed Electric Propulsion on Small UAVS at Low Reynolds Numbers.” 2017. Thesis, Old Dominion University. Accessed November 22, 2019. 9780355081923 ; https://digitalcommons.odu.edu/mae_etds/24.

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

MLA Handbook (7th Edition):

Baris, Engin. “An Investigation into the Potential Benefits of Distributed Electric Propulsion on Small UAVS at Low Reynolds Numbers.” 2017. Web. 22 Nov 2019.

Vancouver:

Baris E. An Investigation into the Potential Benefits of Distributed Electric Propulsion on Small UAVS at Low Reynolds Numbers. [Internet] [Thesis]. Old Dominion University; 2017. [cited 2019 Nov 22]. Available from: 9780355081923 ; https://digitalcommons.odu.edu/mae_etds/24.

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

Council of Science Editors:

Baris E. An Investigation into the Potential Benefits of Distributed Electric Propulsion on Small UAVS at Low Reynolds Numbers. [Thesis]. Old Dominion University; 2017. Available from: 9780355081923 ; https://digitalcommons.odu.edu/mae_etds/24

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

10. Sadowski, Nicholas Barrett. A Cost Effective Design for a Propeller Thrust/Torque Balance.

Degree: MS, Mechanical & Aerospace Engineering, 2018, Old Dominion University

  Wind tunnel balances are used with aircraft models, propellers, and components to measure applied forces and moments. The design and manufacture of a balance… (more)

Subjects/Keywords: Balance; Load cell; Mechanical design; Strain gage; Wind tunnel; Aerospace Engineering; Mechanical Engineering

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APA (6th Edition):

Sadowski, N. B. (2018). A Cost Effective Design for a Propeller Thrust/Torque Balance. (Thesis). Old Dominion University. Retrieved from 9780438022041 ; https://digitalcommons.odu.edu/mae_etds/39

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):

Sadowski, Nicholas Barrett. “A Cost Effective Design for a Propeller Thrust/Torque Balance.” 2018. Thesis, Old Dominion University. Accessed November 22, 2019. 9780438022041 ; https://digitalcommons.odu.edu/mae_etds/39.

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

MLA Handbook (7th Edition):

Sadowski, Nicholas Barrett. “A Cost Effective Design for a Propeller Thrust/Torque Balance.” 2018. Web. 22 Nov 2019.

Vancouver:

Sadowski NB. A Cost Effective Design for a Propeller Thrust/Torque Balance. [Internet] [Thesis]. Old Dominion University; 2018. [cited 2019 Nov 22]. Available from: 9780438022041 ; https://digitalcommons.odu.edu/mae_etds/39.

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

Council of Science Editors:

Sadowski NB. A Cost Effective Design for a Propeller Thrust/Torque Balance. [Thesis]. Old Dominion University; 2018. Available from: 9780438022041 ; https://digitalcommons.odu.edu/mae_etds/39

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

11. Phillips, Ben D. Design of Experiments Enhanced Statistical Process Control for Wind Tunnel Check Standard Testing.

Degree: PhD, Aerospace Engineering, 2016, Old Dominion University

  The current wind tunnel check standard testing program at NASA Langley Research Center is focused on increasing data quality, uncertainty quantification and overall control… (more)

Subjects/Keywords: Data quality; NASA Langley Research Center; Wind tunnel check standard testing program; Measurement processes; Statistical process control (SPC); Aerospace Engineering

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APA (6th Edition):

Phillips, B. D. (2016). Design of Experiments Enhanced Statistical Process Control for Wind Tunnel Check Standard Testing. (Doctoral Dissertation). Old Dominion University. Retrieved from 9781369183740 ; https://digitalcommons.odu.edu/mae_etds/15

Chicago Manual of Style (16th Edition):

Phillips, Ben D. “Design of Experiments Enhanced Statistical Process Control for Wind Tunnel Check Standard Testing.” 2016. Doctoral Dissertation, Old Dominion University. Accessed November 22, 2019. 9781369183740 ; https://digitalcommons.odu.edu/mae_etds/15.

MLA Handbook (7th Edition):

Phillips, Ben D. “Design of Experiments Enhanced Statistical Process Control for Wind Tunnel Check Standard Testing.” 2016. Web. 22 Nov 2019.

Vancouver:

Phillips BD. Design of Experiments Enhanced Statistical Process Control for Wind Tunnel Check Standard Testing. [Internet] [Doctoral dissertation]. Old Dominion University; 2016. [cited 2019 Nov 22]. Available from: 9781369183740 ; https://digitalcommons.odu.edu/mae_etds/15.

Council of Science Editors:

Phillips BD. Design of Experiments Enhanced Statistical Process Control for Wind Tunnel Check Standard Testing. [Doctoral Dissertation]. Old Dominion University; 2016. Available from: 9781369183740 ; https://digitalcommons.odu.edu/mae_etds/15

12. Simsek, Mehmet R. A Hybrid Position Feedback Controller for Bistable Structures.

Degree: MS, Mechanical & Aerospace Engineering, 2016, Old Dominion University

  Bistability is the property of structures showing the ability to attain two statically stable states. Due to dynamic and static advantages such as no… (more)

Subjects/Keywords: Bistable structure; Hybrid feedback control; Morphing wing; Piezoletric actuation; Smart systems; Snap-through; Aerospace Engineering; Mechanical Engineering

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APA (6th Edition):

Simsek, M. R. (2016). A Hybrid Position Feedback Controller for Bistable Structures. (Thesis). Old Dominion University. Retrieved from 9781339893877 ; https://digitalcommons.odu.edu/mae_etds/5

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):

Simsek, Mehmet R. “A Hybrid Position Feedback Controller for Bistable Structures.” 2016. Thesis, Old Dominion University. Accessed November 22, 2019. 9781339893877 ; https://digitalcommons.odu.edu/mae_etds/5.

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

MLA Handbook (7th Edition):

Simsek, Mehmet R. “A Hybrid Position Feedback Controller for Bistable Structures.” 2016. Web. 22 Nov 2019.

Vancouver:

Simsek MR. A Hybrid Position Feedback Controller for Bistable Structures. [Internet] [Thesis]. Old Dominion University; 2016. [cited 2019 Nov 22]. Available from: 9781339893877 ; https://digitalcommons.odu.edu/mae_etds/5.

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

Council of Science Editors:

Simsek MR. A Hybrid Position Feedback Controller for Bistable Structures. [Thesis]. Old Dominion University; 2016. Available from: 9781339893877 ; https://digitalcommons.odu.edu/mae_etds/5

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

13. Callahan, Ryan James. Long-Term Quantitative Study of Wind-Tunnel Balance Calibrations Across Multiple Calibration Systems.

Degree: MS, Aerospace Engineering, 2016, Old Dominion University

  Internal strain-gauge balances are multi-dimensional force transducers widely employed in wind tunnels to obtain accurate aerodynamic force and moment data on an aircraft model.… (more)

Subjects/Keywords: Calibration; Design of experiments; Long-term study; Regression; Statistical process control; Wind-tunnel balance; Aerospace Engineering

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APA (6th Edition):

Callahan, R. J. (2016). Long-Term Quantitative Study of Wind-Tunnel Balance Calibrations Across Multiple Calibration Systems. (Thesis). Old Dominion University. Retrieved from 9781339837451 ; https://digitalcommons.odu.edu/mae_etds/3

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):

Callahan, Ryan James. “Long-Term Quantitative Study of Wind-Tunnel Balance Calibrations Across Multiple Calibration Systems.” 2016. Thesis, Old Dominion University. Accessed November 22, 2019. 9781339837451 ; https://digitalcommons.odu.edu/mae_etds/3.

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

MLA Handbook (7th Edition):

Callahan, Ryan James. “Long-Term Quantitative Study of Wind-Tunnel Balance Calibrations Across Multiple Calibration Systems.” 2016. Web. 22 Nov 2019.

Vancouver:

Callahan RJ. Long-Term Quantitative Study of Wind-Tunnel Balance Calibrations Across Multiple Calibration Systems. [Internet] [Thesis]. Old Dominion University; 2016. [cited 2019 Nov 22]. Available from: 9781339837451 ; https://digitalcommons.odu.edu/mae_etds/3.

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

Council of Science Editors:

Callahan RJ. Long-Term Quantitative Study of Wind-Tunnel Balance Calibrations Across Multiple Calibration Systems. [Thesis]. Old Dominion University; 2016. Available from: 9781339837451 ; https://digitalcommons.odu.edu/mae_etds/3

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

14. Thompson, Michael P. Experimental Analysis of Turbulent Structures and the Effects of Non-Equilibrium on an Axial Vortex.

Degree: MS, Mechanical & Aerospace Engineering, 2016, Old Dominion University

  Examples of the axial vortex include, dust devils, trailing line aircraft wake vortices, and tornadoes. Some of these vortices can prove hazardous to individuals… (more)

Subjects/Keywords: Axial vortex; Fluid mechanics; Hot-wire annemometrey; Non-equilibrium pressure; Turbulent flows; Aerospace Engineering; Physics

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APA (6th Edition):

Thompson, M. P. (2016). Experimental Analysis of Turbulent Structures and the Effects of Non-Equilibrium on an Axial Vortex. (Thesis). Old Dominion University. Retrieved from 9781339893891 ; https://digitalcommons.odu.edu/mae_etds/8

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):

Thompson, Michael P. “Experimental Analysis of Turbulent Structures and the Effects of Non-Equilibrium on an Axial Vortex.” 2016. Thesis, Old Dominion University. Accessed November 22, 2019. 9781339893891 ; https://digitalcommons.odu.edu/mae_etds/8.

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

MLA Handbook (7th Edition):

Thompson, Michael P. “Experimental Analysis of Turbulent Structures and the Effects of Non-Equilibrium on an Axial Vortex.” 2016. Web. 22 Nov 2019.

Vancouver:

Thompson MP. Experimental Analysis of Turbulent Structures and the Effects of Non-Equilibrium on an Axial Vortex. [Internet] [Thesis]. Old Dominion University; 2016. [cited 2019 Nov 22]. Available from: 9781339893891 ; https://digitalcommons.odu.edu/mae_etds/8.

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

Council of Science Editors:

Thompson MP. Experimental Analysis of Turbulent Structures and the Effects of Non-Equilibrium on an Axial Vortex. [Thesis]. Old Dominion University; 2016. Available from: 9781339893891 ; https://digitalcommons.odu.edu/mae_etds/8

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

15. Mills, Lucas Coleman. Gust Alleviation System for General Aviation Aircraft.

Degree: MS, Mechanical & Aerospace Engineering, 2018, Old Dominion University

  A designed control motion scheme to improve passenger comfort in general aviation aircraft by reducing normal acceleration and pitch rate due to turbulence is… (more)

Subjects/Keywords: Aviation aircraft; Passenger comfort; Control motion; Aerospace Engineering

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APA (6th Edition):

Mills, L. C. (2018). Gust Alleviation System for General Aviation Aircraft. (Thesis). Old Dominion University. Retrieved from 9780438991736 ; https://digitalcommons.odu.edu/mae_etds/174

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):

Mills, Lucas Coleman. “Gust Alleviation System for General Aviation Aircraft.” 2018. Thesis, Old Dominion University. Accessed November 22, 2019. 9780438991736 ; https://digitalcommons.odu.edu/mae_etds/174.

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

MLA Handbook (7th Edition):

Mills, Lucas Coleman. “Gust Alleviation System for General Aviation Aircraft.” 2018. Web. 22 Nov 2019.

Vancouver:

Mills LC. Gust Alleviation System for General Aviation Aircraft. [Internet] [Thesis]. Old Dominion University; 2018. [cited 2019 Nov 22]. Available from: 9780438991736 ; https://digitalcommons.odu.edu/mae_etds/174.

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

Council of Science Editors:

Mills LC. Gust Alleviation System for General Aviation Aircraft. [Thesis]. Old Dominion University; 2018. Available from: 9780438991736 ; https://digitalcommons.odu.edu/mae_etds/174

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

16. Webb, Thomas Ladson, III. A Monolithic Internal Strain-Gage Balance Design Based on Design for Manufacturability.

Degree: MS, Mechanical & Aerospace Engineering, 2018, Old Dominion University

  This paper proposes an alternative approach to internal strain-gage balance design driven by Design for Manufacturability (DFM) principles. The objective of this research was… (more)

Subjects/Keywords: Balance; Design; Manufacturing; Measurement; NASA; Optimization; Aerospace Engineering; Mechanical Engineering

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APA (6th Edition):

Webb, Thomas Ladson, I. (2018). A Monolithic Internal Strain-Gage Balance Design Based on Design for Manufacturability. (Thesis). Old Dominion University. Retrieved from 9780438991668 ; https://digitalcommons.odu.edu/mae_etds/171

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):

Webb, Thomas Ladson, III. “A Monolithic Internal Strain-Gage Balance Design Based on Design for Manufacturability.” 2018. Thesis, Old Dominion University. Accessed November 22, 2019. 9780438991668 ; https://digitalcommons.odu.edu/mae_etds/171.

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

MLA Handbook (7th Edition):

Webb, Thomas Ladson, III. “A Monolithic Internal Strain-Gage Balance Design Based on Design for Manufacturability.” 2018. Web. 22 Nov 2019.

Vancouver:

Webb, Thomas Ladson I. A Monolithic Internal Strain-Gage Balance Design Based on Design for Manufacturability. [Internet] [Thesis]. Old Dominion University; 2018. [cited 2019 Nov 22]. Available from: 9780438991668 ; https://digitalcommons.odu.edu/mae_etds/171.

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

Council of Science Editors:

Webb, Thomas Ladson I. A Monolithic Internal Strain-Gage Balance Design Based on Design for Manufacturability. [Thesis]. Old Dominion University; 2018. Available from: 9780438991668 ; https://digitalcommons.odu.edu/mae_etds/171

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

17. Neill, Cameron K. Comparison of Support Methods for Static Aerodynamic Testing and Validation of a Magnetic Suspension and Balance System.

Degree: MS, Mechanical & Aerospace Engineering, 2019, Old Dominion University

  Magnetic suspension wind tunnels offer an alternative to traditional physical support methods. They allow for the collection of support interference free data and broader… (more)

Subjects/Keywords: Magnetic suspension; MSBS; NASA; Stardust; Static; Support interference; Aerospace Engineering; Mechanical Engineering

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APA (6th Edition):

Neill, C. K. (2019). Comparison of Support Methods for Static Aerodynamic Testing and Validation of a Magnetic Suspension and Balance System. (Thesis). Old Dominion University. Retrieved from 9781085602839 ; https://digitalcommons.odu.edu/mae_etds/203

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):

Neill, Cameron K. “Comparison of Support Methods for Static Aerodynamic Testing and Validation of a Magnetic Suspension and Balance System.” 2019. Thesis, Old Dominion University. Accessed November 22, 2019. 9781085602839 ; https://digitalcommons.odu.edu/mae_etds/203.

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

MLA Handbook (7th Edition):

Neill, Cameron K. “Comparison of Support Methods for Static Aerodynamic Testing and Validation of a Magnetic Suspension and Balance System.” 2019. Web. 22 Nov 2019.

Vancouver:

Neill CK. Comparison of Support Methods for Static Aerodynamic Testing and Validation of a Magnetic Suspension and Balance System. [Internet] [Thesis]. Old Dominion University; 2019. [cited 2019 Nov 22]. Available from: 9781085602839 ; https://digitalcommons.odu.edu/mae_etds/203.

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

Council of Science Editors:

Neill CK. Comparison of Support Methods for Static Aerodynamic Testing and Validation of a Magnetic Suspension and Balance System. [Thesis]. Old Dominion University; 2019. Available from: 9781085602839 ; https://digitalcommons.odu.edu/mae_etds/203

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

18. Benjamin, Colin Bruce Leighton. Characterization and Optimization of a Propeller Test Stand.

Degree: MS, Mechanical & Aerospace Engineering, 2019, Old Dominion University

  In recent history, there has been a rapid rise in the use of drones, and they are expanding in popularity each year. The widespread… (more)

Subjects/Keywords: Characterization; Optimization; Propeller; Stand; Test; Aerospace Engineering; Mechanical Engineering

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APA (6th Edition):

Benjamin, C. B. L. (2019). Characterization and Optimization of a Propeller Test Stand. (Thesis). Old Dominion University. Retrieved from 9781085639361 ; https://digitalcommons.odu.edu/mae_etds/198

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):

Benjamin, Colin Bruce Leighton. “Characterization and Optimization of a Propeller Test Stand.” 2019. Thesis, Old Dominion University. Accessed November 22, 2019. 9781085639361 ; https://digitalcommons.odu.edu/mae_etds/198.

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

MLA Handbook (7th Edition):

Benjamin, Colin Bruce Leighton. “Characterization and Optimization of a Propeller Test Stand.” 2019. Web. 22 Nov 2019.

Vancouver:

Benjamin CBL. Characterization and Optimization of a Propeller Test Stand. [Internet] [Thesis]. Old Dominion University; 2019. [cited 2019 Nov 22]. Available from: 9781085639361 ; https://digitalcommons.odu.edu/mae_etds/198.

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

Council of Science Editors:

Benjamin CBL. Characterization and Optimization of a Propeller Test Stand. [Thesis]. Old Dominion University; 2019. Available from: 9781085639361 ; https://digitalcommons.odu.edu/mae_etds/198

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

19. Johnson, Thomas H. A Variable Acceleration Calibration System.

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

  A variable acceleration calibration system that applies loads using gravitational and centripetal acceleration serves as an alternative, efficient and cost effective method for calibrating… (more)

Subjects/Keywords: Acceleration; Calibration; Force balance; Internal wind tunnel; Loads; Aerospace Engineering

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APA (6th Edition):

Johnson, T. H. (2011). A Variable Acceleration Calibration System. (Doctoral Dissertation). Old Dominion University. Retrieved from 9781124973067 ; https://digitalcommons.odu.edu/mae_etds/65

Chicago Manual of Style (16th Edition):

Johnson, Thomas H. “A Variable Acceleration Calibration System.” 2011. Doctoral Dissertation, Old Dominion University. Accessed November 22, 2019. 9781124973067 ; https://digitalcommons.odu.edu/mae_etds/65.

MLA Handbook (7th Edition):

Johnson, Thomas H. “A Variable Acceleration Calibration System.” 2011. Web. 22 Nov 2019.

Vancouver:

Johnson TH. A Variable Acceleration Calibration System. [Internet] [Doctoral dissertation]. Old Dominion University; 2011. [cited 2019 Nov 22]. Available from: 9781124973067 ; https://digitalcommons.odu.edu/mae_etds/65.

Council of Science Editors:

Johnson TH. A Variable Acceleration Calibration System. [Doctoral Dissertation]. Old Dominion University; 2011. Available from: 9781124973067 ; https://digitalcommons.odu.edu/mae_etds/65

20. Nacakli, Yavuz. Analysis of Helicopter Downwash/Frigate Airwake Interaction Using Statistically Designed Experiments.

Degree: PhD, Aerospace Engineering, 2010, Old Dominion University

  A research program to investigate helicopter downwash/frigate airwake interaction has been initiated using a statistically robust experimental program featuring Design of Experiments. Engineering analysis… (more)

Subjects/Keywords: Airwakes; Downwash; Frigates; Helicopters; Aerospace Engineering

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APA (6th Edition):

Nacakli, Y. (2010). Analysis of Helicopter Downwash/Frigate Airwake Interaction Using Statistically Designed Experiments. (Doctoral Dissertation). Old Dominion University. Retrieved from 9781124113142 ; https://digitalcommons.odu.edu/mae_etds/73

Chicago Manual of Style (16th Edition):

Nacakli, Yavuz. “Analysis of Helicopter Downwash/Frigate Airwake Interaction Using Statistically Designed Experiments.” 2010. Doctoral Dissertation, Old Dominion University. Accessed November 22, 2019. 9781124113142 ; https://digitalcommons.odu.edu/mae_etds/73.

MLA Handbook (7th Edition):

Nacakli, Yavuz. “Analysis of Helicopter Downwash/Frigate Airwake Interaction Using Statistically Designed Experiments.” 2010. Web. 22 Nov 2019.

Vancouver:

Nacakli Y. Analysis of Helicopter Downwash/Frigate Airwake Interaction Using Statistically Designed Experiments. [Internet] [Doctoral dissertation]. Old Dominion University; 2010. [cited 2019 Nov 22]. Available from: 9781124113142 ; https://digitalcommons.odu.edu/mae_etds/73.

Council of Science Editors:

Nacakli Y. Analysis of Helicopter Downwash/Frigate Airwake Interaction Using Statistically Designed Experiments. [Doctoral Dissertation]. Old Dominion University; 2010. Available from: 9781124113142 ; https://digitalcommons.odu.edu/mae_etds/73

21. Como, Sean A. Measurement System Characterization in the Presence of Measurement Errors.

Degree: PhD, Mechanical & Aerospace Engineering, 2012, Old Dominion University

  In the calibration of a measurement system, data are collected in order to estimate a mathematical model between one or more factors of interest… (more)

Subjects/Keywords: Measurement errors; Modified least squares; Models; Aerospace Engineering

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APA (6th Edition):

Como, S. A. (2012). Measurement System Characterization in the Presence of Measurement Errors. (Doctoral Dissertation). Old Dominion University. Retrieved from 9781267736529 ; https://digitalcommons.odu.edu/mae_etds/122

Chicago Manual of Style (16th Edition):

Como, Sean A. “Measurement System Characterization in the Presence of Measurement Errors.” 2012. Doctoral Dissertation, Old Dominion University. Accessed November 22, 2019. 9781267736529 ; https://digitalcommons.odu.edu/mae_etds/122.

MLA Handbook (7th Edition):

Como, Sean A. “Measurement System Characterization in the Presence of Measurement Errors.” 2012. Web. 22 Nov 2019.

Vancouver:

Como SA. Measurement System Characterization in the Presence of Measurement Errors. [Internet] [Doctoral dissertation]. Old Dominion University; 2012. [cited 2019 Nov 22]. Available from: 9781267736529 ; https://digitalcommons.odu.edu/mae_etds/122.

Council of Science Editors:

Como SA. Measurement System Characterization in the Presence of Measurement Errors. [Doctoral Dissertation]. Old Dominion University; 2012. Available from: 9781267736529 ; https://digitalcommons.odu.edu/mae_etds/122

22. Norman, Narcrisha S. Modeling Martian Planetary Entry Descent and Landing Using Monte Carlo Driven Response Surface Methodology.

Degree: PhD, Aerospace Engineering, 2012, Old Dominion University

  Response surface methodology (RSM) is a statistical method that explores the relationships between several descriptive variables and one or more response variables. For over… (more)

Subjects/Keywords: Design of experiments; Martian planetary entry descent; Martian planetary landing; Regression modeling; Response surface methodology; Viking; Aerospace Engineering; Applied Statistics; Physics

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APA (6th Edition):

Norman, N. S. (2012). Modeling Martian Planetary Entry Descent and Landing Using Monte Carlo Driven Response Surface Methodology. (Doctoral Dissertation). Old Dominion University. Retrieved from 9781303080043 ; https://digitalcommons.odu.edu/mae_etds/151

Chicago Manual of Style (16th Edition):

Norman, Narcrisha S. “Modeling Martian Planetary Entry Descent and Landing Using Monte Carlo Driven Response Surface Methodology.” 2012. Doctoral Dissertation, Old Dominion University. Accessed November 22, 2019. 9781303080043 ; https://digitalcommons.odu.edu/mae_etds/151.

MLA Handbook (7th Edition):

Norman, Narcrisha S. “Modeling Martian Planetary Entry Descent and Landing Using Monte Carlo Driven Response Surface Methodology.” 2012. Web. 22 Nov 2019.

Vancouver:

Norman NS. Modeling Martian Planetary Entry Descent and Landing Using Monte Carlo Driven Response Surface Methodology. [Internet] [Doctoral dissertation]. Old Dominion University; 2012. [cited 2019 Nov 22]. Available from: 9781303080043 ; https://digitalcommons.odu.edu/mae_etds/151.

Council of Science Editors:

Norman NS. Modeling Martian Planetary Entry Descent and Landing Using Monte Carlo Driven Response Surface Methodology. [Doctoral Dissertation]. Old Dominion University; 2012. Available from: 9781303080043 ; https://digitalcommons.odu.edu/mae_etds/151

23. Sahin, Burhan. Analysis of Wake Vortices of a Medium Range Twin-Propeller Military Cargo Aircraft Using Statistically Designed Experiments.

Degree: PhD, Aerospace Engineering, 2010, Old Dominion University

  An experimental study was initiated to analyze the trajectories of the streamwise vortices behind the wing tip and flap of a medium range and… (more)

Subjects/Keywords: Aerodynamics; Military aircraft; Wake vortices; Aerodynamics and Fluid Mechanics; Aerospace Engineering; Mechanical Engineering

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APA (6th Edition):

Sahin, B. (2010). Analysis of Wake Vortices of a Medium Range Twin-Propeller Military Cargo Aircraft Using Statistically Designed Experiments. (Doctoral Dissertation). Old Dominion University. Retrieved from 9781124453071 ; https://digitalcommons.odu.edu/mae_etds/87

Chicago Manual of Style (16th Edition):

Sahin, Burhan. “Analysis of Wake Vortices of a Medium Range Twin-Propeller Military Cargo Aircraft Using Statistically Designed Experiments.” 2010. Doctoral Dissertation, Old Dominion University. Accessed November 22, 2019. 9781124453071 ; https://digitalcommons.odu.edu/mae_etds/87.

MLA Handbook (7th Edition):

Sahin, Burhan. “Analysis of Wake Vortices of a Medium Range Twin-Propeller Military Cargo Aircraft Using Statistically Designed Experiments.” 2010. Web. 22 Nov 2019.

Vancouver:

Sahin B. Analysis of Wake Vortices of a Medium Range Twin-Propeller Military Cargo Aircraft Using Statistically Designed Experiments. [Internet] [Doctoral dissertation]. Old Dominion University; 2010. [cited 2019 Nov 22]. Available from: 9781124453071 ; https://digitalcommons.odu.edu/mae_etds/87.

Council of Science Editors:

Sahin B. Analysis of Wake Vortices of a Medium Range Twin-Propeller Military Cargo Aircraft Using Statistically Designed Experiments. [Doctoral Dissertation]. Old Dominion University; 2010. Available from: 9781124453071 ; https://digitalcommons.odu.edu/mae_etds/87

24. Williams, Brianne Y. The Effect of Systematic Error in Forced Oscillation Wind Tunnel Test Apparatuses on Determining Nonlinear Unsteady Aerodynamic Stability Derivatives.

Degree: PhD, Aerospace Engineering, 2010, Old Dominion University

  One of the basic problems of flight dynamics is the formulation of aerodynamic forces and moments acting on an aircraft in arbitrary motion. Classically… (more)

Subjects/Keywords: Forced oscillation; Stability derivatives; Wind tunnels; Aerospace Engineering

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APA (6th Edition):

Williams, B. Y. (2010). The Effect of Systematic Error in Forced Oscillation Wind Tunnel Test Apparatuses on Determining Nonlinear Unsteady Aerodynamic Stability Derivatives. (Doctoral Dissertation). Old Dominion University. Retrieved from 9781124342993 ; https://digitalcommons.odu.edu/mae_etds/91

Chicago Manual of Style (16th Edition):

Williams, Brianne Y. “The Effect of Systematic Error in Forced Oscillation Wind Tunnel Test Apparatuses on Determining Nonlinear Unsteady Aerodynamic Stability Derivatives.” 2010. Doctoral Dissertation, Old Dominion University. Accessed November 22, 2019. 9781124342993 ; https://digitalcommons.odu.edu/mae_etds/91.

MLA Handbook (7th Edition):

Williams, Brianne Y. “The Effect of Systematic Error in Forced Oscillation Wind Tunnel Test Apparatuses on Determining Nonlinear Unsteady Aerodynamic Stability Derivatives.” 2010. Web. 22 Nov 2019.

Vancouver:

Williams BY. The Effect of Systematic Error in Forced Oscillation Wind Tunnel Test Apparatuses on Determining Nonlinear Unsteady Aerodynamic Stability Derivatives. [Internet] [Doctoral dissertation]. Old Dominion University; 2010. [cited 2019 Nov 22]. Available from: 9781124342993 ; https://digitalcommons.odu.edu/mae_etds/91.

Council of Science Editors:

Williams BY. The Effect of Systematic Error in Forced Oscillation Wind Tunnel Test Apparatuses on Determining Nonlinear Unsteady Aerodynamic Stability Derivatives. [Doctoral Dissertation]. Old Dominion University; 2010. Available from: 9781124342993 ; https://digitalcommons.odu.edu/mae_etds/91

25. Bayraktar, Ilhan. External Aerodynamics of Heavy Ground Vehicles: Computations and Wind Tunnel Testing.

Degree: PhD, Aerospace Engineering, 2002, Old Dominion University

  Aerodynamic characteristics of a ground vehicle affect vehicle operation in many ways. Aerodynamic drag, lift and side forces have influence on fuel efficiency, vehicle… (more)

Subjects/Keywords: Aerodynamics; Bluff body; Ground vehicles; Wind tunnel; Aerodynamics and Fluid Mechanics; Aerospace Engineering; Automotive Engineering; Mechanical Engineering

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APA (6th Edition):

Bayraktar, I. (2002). External Aerodynamics of Heavy Ground Vehicles: Computations and Wind Tunnel Testing. (Doctoral Dissertation). Old Dominion University. Retrieved from 9780493712970 ; https://digitalcommons.odu.edu/mae_etds/49

Chicago Manual of Style (16th Edition):

Bayraktar, Ilhan. “External Aerodynamics of Heavy Ground Vehicles: Computations and Wind Tunnel Testing.” 2002. Doctoral Dissertation, Old Dominion University. Accessed November 22, 2019. 9780493712970 ; https://digitalcommons.odu.edu/mae_etds/49.

MLA Handbook (7th Edition):

Bayraktar, Ilhan. “External Aerodynamics of Heavy Ground Vehicles: Computations and Wind Tunnel Testing.” 2002. Web. 22 Nov 2019.

Vancouver:

Bayraktar I. External Aerodynamics of Heavy Ground Vehicles: Computations and Wind Tunnel Testing. [Internet] [Doctoral dissertation]. Old Dominion University; 2002. [cited 2019 Nov 22]. Available from: 9780493712970 ; https://digitalcommons.odu.edu/mae_etds/49.

Council of Science Editors:

Bayraktar I. External Aerodynamics of Heavy Ground Vehicles: Computations and Wind Tunnel Testing. [Doctoral Dissertation]. Old Dominion University; 2002. Available from: 9780493712970 ; https://digitalcommons.odu.edu/mae_etds/49

26. Koc, Ilteris. Experimental Investigation of Active Control of Bluff Body Vortex Shedding.

Degree: PhD, Aerospace Engineering, 2008, Old Dominion University

  Mean and fluctuating forces acting on a body are strongly related to vortex shedding generated behind it. Therefore, it is possible to obtain substantial… (more)

Subjects/Keywords: Active control; Bluff bodies; Ogive cylinders; Vortex shedding; Aerodynamics and Fluid Mechanics; Mechanical Engineering; Navigation, Guidance, Control and Dynamics; Structures and Materials

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APA (6th Edition):

Koc, I. (2008). Experimental Investigation of Active Control of Bluff Body Vortex Shedding. (Doctoral Dissertation). Old Dominion University. Retrieved from 9780549920861 ; https://digitalcommons.odu.edu/mae_etds/71

Chicago Manual of Style (16th Edition):

Koc, Ilteris. “Experimental Investigation of Active Control of Bluff Body Vortex Shedding.” 2008. Doctoral Dissertation, Old Dominion University. Accessed November 22, 2019. 9780549920861 ; https://digitalcommons.odu.edu/mae_etds/71.

MLA Handbook (7th Edition):

Koc, Ilteris. “Experimental Investigation of Active Control of Bluff Body Vortex Shedding.” 2008. Web. 22 Nov 2019.

Vancouver:

Koc I. Experimental Investigation of Active Control of Bluff Body Vortex Shedding. [Internet] [Doctoral dissertation]. Old Dominion University; 2008. [cited 2019 Nov 22]. Available from: 9780549920861 ; https://digitalcommons.odu.edu/mae_etds/71.

Council of Science Editors:

Koc I. Experimental Investigation of Active Control of Bluff Body Vortex Shedding. [Doctoral Dissertation]. Old Dominion University; 2008. Available from: 9780549920861 ; https://digitalcommons.odu.edu/mae_etds/71

27. Mokhtar, Wael Ahmed. Boundary Interference Assessment and Correction for Open Jet Wind Tunnels Using Panel Methods.

Degree: PhD, Aerospace Engineering, 2006, Old Dominion University

  The presence of nearby boundaries in a wind tunnel can lead to aerodynamic measurements on a model in the wind tunnel that differ from… (more)

Subjects/Keywords: Boundary interference; Open jet; Wind tunnels; Aerospace Engineering; Mechanical Engineering; Structures and Materials

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APA (6th Edition):

Mokhtar, W. A. (2006). Boundary Interference Assessment and Correction for Open Jet Wind Tunnels Using Panel Methods. (Doctoral Dissertation). Old Dominion University. Retrieved from 9780542753879 ; https://digitalcommons.odu.edu/mae_etds/74

Chicago Manual of Style (16th Edition):

Mokhtar, Wael Ahmed. “Boundary Interference Assessment and Correction for Open Jet Wind Tunnels Using Panel Methods.” 2006. Doctoral Dissertation, Old Dominion University. Accessed November 22, 2019. 9780542753879 ; https://digitalcommons.odu.edu/mae_etds/74.

MLA Handbook (7th Edition):

Mokhtar, Wael Ahmed. “Boundary Interference Assessment and Correction for Open Jet Wind Tunnels Using Panel Methods.” 2006. Web. 22 Nov 2019.

Vancouver:

Mokhtar WA. Boundary Interference Assessment and Correction for Open Jet Wind Tunnels Using Panel Methods. [Internet] [Doctoral dissertation]. Old Dominion University; 2006. [cited 2019 Nov 22]. Available from: 9780542753879 ; https://digitalcommons.odu.edu/mae_etds/74.

Council of Science Editors:

Mokhtar WA. Boundary Interference Assessment and Correction for Open Jet Wind Tunnels Using Panel Methods. [Doctoral Dissertation]. Old Dominion University; 2006. Available from: 9780542753879 ; https://digitalcommons.odu.edu/mae_etds/74

28. Isik, Okay. An Integrated Probability-Based Approach for Multiple Response Surface Optimization.

Degree: PhD, Engineering Management, 2009, Old Dominion University

  Nearly all real life systems have multiple quality characteristics where individual modeling and optimization approaches can not provide a balanced compromising solution. Since performance,… (more)

Subjects/Keywords: Surface optimization; Quality management; Quality control; Business Administration, Management, and Operations; Industrial Engineering

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APA (6th Edition):

Isik, O. (2009). An Integrated Probability-Based Approach for Multiple Response Surface Optimization. (Doctoral Dissertation). Old Dominion University. Retrieved from 9781109566307 ; https://digitalcommons.odu.edu/emse_etds/86

Chicago Manual of Style (16th Edition):

Isik, Okay. “An Integrated Probability-Based Approach for Multiple Response Surface Optimization.” 2009. Doctoral Dissertation, Old Dominion University. Accessed November 22, 2019. 9781109566307 ; https://digitalcommons.odu.edu/emse_etds/86.

MLA Handbook (7th Edition):

Isik, Okay. “An Integrated Probability-Based Approach for Multiple Response Surface Optimization.” 2009. Web. 22 Nov 2019.

Vancouver:

Isik O. An Integrated Probability-Based Approach for Multiple Response Surface Optimization. [Internet] [Doctoral dissertation]. Old Dominion University; 2009. [cited 2019 Nov 22]. Available from: 9781109566307 ; https://digitalcommons.odu.edu/emse_etds/86.

Council of Science Editors:

Isik O. An Integrated Probability-Based Approach for Multiple Response Surface Optimization. [Doctoral Dissertation]. Old Dominion University; 2009. Available from: 9781109566307 ; https://digitalcommons.odu.edu/emse_etds/86

29. Walker, Ira James. An Experimental Study of Flow Control Techniques on a Multi-Element Airfoil.

Degree: PhD, Aerospace Engineering, 2003, Old Dominion University

  The results of a wind tunnel experiment are reported, which investigated two different flow control techniques that demonstrated the potential of increasing the lift… (more)

Subjects/Keywords: Airfoil; Flow control; Lift coefficient; Trailing-edge flap; Aerospace Engineering

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

APA (6th Edition):

Walker, I. J. (2003). An Experimental Study of Flow Control Techniques on a Multi-Element Airfoil. (Doctoral Dissertation). Old Dominion University. Retrieved from https://digitalcommons.odu.edu/mae_etds/90

Chicago Manual of Style (16th Edition):

Walker, Ira James. “An Experimental Study of Flow Control Techniques on a Multi-Element Airfoil.” 2003. Doctoral Dissertation, Old Dominion University. Accessed November 22, 2019. https://digitalcommons.odu.edu/mae_etds/90.

MLA Handbook (7th Edition):

Walker, Ira James. “An Experimental Study of Flow Control Techniques on a Multi-Element Airfoil.” 2003. Web. 22 Nov 2019.

Vancouver:

Walker IJ. An Experimental Study of Flow Control Techniques on a Multi-Element Airfoil. [Internet] [Doctoral dissertation]. Old Dominion University; 2003. [cited 2019 Nov 22]. Available from: https://digitalcommons.odu.edu/mae_etds/90.

Council of Science Editors:

Walker IJ. An Experimental Study of Flow Control Techniques on a Multi-Element Airfoil. [Doctoral Dissertation]. Old Dominion University; 2003. Available from: https://digitalcommons.odu.edu/mae_etds/90

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