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You searched for +publisher:"University of Kansas" +contributor:("Keshmiri, Shawn"). Showing records 1 – 26 of 26 total matches.

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University of Kansas

1. Brown, Matthew Alan. A Computational Method for Determining Distributed Aerodynamic Loads on Planforms of Arbitrary Shape in Compressible Subsonic Flow.

Degree: MS, Aerospace Engineering, 2013, University of Kansas

 The methods presented in this work are intended to provided an easy to understand and easy to apply method for determining the distributed aerodynamic loads… (more)

Subjects/Keywords: Aerospace engineering; Aerodyanmic loads; Cranked wing; Wing aerodyanmics; Wing loads

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APA (6th Edition):

Brown, M. A. (2013). A Computational Method for Determining Distributed Aerodynamic Loads on Planforms of Arbitrary Shape in Compressible Subsonic Flow. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/14195

Chicago Manual of Style (16th Edition):

Brown, Matthew Alan. “A Computational Method for Determining Distributed Aerodynamic Loads on Planforms of Arbitrary Shape in Compressible Subsonic Flow.” 2013. Masters Thesis, University of Kansas. Accessed January 18, 2021. http://hdl.handle.net/1808/14195.

MLA Handbook (7th Edition):

Brown, Matthew Alan. “A Computational Method for Determining Distributed Aerodynamic Loads on Planforms of Arbitrary Shape in Compressible Subsonic Flow.” 2013. Web. 18 Jan 2021.

Vancouver:

Brown MA. A Computational Method for Determining Distributed Aerodynamic Loads on Planforms of Arbitrary Shape in Compressible Subsonic Flow. [Internet] [Masters thesis]. University of Kansas; 2013. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1808/14195.

Council of Science Editors:

Brown MA. A Computational Method for Determining Distributed Aerodynamic Loads on Planforms of Arbitrary Shape in Compressible Subsonic Flow. [Masters Thesis]. University of Kansas; 2013. Available from: http://hdl.handle.net/1808/14195


University of Kansas

2. Lykins, Ryan. Unsteady Aerodynamic and Dynamic Analysis of the Meridian UAS in a Rolling-Yawing Motion.

Degree: MS, Aerospace Engineering, 2014, University of Kansas

 The nonlinear and unsteady aerodynamic effects of operating the Meridian unmanned aerial system (UAS) in crosswinds and at high angular rates is investigated in this… (more)

Subjects/Keywords: Aerospace engineering; Crosswind; Unmanned aerial system; Unsteady aerodynamics; V-tail

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APA (6th Edition):

Lykins, R. (2014). Unsteady Aerodynamic and Dynamic Analysis of the Meridian UAS in a Rolling-Yawing Motion. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/14605

Chicago Manual of Style (16th Edition):

Lykins, Ryan. “Unsteady Aerodynamic and Dynamic Analysis of the Meridian UAS in a Rolling-Yawing Motion.” 2014. Masters Thesis, University of Kansas. Accessed January 18, 2021. http://hdl.handle.net/1808/14605.

MLA Handbook (7th Edition):

Lykins, Ryan. “Unsteady Aerodynamic and Dynamic Analysis of the Meridian UAS in a Rolling-Yawing Motion.” 2014. Web. 18 Jan 2021.

Vancouver:

Lykins R. Unsteady Aerodynamic and Dynamic Analysis of the Meridian UAS in a Rolling-Yawing Motion. [Internet] [Masters thesis]. University of Kansas; 2014. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1808/14605.

Council of Science Editors:

Lykins R. Unsteady Aerodynamic and Dynamic Analysis of the Meridian UAS in a Rolling-Yawing Motion. [Masters Thesis]. University of Kansas; 2014. Available from: http://hdl.handle.net/1808/14605


University of Kansas

3. Homsrivaranon, Kanin. Investigation of Active Flow Control on an Extremely Thick Wind Turbine Airfoil.

Degree: MS, Aerospace Engineering, 2016, University of Kansas

 Today, modern wind turbine size has become larger than ever. The conventional airfoil near rotor hub cannot provide the structure integrity for the rotor blades.… (more)

Subjects/Keywords: Aerospace engineering

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APA (6th Edition):

Homsrivaranon, K. (2016). Investigation of Active Flow Control on an Extremely Thick Wind Turbine Airfoil. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/21970

Chicago Manual of Style (16th Edition):

Homsrivaranon, Kanin. “Investigation of Active Flow Control on an Extremely Thick Wind Turbine Airfoil.” 2016. Masters Thesis, University of Kansas. Accessed January 18, 2021. http://hdl.handle.net/1808/21970.

MLA Handbook (7th Edition):

Homsrivaranon, Kanin. “Investigation of Active Flow Control on an Extremely Thick Wind Turbine Airfoil.” 2016. Web. 18 Jan 2021.

Vancouver:

Homsrivaranon K. Investigation of Active Flow Control on an Extremely Thick Wind Turbine Airfoil. [Internet] [Masters thesis]. University of Kansas; 2016. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1808/21970.

Council of Science Editors:

Homsrivaranon K. Investigation of Active Flow Control on an Extremely Thick Wind Turbine Airfoil. [Masters Thesis]. University of Kansas; 2016. Available from: http://hdl.handle.net/1808/21970


University of Kansas

4. Lee, Adrian Kok Chiang. Evaluation of Protruding Centerbody on the Novel Airdata Sensor.

Degree: MS, Aerospace Engineering, 2016, University of Kansas

 A novel airdata sensor was developed at the University of Kansas1. The Bio-Inspired probe was designed for high angles of attack and sideslip use, suitable… (more)

Subjects/Keywords: Aerospace engineering; Engineering; airdata sensor; Bio-Inspired; Coanda effect; flow capture; protruding centerbody

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APA (6th Edition):

Lee, A. K. C. (2016). Evaluation of Protruding Centerbody on the Novel Airdata Sensor. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/22341

Chicago Manual of Style (16th Edition):

Lee, Adrian Kok Chiang. “Evaluation of Protruding Centerbody on the Novel Airdata Sensor.” 2016. Masters Thesis, University of Kansas. Accessed January 18, 2021. http://hdl.handle.net/1808/22341.

MLA Handbook (7th Edition):

Lee, Adrian Kok Chiang. “Evaluation of Protruding Centerbody on the Novel Airdata Sensor.” 2016. Web. 18 Jan 2021.

Vancouver:

Lee AKC. Evaluation of Protruding Centerbody on the Novel Airdata Sensor. [Internet] [Masters thesis]. University of Kansas; 2016. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1808/22341.

Council of Science Editors:

Lee AKC. Evaluation of Protruding Centerbody on the Novel Airdata Sensor. [Masters Thesis]. University of Kansas; 2016. Available from: http://hdl.handle.net/1808/22341


University of Kansas

5. D'Silva, Adam. Investigation on Entropy Signature of Objects.

Degree: MS, Aerospace Engineering, 2017, University of Kansas

 With the use of modern configuration and advanced stealth technologies, aircraft have the ability to minimize their signatures significantly. The three main signatures being infrared,… (more)

Subjects/Keywords: Aerospace engineering; Entropy Signature; Low Observable

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APA (6th Edition):

D'Silva, A. (2017). Investigation on Entropy Signature of Objects. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/24146

Chicago Manual of Style (16th Edition):

D'Silva, Adam. “Investigation on Entropy Signature of Objects.” 2017. Masters Thesis, University of Kansas. Accessed January 18, 2021. http://hdl.handle.net/1808/24146.

MLA Handbook (7th Edition):

D'Silva, Adam. “Investigation on Entropy Signature of Objects.” 2017. Web. 18 Jan 2021.

Vancouver:

D'Silva A. Investigation on Entropy Signature of Objects. [Internet] [Masters thesis]. University of Kansas; 2017. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1808/24146.

Council of Science Editors:

D'Silva A. Investigation on Entropy Signature of Objects. [Masters Thesis]. University of Kansas; 2017. Available from: http://hdl.handle.net/1808/24146


University of Kansas

6. Chandra, Yatish. Investigation of the Aerodynamic Performance of a DG808s UAS in Propeller Slipstream using Computational Fluid Dynamics.

Degree: MS, Aerospace Engineering, 2017, University of Kansas

 Unmanned Aerial Systems (UASs) are relatively affordable and immediately available compared to commercial aircraft. Hence, their aerodynamics and design accuracies are often based on extrapolating… (more)

Subjects/Keywords: Aerospace engineering; Aerodynamics; CFD; DG808s; Downwash; Sidewash; UAS

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APA (6th Edition):

Chandra, Y. (2017). Investigation of the Aerodynamic Performance of a DG808s UAS in Propeller Slipstream using Computational Fluid Dynamics. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/25935

Chicago Manual of Style (16th Edition):

Chandra, Yatish. “Investigation of the Aerodynamic Performance of a DG808s UAS in Propeller Slipstream using Computational Fluid Dynamics.” 2017. Masters Thesis, University of Kansas. Accessed January 18, 2021. http://hdl.handle.net/1808/25935.

MLA Handbook (7th Edition):

Chandra, Yatish. “Investigation of the Aerodynamic Performance of a DG808s UAS in Propeller Slipstream using Computational Fluid Dynamics.” 2017. Web. 18 Jan 2021.

Vancouver:

Chandra Y. Investigation of the Aerodynamic Performance of a DG808s UAS in Propeller Slipstream using Computational Fluid Dynamics. [Internet] [Masters thesis]. University of Kansas; 2017. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1808/25935.

Council of Science Editors:

Chandra Y. Investigation of the Aerodynamic Performance of a DG808s UAS in Propeller Slipstream using Computational Fluid Dynamics. [Masters Thesis]. University of Kansas; 2017. Available from: http://hdl.handle.net/1808/25935


University of Kansas

7. Wei, Zhenglun. Numerical and theoretical study of flapping airfoil aerodynamics using a parallelized immersed-boundary method.

Degree: PhD, Aerospace Engineering, 2014, University of Kansas

 Flight has fascinated humans for centuries. Human inventions such as missiles, aircraft , unmanned aerial vehicles (UAV), and micro air vehicle (MAV) are inspired by… (more)

Subjects/Keywords: Aerospace engineering; Mechanical engineering

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APA (6th Edition):

Wei, Z. (2014). Numerical and theoretical study of flapping airfoil aerodynamics using a parallelized immersed-boundary method. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/19600

Chicago Manual of Style (16th Edition):

Wei, Zhenglun. “Numerical and theoretical study of flapping airfoil aerodynamics using a parallelized immersed-boundary method.” 2014. Doctoral Dissertation, University of Kansas. Accessed January 18, 2021. http://hdl.handle.net/1808/19600.

MLA Handbook (7th Edition):

Wei, Zhenglun. “Numerical and theoretical study of flapping airfoil aerodynamics using a parallelized immersed-boundary method.” 2014. Web. 18 Jan 2021.

Vancouver:

Wei Z. Numerical and theoretical study of flapping airfoil aerodynamics using a parallelized immersed-boundary method. [Internet] [Doctoral dissertation]. University of Kansas; 2014. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1808/19600.

Council of Science Editors:

Wei Z. Numerical and theoretical study of flapping airfoil aerodynamics using a parallelized immersed-boundary method. [Doctoral Dissertation]. University of Kansas; 2014. Available from: http://hdl.handle.net/1808/19600


University of Kansas

8. Stastny, Thomas James. Collision Avoidance for Fixed-Wing Unmanned Aerial Systems Using Morphing Potential Field Navigation with Robust and Predictive Control.

Degree: MS, Aerospace Engineering, 2014, University of Kansas

 The vast utility of unmanned aerial systems in wide-ranging applications, whether civil, militaristic, or academic, has accelerated the prospect of integration into civil airspace, and… (more)

Subjects/Keywords: Aerospace engineering; Artificial Potential Field; Collision Avoidance; Path Planning; Real-time; Robust Control; UAS

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APA (6th Edition):

Stastny, T. J. (2014). Collision Avoidance for Fixed-Wing Unmanned Aerial Systems Using Morphing Potential Field Navigation with Robust and Predictive Control. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/19613

Chicago Manual of Style (16th Edition):

Stastny, Thomas James. “Collision Avoidance for Fixed-Wing Unmanned Aerial Systems Using Morphing Potential Field Navigation with Robust and Predictive Control.” 2014. Masters Thesis, University of Kansas. Accessed January 18, 2021. http://hdl.handle.net/1808/19613.

MLA Handbook (7th Edition):

Stastny, Thomas James. “Collision Avoidance for Fixed-Wing Unmanned Aerial Systems Using Morphing Potential Field Navigation with Robust and Predictive Control.” 2014. Web. 18 Jan 2021.

Vancouver:

Stastny TJ. Collision Avoidance for Fixed-Wing Unmanned Aerial Systems Using Morphing Potential Field Navigation with Robust and Predictive Control. [Internet] [Masters thesis]. University of Kansas; 2014. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1808/19613.

Council of Science Editors:

Stastny TJ. Collision Avoidance for Fixed-Wing Unmanned Aerial Systems Using Morphing Potential Field Navigation with Robust and Predictive Control. [Masters Thesis]. University of Kansas; 2014. Available from: http://hdl.handle.net/1808/19613


University of Kansas

9. Al Aziz, Masud. Navigation for UAVs using Signals of Opportunity.

Degree: PhD, Electrical Engineering & Computer Science, 2015, University of Kansas

 The reliance of Unmanned Aerial Vehicles (UAVs) on Global Navigation Satellite System (GNSS) for autonomous operation represents a significant vulnerability to their reliable and secure… (more)

Subjects/Keywords: Electrical engineering

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APA (6th Edition):

Al Aziz, M. (2015). Navigation for UAVs using Signals of Opportunity. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/20929

Chicago Manual of Style (16th Edition):

Al Aziz, Masud. “Navigation for UAVs using Signals of Opportunity.” 2015. Doctoral Dissertation, University of Kansas. Accessed January 18, 2021. http://hdl.handle.net/1808/20929.

MLA Handbook (7th Edition):

Al Aziz, Masud. “Navigation for UAVs using Signals of Opportunity.” 2015. Web. 18 Jan 2021.

Vancouver:

Al Aziz M. Navigation for UAVs using Signals of Opportunity. [Internet] [Doctoral dissertation]. University of Kansas; 2015. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1808/20929.

Council of Science Editors:

Al Aziz M. Navigation for UAVs using Signals of Opportunity. [Doctoral Dissertation]. University of Kansas; 2015. Available from: http://hdl.handle.net/1808/20929


University of Kansas

10. Bowman, Alec Davis. Gain-Scheduled H-Infinity Control and Analysis of a Nonlinear Generic Hypersonic Vehicle.

Degree: MS, Aerospace Engineering, 2016, University of Kansas

 The concept of hypersonic flight has been around for many years. In recent years, emerging technologies and market forces have renewed latent interest in this… (more)

Subjects/Keywords: Aerospace engineering; aircraft dynamics; control theory; gain scheduling; h-infinity control; Hypersonic aircraft; robust control

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APA (6th Edition):

Bowman, A. D. (2016). Gain-Scheduled H-Infinity Control and Analysis of a Nonlinear Generic Hypersonic Vehicle. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/22339

Chicago Manual of Style (16th Edition):

Bowman, Alec Davis. “Gain-Scheduled H-Infinity Control and Analysis of a Nonlinear Generic Hypersonic Vehicle.” 2016. Masters Thesis, University of Kansas. Accessed January 18, 2021. http://hdl.handle.net/1808/22339.

MLA Handbook (7th Edition):

Bowman, Alec Davis. “Gain-Scheduled H-Infinity Control and Analysis of a Nonlinear Generic Hypersonic Vehicle.” 2016. Web. 18 Jan 2021.

Vancouver:

Bowman AD. Gain-Scheduled H-Infinity Control and Analysis of a Nonlinear Generic Hypersonic Vehicle. [Internet] [Masters thesis]. University of Kansas; 2016. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1808/22339.

Council of Science Editors:

Bowman AD. Gain-Scheduled H-Infinity Control and Analysis of a Nonlinear Generic Hypersonic Vehicle. [Masters Thesis]. University of Kansas; 2016. Available from: http://hdl.handle.net/1808/22339


University of Kansas

11. Raina, Amool A. IMPACT ON WIND TURBINE BLADE DESIGN AND AERODYNAMIC PERFORMANCE USING INTEGRAL VORTEX GENERATORS.

Degree: PhD, Aerospace Engineering, 2016, University of Kansas

 This dissertation is aimed at understanding the impact on performance, loads and cost using integral vortex generators on wind turbine blade designs. In order to… (more)

Subjects/Keywords: Aerospace engineering; Vortex generators; Wind Energy; Wind Turbines

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APA (6th Edition):

Raina, A. A. (2016). IMPACT ON WIND TURBINE BLADE DESIGN AND AERODYNAMIC PERFORMANCE USING INTEGRAL VORTEX GENERATORS. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/23513

Chicago Manual of Style (16th Edition):

Raina, Amool A. “IMPACT ON WIND TURBINE BLADE DESIGN AND AERODYNAMIC PERFORMANCE USING INTEGRAL VORTEX GENERATORS.” 2016. Doctoral Dissertation, University of Kansas. Accessed January 18, 2021. http://hdl.handle.net/1808/23513.

MLA Handbook (7th Edition):

Raina, Amool A. “IMPACT ON WIND TURBINE BLADE DESIGN AND AERODYNAMIC PERFORMANCE USING INTEGRAL VORTEX GENERATORS.” 2016. Web. 18 Jan 2021.

Vancouver:

Raina AA. IMPACT ON WIND TURBINE BLADE DESIGN AND AERODYNAMIC PERFORMANCE USING INTEGRAL VORTEX GENERATORS. [Internet] [Doctoral dissertation]. University of Kansas; 2016. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1808/23513.

Council of Science Editors:

Raina AA. IMPACT ON WIND TURBINE BLADE DESIGN AND AERODYNAMIC PERFORMANCE USING INTEGRAL VORTEX GENERATORS. [Doctoral Dissertation]. University of Kansas; 2016. Available from: http://hdl.handle.net/1808/23513

12. Underwood, Sean Christopher. Aerothermodynamics of Impingement and Film Cooling in a Gas Turbine Blade.

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

 The service life of gas turbine engine turbine blades depends on the blade’s material, service temperature and total stress. In high-performance gas turbines, film cooling… (more)

Subjects/Keywords: Aerospace engineering; Mechanical engineering; Aerothermodynamics; Film Cooling; Gas Turbine; Impingement Cooling; Propulsion; Turbine Blade Cooling

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APA (6th Edition):

Underwood, S. C. (2018). Aerothermodynamics of Impingement and Film Cooling in a Gas Turbine Blade. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/27605

Chicago Manual of Style (16th Edition):

Underwood, Sean Christopher. “Aerothermodynamics of Impingement and Film Cooling in a Gas Turbine Blade.” 2018. Doctoral Dissertation, University of Kansas. Accessed January 18, 2021. http://hdl.handle.net/1808/27605.

MLA Handbook (7th Edition):

Underwood, Sean Christopher. “Aerothermodynamics of Impingement and Film Cooling in a Gas Turbine Blade.” 2018. Web. 18 Jan 2021.

Vancouver:

Underwood SC. Aerothermodynamics of Impingement and Film Cooling in a Gas Turbine Blade. [Internet] [Doctoral dissertation]. University of Kansas; 2018. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1808/27605.

Council of Science Editors:

Underwood SC. Aerothermodynamics of Impingement and Film Cooling in a Gas Turbine Blade. [Doctoral Dissertation]. University of Kansas; 2018. Available from: http://hdl.handle.net/1808/27605


University of Kansas

13. Smith, Leslie Ann. The Effect of Pulsed Injection on Shear Layer Dynamics in a Scramjet Combustion Chamber.

Degree: PhD, Aerospace Engineering, 2015, University of Kansas

 One of the greatest problems that scramjet research faces is fuel air mixing. The residence time for a scramjet engine, or the time it takes… (more)

Subjects/Keywords: Aerospace engineering; Injector; Micro-mixing; Pulsed Injection; Scramjet; Shear Layer

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APA (6th Edition):

Smith, L. A. (2015). The Effect of Pulsed Injection on Shear Layer Dynamics in a Scramjet Combustion Chamber. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/19415

Chicago Manual of Style (16th Edition):

Smith, Leslie Ann. “The Effect of Pulsed Injection on Shear Layer Dynamics in a Scramjet Combustion Chamber.” 2015. Doctoral Dissertation, University of Kansas. Accessed January 18, 2021. http://hdl.handle.net/1808/19415.

MLA Handbook (7th Edition):

Smith, Leslie Ann. “The Effect of Pulsed Injection on Shear Layer Dynamics in a Scramjet Combustion Chamber.” 2015. Web. 18 Jan 2021.

Vancouver:

Smith LA. The Effect of Pulsed Injection on Shear Layer Dynamics in a Scramjet Combustion Chamber. [Internet] [Doctoral dissertation]. University of Kansas; 2015. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1808/19415.

Council of Science Editors:

Smith LA. The Effect of Pulsed Injection on Shear Layer Dynamics in a Scramjet Combustion Chamber. [Doctoral Dissertation]. University of Kansas; 2015. Available from: http://hdl.handle.net/1808/19415


University of Kansas

14. Kim, A Ram. Intelligent Guidance, Navigation and Control of Multi-Agent UASs with Validation and Verification.

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

 Following the exponential growth in the usage of unmanned aerial systems (UASs) across the Aerospace Industry, more intelligent and robust guidance, navigation, and control algorithms… (more)

Subjects/Keywords: Aerospace engineering; Guidance; Multi-agent; Navigation; Validation; Verification

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APA (6th Edition):

Kim, A. R. (2018). Intelligent Guidance, Navigation and Control of Multi-Agent UASs with Validation and Verification. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/27816

Chicago Manual of Style (16th Edition):

Kim, A Ram. “Intelligent Guidance, Navigation and Control of Multi-Agent UASs with Validation and Verification.” 2018. Doctoral Dissertation, University of Kansas. Accessed January 18, 2021. http://hdl.handle.net/1808/27816.

MLA Handbook (7th Edition):

Kim, A Ram. “Intelligent Guidance, Navigation and Control of Multi-Agent UASs with Validation and Verification.” 2018. Web. 18 Jan 2021.

Vancouver:

Kim AR. Intelligent Guidance, Navigation and Control of Multi-Agent UASs with Validation and Verification. [Internet] [Doctoral dissertation]. University of Kansas; 2018. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1808/27816.

Council of Science Editors:

Kim AR. Intelligent Guidance, Navigation and Control of Multi-Agent UASs with Validation and Verification. [Doctoral Dissertation]. University of Kansas; 2018. Available from: http://hdl.handle.net/1808/27816


University of Kansas

15. Yu, Yufei. An Adaptive Moving Mesh Finite Element Method and Its Application to Mathematical Models from Physical Sciences and Image Processing.

Degree: PhD, Mathematics, 2019, University of Kansas

 Moving sharp fronts are an important feature of many mathematical models from physical sciences and cause challenges in numerical computation. In order to obtain accurate… (more)

Subjects/Keywords: Applied mathematics

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APA (6th Edition):

Yu, Y. (2019). An Adaptive Moving Mesh Finite Element Method and Its Application to Mathematical Models from Physical Sciences and Image Processing. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/30071

Chicago Manual of Style (16th Edition):

Yu, Yufei. “An Adaptive Moving Mesh Finite Element Method and Its Application to Mathematical Models from Physical Sciences and Image Processing.” 2019. Doctoral Dissertation, University of Kansas. Accessed January 18, 2021. http://hdl.handle.net/1808/30071.

MLA Handbook (7th Edition):

Yu, Yufei. “An Adaptive Moving Mesh Finite Element Method and Its Application to Mathematical Models from Physical Sciences and Image Processing.” 2019. Web. 18 Jan 2021.

Vancouver:

Yu Y. An Adaptive Moving Mesh Finite Element Method and Its Application to Mathematical Models from Physical Sciences and Image Processing. [Internet] [Doctoral dissertation]. University of Kansas; 2019. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1808/30071.

Council of Science Editors:

Yu Y. An Adaptive Moving Mesh Finite Element Method and Its Application to Mathematical Models from Physical Sciences and Image Processing. [Doctoral Dissertation]. University of Kansas; 2019. Available from: http://hdl.handle.net/1808/30071

16. Smith, Nathan Allen. Optimal Lateral Guidance for Automatic Landing of a High Altitude Long Endurance Unmanned Aerial System with Crosswind Rejection.

Degree: MS, Aerospace Engineering, 2016, University of Kansas

 Unmanned aerial systems will be the dominant force in the aviation industry. Among these aircraft the use of high altitude long endurance unmanned aerial systems… (more)

Subjects/Keywords: Aerospace engineering; Crosswind; Guidance; High Altitude Long Endurance; Unmanned Aerial System

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APA (6th Edition):

Smith, N. A. (2016). Optimal Lateral Guidance for Automatic Landing of a High Altitude Long Endurance Unmanned Aerial System with Crosswind Rejection. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/22354

Chicago Manual of Style (16th Edition):

Smith, Nathan Allen. “Optimal Lateral Guidance for Automatic Landing of a High Altitude Long Endurance Unmanned Aerial System with Crosswind Rejection.” 2016. Masters Thesis, University of Kansas. Accessed January 18, 2021. http://hdl.handle.net/1808/22354.

MLA Handbook (7th Edition):

Smith, Nathan Allen. “Optimal Lateral Guidance for Automatic Landing of a High Altitude Long Endurance Unmanned Aerial System with Crosswind Rejection.” 2016. Web. 18 Jan 2021.

Vancouver:

Smith NA. Optimal Lateral Guidance for Automatic Landing of a High Altitude Long Endurance Unmanned Aerial System with Crosswind Rejection. [Internet] [Masters thesis]. University of Kansas; 2016. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1808/22354.

Council of Science Editors:

Smith NA. Optimal Lateral Guidance for Automatic Landing of a High Altitude Long Endurance Unmanned Aerial System with Crosswind Rejection. [Masters Thesis]. University of Kansas; 2016. Available from: http://hdl.handle.net/1808/22354

17. Benyamen, Hady. Stability and Control Derivatives Identification for an Unmanned Aerial Vehicle with Low Cost Sensors Using an Extended Kalman Filter Algorithm.

Degree: MS, Aerospace Engineering, 2019, University of Kansas

 Unmanned aerial systems (UASs) tend to be autonomous vehicles. Thus, they require control algorithms. More advanced control algorithms can be developed when high quality UAS… (more)

Subjects/Keywords: Aerospace engineering; Mechanical engineering; Aircraft System Identification; Extended Kalman Filter; Flight Dynamics; Stability and Control Derivatives; UAV; Unmanned Aerial Vehicle

…CFD results obtained from another UAS at the University of Kansas [18]. This… …of Kansas Flight Systems Team owns several SkyHunter aircraft that it uses for research… …the SkyHunter UAS. An image of the UAS is presented in the following figure. The University… 

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APA (6th Edition):

Benyamen, H. (2019). Stability and Control Derivatives Identification for an Unmanned Aerial Vehicle with Low Cost Sensors Using an Extended Kalman Filter Algorithm. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/29631

Chicago Manual of Style (16th Edition):

Benyamen, Hady. “Stability and Control Derivatives Identification for an Unmanned Aerial Vehicle with Low Cost Sensors Using an Extended Kalman Filter Algorithm.” 2019. Masters Thesis, University of Kansas. Accessed January 18, 2021. http://hdl.handle.net/1808/29631.

MLA Handbook (7th Edition):

Benyamen, Hady. “Stability and Control Derivatives Identification for an Unmanned Aerial Vehicle with Low Cost Sensors Using an Extended Kalman Filter Algorithm.” 2019. Web. 18 Jan 2021.

Vancouver:

Benyamen H. Stability and Control Derivatives Identification for an Unmanned Aerial Vehicle with Low Cost Sensors Using an Extended Kalman Filter Algorithm. [Internet] [Masters thesis]. University of Kansas; 2019. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1808/29631.

Council of Science Editors:

Benyamen H. Stability and Control Derivatives Identification for an Unmanned Aerial Vehicle with Low Cost Sensors Using an Extended Kalman Filter Algorithm. [Masters Thesis]. University of Kansas; 2019. Available from: http://hdl.handle.net/1808/29631

18. Mullick, Sunayan. IMPACT OF NEW CHEVRON CONFIGURATIONS ON MIXING ENHANCEMENT IN SUBSONIC JETS.

Degree: MS, Aerospace Engineering, 2017, University of Kansas

 A major contributor to the overall noise of an aircraft is jet noise – the noise generated by the gases exiting the exhaust nozzle of… (more)

Subjects/Keywords: Aerospace engineering

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APA (6th Edition):

Mullick, S. (2017). IMPACT OF NEW CHEVRON CONFIGURATIONS ON MIXING ENHANCEMENT IN SUBSONIC JETS. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/25896

Chicago Manual of Style (16th Edition):

Mullick, Sunayan. “IMPACT OF NEW CHEVRON CONFIGURATIONS ON MIXING ENHANCEMENT IN SUBSONIC JETS.” 2017. Masters Thesis, University of Kansas. Accessed January 18, 2021. http://hdl.handle.net/1808/25896.

MLA Handbook (7th Edition):

Mullick, Sunayan. “IMPACT OF NEW CHEVRON CONFIGURATIONS ON MIXING ENHANCEMENT IN SUBSONIC JETS.” 2017. Web. 18 Jan 2021.

Vancouver:

Mullick S. IMPACT OF NEW CHEVRON CONFIGURATIONS ON MIXING ENHANCEMENT IN SUBSONIC JETS. [Internet] [Masters thesis]. University of Kansas; 2017. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1808/25896.

Council of Science Editors:

Mullick S. IMPACT OF NEW CHEVRON CONFIGURATIONS ON MIXING ENHANCEMENT IN SUBSONIC JETS. [Masters Thesis]. University of Kansas; 2017. Available from: http://hdl.handle.net/1808/25896

19. Kolpuke, Shriniwas. Bio-inspired Navigation Algorithm for GPS Denial Modes.

Degree: MS, Aerospace Engineering, 2017, University of Kansas

 The wide use of the Global Positioning System (GPS) for navigation has been persistent for a long time. However, in today’s scenario when technologies are… (more)

Subjects/Keywords: Aerospace engineering; Bio-inspired; GPS; GPS Denial Modes; Navigation

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APA (6th Edition):

Kolpuke, S. (2017). Bio-inspired Navigation Algorithm for GPS Denial Modes. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/25760

Chicago Manual of Style (16th Edition):

Kolpuke, Shriniwas. “Bio-inspired Navigation Algorithm for GPS Denial Modes.” 2017. Masters Thesis, University of Kansas. Accessed January 18, 2021. http://hdl.handle.net/1808/25760.

MLA Handbook (7th Edition):

Kolpuke, Shriniwas. “Bio-inspired Navigation Algorithm for GPS Denial Modes.” 2017. Web. 18 Jan 2021.

Vancouver:

Kolpuke S. Bio-inspired Navigation Algorithm for GPS Denial Modes. [Internet] [Masters thesis]. University of Kansas; 2017. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1808/25760.

Council of Science Editors:

Kolpuke S. Bio-inspired Navigation Algorithm for GPS Denial Modes. [Masters Thesis]. University of Kansas; 2017. Available from: http://hdl.handle.net/1808/25760

20. Bodlak, Eric. The Design Space Exploration and Preliminary Testing of a New Class of Tailsitting Quadrotor Aircraft.

Degree: MS, Aerospace Engineering, 2016, University of Kansas

 Within the last decade, multi-rotor aircraft have become the most prevalent form of unmanned aerial vehicle (UAV), with applications in the military, commercial, and civilian… (more)

Subjects/Keywords: Aerospace engineering; aircraft; design; quadrotor; scaling; tailsitter; VTOL

…KUTRI . . . . . University of Kansas Transportation Research Institute. LFP… …projected gross weight of 10,000-12,000 pounds 11 The University of Kansas Transportation… 

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APA (6th Edition):

Bodlak, E. (2016). The Design Space Exploration and Preliminary Testing of a New Class of Tailsitting Quadrotor Aircraft. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/24135

Chicago Manual of Style (16th Edition):

Bodlak, Eric. “The Design Space Exploration and Preliminary Testing of a New Class of Tailsitting Quadrotor Aircraft.” 2016. Masters Thesis, University of Kansas. Accessed January 18, 2021. http://hdl.handle.net/1808/24135.

MLA Handbook (7th Edition):

Bodlak, Eric. “The Design Space Exploration and Preliminary Testing of a New Class of Tailsitting Quadrotor Aircraft.” 2016. Web. 18 Jan 2021.

Vancouver:

Bodlak E. The Design Space Exploration and Preliminary Testing of a New Class of Tailsitting Quadrotor Aircraft. [Internet] [Masters thesis]. University of Kansas; 2016. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1808/24135.

Council of Science Editors:

Bodlak E. The Design Space Exploration and Preliminary Testing of a New Class of Tailsitting Quadrotor Aircraft. [Masters Thesis]. University of Kansas; 2016. Available from: http://hdl.handle.net/1808/24135

21. Karwas, Alex A. An Unconditionally Stable Method for Numerically Solving Solar Sail Spacecraft Equations of Motion.

Degree: PhD, Aerospace Engineering, 2015, University of Kansas

 Solar sails use the endless supply of the Sun's radiation to propel spacecraft through space. The sails use the momentum transfer from the impinging solar… (more)

Subjects/Keywords: Aerospace engineering; Finite Element Method; Propagation; Sailcraft; Solar Sail; Spacecraft; Trajectory

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APA (6th Edition):

Karwas, A. A. (2015). An Unconditionally Stable Method for Numerically Solving Solar Sail Spacecraft Equations of Motion. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/19374

Chicago Manual of Style (16th Edition):

Karwas, Alex A. “An Unconditionally Stable Method for Numerically Solving Solar Sail Spacecraft Equations of Motion.” 2015. Doctoral Dissertation, University of Kansas. Accessed January 18, 2021. http://hdl.handle.net/1808/19374.

MLA Handbook (7th Edition):

Karwas, Alex A. “An Unconditionally Stable Method for Numerically Solving Solar Sail Spacecraft Equations of Motion.” 2015. Web. 18 Jan 2021.

Vancouver:

Karwas AA. An Unconditionally Stable Method for Numerically Solving Solar Sail Spacecraft Equations of Motion. [Internet] [Doctoral dissertation]. University of Kansas; 2015. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1808/19374.

Council of Science Editors:

Karwas AA. An Unconditionally Stable Method for Numerically Solving Solar Sail Spacecraft Equations of Motion. [Doctoral Dissertation]. University of Kansas; 2015. Available from: http://hdl.handle.net/1808/19374

22. Nimmakayala, Surya Tej. Heuristics to predict and eagerly translate code in DBTs.

Degree: PhD, Electrical Engineering & Computer Science, 2019, University of Kansas

 Dynamic Binary Translators(DBTs) have a variety of uses, like instrumentation, profiling, security, portability, etc. In order for the desired application to run with these enhanced… (more)

Subjects/Keywords: Computer science; Computer engineering; data-mining; dynamic binary translation; heuristics; startup overhead

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APA (6th Edition):

Nimmakayala, S. T. (2019). Heuristics to predict and eagerly translate code in DBTs. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/29617

Chicago Manual of Style (16th Edition):

Nimmakayala, Surya Tej. “Heuristics to predict and eagerly translate code in DBTs.” 2019. Doctoral Dissertation, University of Kansas. Accessed January 18, 2021. http://hdl.handle.net/1808/29617.

MLA Handbook (7th Edition):

Nimmakayala, Surya Tej. “Heuristics to predict and eagerly translate code in DBTs.” 2019. Web. 18 Jan 2021.

Vancouver:

Nimmakayala ST. Heuristics to predict and eagerly translate code in DBTs. [Internet] [Doctoral dissertation]. University of Kansas; 2019. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1808/29617.

Council of Science Editors:

Nimmakayala ST. Heuristics to predict and eagerly translate code in DBTs. [Doctoral Dissertation]. University of Kansas; 2019. Available from: http://hdl.handle.net/1808/29617

23. Giridhar, Rohith. Prediction of Aerodynamic Noise Generated By Wind Turbine Blades.

Degree: MS, Aerospace Engineering, 2016, University of Kansas

 The preliminary step in the computational study of mitigating the aerodynamic noise generated by wind turbine blades involves accurate prediction of aerodynamic noise generated by… (more)

Subjects/Keywords: Aerospace engineering; Aero acoustics; Aerodynamic Noise; Curle; NREL Phase VI; SST k-omega; Wind Turbine Noise

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APA (6th Edition):

Giridhar, R. (2016). Prediction of Aerodynamic Noise Generated By Wind Turbine Blades. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/21976

Chicago Manual of Style (16th Edition):

Giridhar, Rohith. “Prediction of Aerodynamic Noise Generated By Wind Turbine Blades.” 2016. Masters Thesis, University of Kansas. Accessed January 18, 2021. http://hdl.handle.net/1808/21976.

MLA Handbook (7th Edition):

Giridhar, Rohith. “Prediction of Aerodynamic Noise Generated By Wind Turbine Blades.” 2016. Web. 18 Jan 2021.

Vancouver:

Giridhar R. Prediction of Aerodynamic Noise Generated By Wind Turbine Blades. [Internet] [Masters thesis]. University of Kansas; 2016. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1808/21976.

Council of Science Editors:

Giridhar R. Prediction of Aerodynamic Noise Generated By Wind Turbine Blades. [Masters Thesis]. University of Kansas; 2016. Available from: http://hdl.handle.net/1808/21976

24. Sizemore, Alex. Improved Atmospheric Density Estimation and Characterization of Uncertainty.

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

 Precise knowledge of the density in the upper atmosphere is a vital component of the orbit determination process for low Earth orbit, as inaccuracies in… (more)

Subjects/Keywords: Aerospace engineering

…Los Alamos and The University of Kansas as presented in McLaughlin et. al. [3]… 

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APA (6th Edition):

Sizemore, A. (2018). Improved Atmospheric Density Estimation and Characterization of Uncertainty. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/27610

Chicago Manual of Style (16th Edition):

Sizemore, Alex. “Improved Atmospheric Density Estimation and Characterization of Uncertainty.” 2018. Doctoral Dissertation, University of Kansas. Accessed January 18, 2021. http://hdl.handle.net/1808/27610.

MLA Handbook (7th Edition):

Sizemore, Alex. “Improved Atmospheric Density Estimation and Characterization of Uncertainty.” 2018. Web. 18 Jan 2021.

Vancouver:

Sizemore A. Improved Atmospheric Density Estimation and Characterization of Uncertainty. [Internet] [Doctoral dissertation]. University of Kansas; 2018. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1808/27610.

Council of Science Editors:

Sizemore A. Improved Atmospheric Density Estimation and Characterization of Uncertainty. [Doctoral Dissertation]. University of Kansas; 2018. Available from: http://hdl.handle.net/1808/27610

25. Rahmaninezhad, Seyed Mustapha Mustapha. Geosynthetic-Reinforced Retaining Walls with Flexible Facing Subjected to Footing Loading.

Degree: PhD, Civil, Environmental & Architectural Engineering, 2019, University of Kansas

 Geosynthetic-reinforced retaining (GRR) walls have been used as bridge abutments to support shallow foundations. This technology eliminates the need for traditional deep foundations, such as… (more)

Subjects/Keywords: Civil engineering; Gender studies; Abutment; Bridge; Geosynthetic; Retaining Wall

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APA (6th Edition):

Rahmaninezhad, S. M. M. (2019). Geosynthetic-Reinforced Retaining Walls with Flexible Facing Subjected to Footing Loading. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/29690

Chicago Manual of Style (16th Edition):

Rahmaninezhad, Seyed Mustapha Mustapha. “Geosynthetic-Reinforced Retaining Walls with Flexible Facing Subjected to Footing Loading.” 2019. Doctoral Dissertation, University of Kansas. Accessed January 18, 2021. http://hdl.handle.net/1808/29690.

MLA Handbook (7th Edition):

Rahmaninezhad, Seyed Mustapha Mustapha. “Geosynthetic-Reinforced Retaining Walls with Flexible Facing Subjected to Footing Loading.” 2019. Web. 18 Jan 2021.

Vancouver:

Rahmaninezhad SMM. Geosynthetic-Reinforced Retaining Walls with Flexible Facing Subjected to Footing Loading. [Internet] [Doctoral dissertation]. University of Kansas; 2019. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1808/29690.

Council of Science Editors:

Rahmaninezhad SMM. Geosynthetic-Reinforced Retaining Walls with Flexible Facing Subjected to Footing Loading. [Doctoral Dissertation]. University of Kansas; 2019. Available from: http://hdl.handle.net/1808/29690

26. Legursky, Katrina. System Identification and the Modeling of Sailing Yachts.

Degree: PhD, Aerospace Engineering, 2013, University of Kansas

 This research represents an exploration of sailing yacht dynamics with full-scale sailing motion data, physics-based models, and system identification techniques. The goal is to provide… (more)

Subjects/Keywords: Aerospace engineering; Ocean engineering; Autonomous sailboat; Full-scale data; One-shot least squares; Sailing yacht dynamics; System identification; Yacht modeling

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APA (6th Edition):

Legursky, K. (2013). System Identification and the Modeling of Sailing Yachts. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/14198

Chicago Manual of Style (16th Edition):

Legursky, Katrina. “System Identification and the Modeling of Sailing Yachts.” 2013. Doctoral Dissertation, University of Kansas. Accessed January 18, 2021. http://hdl.handle.net/1808/14198.

MLA Handbook (7th Edition):

Legursky, Katrina. “System Identification and the Modeling of Sailing Yachts.” 2013. Web. 18 Jan 2021.

Vancouver:

Legursky K. System Identification and the Modeling of Sailing Yachts. [Internet] [Doctoral dissertation]. University of Kansas; 2013. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1808/14198.

Council of Science Editors:

Legursky K. System Identification and the Modeling of Sailing Yachts. [Doctoral Dissertation]. University of Kansas; 2013. Available from: http://hdl.handle.net/1808/14198

.