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You searched for +publisher:"University of Kansas" +contributor:("Taghavi, Ray"). Showing records 1 – 30 of 56 total matches.

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University of Kansas

1. Lee, Ken Thye. An Analytical and Experimental Investigation of Potential Mechanical Work Extraction from Supersonic Jet Flow on High Speed Mini Turbines.

Degree: MS, Aerospace Engineering, 2010, University of Kansas

 In the present study, an inexpensive method of mechanical power extraction from supersonic jets was investigated. Detailed experiments were carried out to measure the mechanical… (more)

Subjects/Keywords: Aerospace engineering; Mechanical engineering; Kinetic energy; Mechanical work extraction; Microjets; Mini turbines; Sonic underexpanded nozzle; Supersonic flow

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APA (6th Edition):

Lee, K. T. (2010). An Analytical and Experimental Investigation of Potential Mechanical Work Extraction from Supersonic Jet Flow on High Speed Mini Turbines. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/6019

Chicago Manual of Style (16th Edition):

Lee, Ken Thye. “An Analytical and Experimental Investigation of Potential Mechanical Work Extraction from Supersonic Jet Flow on High Speed Mini Turbines.” 2010. Masters Thesis, University of Kansas. Accessed October 18, 2019. http://hdl.handle.net/1808/6019.

MLA Handbook (7th Edition):

Lee, Ken Thye. “An Analytical and Experimental Investigation of Potential Mechanical Work Extraction from Supersonic Jet Flow on High Speed Mini Turbines.” 2010. Web. 18 Oct 2019.

Vancouver:

Lee KT. An Analytical and Experimental Investigation of Potential Mechanical Work Extraction from Supersonic Jet Flow on High Speed Mini Turbines. [Internet] [Masters thesis]. University of Kansas; 2010. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1808/6019.

Council of Science Editors:

Lee KT. An Analytical and Experimental Investigation of Potential Mechanical Work Extraction from Supersonic Jet Flow on High Speed Mini Turbines. [Masters Thesis]. University of Kansas; 2010. Available from: http://hdl.handle.net/1808/6019


University of Kansas

2. Tourani, Chandraprakash Chandra. COMPUTATIONAL SIMULATION OF SCRAMJET COMBUSTORS - A COMPARISON BETWEEN QUASI-ONE DIMENSIONAL AND 2-D NUMERICAL SIMULATIONS.

Degree: MS, Aerospace Engineering, 2011, University of Kansas

 1-D simulations based on the quasi-one-dimensional equations of fluid motion plus an ignition delay model and 2-D numerical simulations based on Reynolds-Averaged Navier-Stokes (RANS) equations… (more)

Subjects/Keywords: Aerospace engineering; Air-breathing propulsion; Combustor; Hypersonic; Quasi one-dimensional; Scramjet

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APA (6th Edition):

Tourani, C. C. (2011). COMPUTATIONAL SIMULATION OF SCRAMJET COMBUSTORS - A COMPARISON BETWEEN QUASI-ONE DIMENSIONAL AND 2-D NUMERICAL SIMULATIONS. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/7635

Chicago Manual of Style (16th Edition):

Tourani, Chandraprakash Chandra. “COMPUTATIONAL SIMULATION OF SCRAMJET COMBUSTORS - A COMPARISON BETWEEN QUASI-ONE DIMENSIONAL AND 2-D NUMERICAL SIMULATIONS.” 2011. Masters Thesis, University of Kansas. Accessed October 18, 2019. http://hdl.handle.net/1808/7635.

MLA Handbook (7th Edition):

Tourani, Chandraprakash Chandra. “COMPUTATIONAL SIMULATION OF SCRAMJET COMBUSTORS - A COMPARISON BETWEEN QUASI-ONE DIMENSIONAL AND 2-D NUMERICAL SIMULATIONS.” 2011. Web. 18 Oct 2019.

Vancouver:

Tourani CC. COMPUTATIONAL SIMULATION OF SCRAMJET COMBUSTORS - A COMPARISON BETWEEN QUASI-ONE DIMENSIONAL AND 2-D NUMERICAL SIMULATIONS. [Internet] [Masters thesis]. University of Kansas; 2011. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1808/7635.

Council of Science Editors:

Tourani CC. COMPUTATIONAL SIMULATION OF SCRAMJET COMBUSTORS - A COMPARISON BETWEEN QUASI-ONE DIMENSIONAL AND 2-D NUMERICAL SIMULATIONS. [Masters Thesis]. University of Kansas; 2011. Available from: http://hdl.handle.net/1808/7635


University of Kansas

3. Carroll, Jonathan. Diffuser Augmented Wind Turbine Analysis Code.

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

 Wind Energy is becoming a significant source of energy throughout the world. This ever increasing field will potentially reach the limit of availability and practicality… (more)

Subjects/Keywords: Aerospace engineering; Aerodynamic analysis; Dawt; Diffuser augmented wind turbine; Shrouded wind turbine; Wind turbine

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APA (6th Edition):

Carroll, J. (2014). Diffuser Augmented Wind Turbine Analysis Code. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/14597

Chicago Manual of Style (16th Edition):

Carroll, Jonathan. “Diffuser Augmented Wind Turbine Analysis Code.” 2014. Masters Thesis, University of Kansas. Accessed October 18, 2019. http://hdl.handle.net/1808/14597.

MLA Handbook (7th Edition):

Carroll, Jonathan. “Diffuser Augmented Wind Turbine Analysis Code.” 2014. Web. 18 Oct 2019.

Vancouver:

Carroll J. Diffuser Augmented Wind Turbine Analysis Code. [Internet] [Masters thesis]. University of Kansas; 2014. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1808/14597.

Council of Science Editors:

Carroll J. Diffuser Augmented Wind Turbine Analysis Code. [Masters Thesis]. University of Kansas; 2014. Available from: http://hdl.handle.net/1808/14597


University of Kansas

4. Schueler, Samantha Katelyn. A Study in Aircraft Efficiency Enhancements via Prandtl-Tailored Dynamically Aerocompliant Wingtip Extensions.

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

 In 2008, the commercial aerospace industry saw substantial reductions in aircraft operating hours because of the struggling economy and high operating costs. Recurring fuel costs… (more)

Subjects/Keywords: Aerospace engineering; Adaptive structures; Wing design

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APA (6th Edition):

Schueler, S. K. (2014). A Study in Aircraft Efficiency Enhancements via Prandtl-Tailored Dynamically Aerocompliant Wingtip Extensions. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/19593

Chicago Manual of Style (16th Edition):

Schueler, Samantha Katelyn. “A Study in Aircraft Efficiency Enhancements via Prandtl-Tailored Dynamically Aerocompliant Wingtip Extensions.” 2014. Masters Thesis, University of Kansas. Accessed October 18, 2019. http://hdl.handle.net/1808/19593.

MLA Handbook (7th Edition):

Schueler, Samantha Katelyn. “A Study in Aircraft Efficiency Enhancements via Prandtl-Tailored Dynamically Aerocompliant Wingtip Extensions.” 2014. Web. 18 Oct 2019.

Vancouver:

Schueler SK. A Study in Aircraft Efficiency Enhancements via Prandtl-Tailored Dynamically Aerocompliant Wingtip Extensions. [Internet] [Masters thesis]. University of Kansas; 2014. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1808/19593.

Council of Science Editors:

Schueler SK. A Study in Aircraft Efficiency Enhancements via Prandtl-Tailored Dynamically Aerocompliant Wingtip Extensions. [Masters Thesis]. University of Kansas; 2014. Available from: http://hdl.handle.net/1808/19593


University of Kansas

5. Burns, Aaron. Turbine Tip Clearance Control Using Fluidic Oscillators.

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

 This study investigates the impact to power generation and efficiency by injecting flow into the tip clearance region of a gas turbine rotor. New to… (more)

Subjects/Keywords: Aerospace engineering; Fluidic Oscillator; Tip Clearance Control; Tip Clearance Loss; Turbine

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APA (6th Edition):

Burns, A. (2015). Turbine Tip Clearance Control Using Fluidic Oscillators. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/19426

Chicago Manual of Style (16th Edition):

Burns, Aaron. “Turbine Tip Clearance Control Using Fluidic Oscillators.” 2015. Masters Thesis, University of Kansas. Accessed October 18, 2019. http://hdl.handle.net/1808/19426.

MLA Handbook (7th Edition):

Burns, Aaron. “Turbine Tip Clearance Control Using Fluidic Oscillators.” 2015. Web. 18 Oct 2019.

Vancouver:

Burns A. Turbine Tip Clearance Control Using Fluidic Oscillators. [Internet] [Masters thesis]. University of Kansas; 2015. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1808/19426.

Council of Science Editors:

Burns A. Turbine Tip Clearance Control Using Fluidic Oscillators. [Masters Thesis]. University of Kansas; 2015. Available from: http://hdl.handle.net/1808/19426


University of Kansas

6. 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 October 18, 2019. 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 Oct 2019.

Vancouver:

Homsrivaranon K. Investigation of Active Flow Control on an Extremely Thick Wind Turbine Airfoil. [Internet] [Masters thesis]. University of Kansas; 2016. [cited 2019 Oct 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

7. 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 October 18, 2019. 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 Oct 2019.

Vancouver:

Lee AKC. Evaluation of Protruding Centerbody on the Novel Airdata Sensor. [Internet] [Masters thesis]. University of Kansas; 2016. [cited 2019 Oct 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

8. 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 October 18, 2019. 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 Oct 2019.

Vancouver:

Mullick S. IMPACT OF NEW CHEVRON CONFIGURATIONS ON MIXING ENHANCEMENT IN SUBSONIC JETS. [Internet] [Masters thesis]. University of Kansas; 2017. [cited 2019 Oct 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


University of Kansas

9. 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 October 18, 2019. 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 Oct 2019.

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 2019 Oct 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

10. 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 October 18, 2019. 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 Oct 2019.

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 2019 Oct 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

11. 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 October 18, 2019. http://hdl.handle.net/1808/24146.

MLA Handbook (7th Edition):

D'Silva, Adam. “Investigation on Entropy Signature of Objects.” 2017. Web. 18 Oct 2019.

Vancouver:

D'Silva A. Investigation on Entropy Signature of Objects. [Internet] [Masters thesis]. University of Kansas; 2017. [cited 2019 Oct 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

12. 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 October 18, 2019. http://hdl.handle.net/1808/25760.

MLA Handbook (7th Edition):

Kolpuke, Shriniwas. “Bio-inspired Navigation Algorithm for GPS Denial Modes.” 2017. Web. 18 Oct 2019.

Vancouver:

Kolpuke S. Bio-inspired Navigation Algorithm for GPS Denial Modes. [Internet] [Masters thesis]. University of Kansas; 2017. [cited 2019 Oct 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


University of Kansas

13. Valleru, Vinay. Aeroacoustic Analysis of a Wind Turbine with Sinusoidal Leading-Edge Blade.

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

 Wind turbines are a major source of renewable power generation in the U.S with a share of 4.7% in total electricity produced and is a… (more)

Subjects/Keywords: Aerospace engineering; Aeroacoustics; Bio-mimicry; CFD; NREL Phase VI; STAR CCM+; Wind Turbines

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APA (6th Edition):

Valleru, V. (2018). Aeroacoustic Analysis of a Wind Turbine with Sinusoidal Leading-Edge Blade. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/27762

Chicago Manual of Style (16th Edition):

Valleru, Vinay. “Aeroacoustic Analysis of a Wind Turbine with Sinusoidal Leading-Edge Blade.” 2018. Masters Thesis, University of Kansas. Accessed October 18, 2019. http://hdl.handle.net/1808/27762.

MLA Handbook (7th Edition):

Valleru, Vinay. “Aeroacoustic Analysis of a Wind Turbine with Sinusoidal Leading-Edge Blade.” 2018. Web. 18 Oct 2019.

Vancouver:

Valleru V. Aeroacoustic Analysis of a Wind Turbine with Sinusoidal Leading-Edge Blade. [Internet] [Masters thesis]. University of Kansas; 2018. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1808/27762.

Council of Science Editors:

Valleru V. Aeroacoustic Analysis of a Wind Turbine with Sinusoidal Leading-Edge Blade. [Masters Thesis]. University of Kansas; 2018. Available from: http://hdl.handle.net/1808/27762


University of Kansas

14. Flesberg, Sonja. Mixing Enhancement in a Scramjet Combustor Using Fuel Jet Injection Swirl.

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

 The scramjet engine has proven to be a viable means of powering a hypersonic vehicle, especially after successful flights of the X-51 WaveRider and various… (more)

Subjects/Keywords: Aerospace engineering; fuel jet injection swirl; mixing enhancement; scramjet combustion

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APA (6th Edition):

Flesberg, S. (2015). Mixing Enhancement in a Scramjet Combustor Using Fuel Jet Injection Swirl. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/19380

Chicago Manual of Style (16th Edition):

Flesberg, Sonja. “Mixing Enhancement in a Scramjet Combustor Using Fuel Jet Injection Swirl.” 2015. Doctoral Dissertation, University of Kansas. Accessed October 18, 2019. http://hdl.handle.net/1808/19380.

MLA Handbook (7th Edition):

Flesberg, Sonja. “Mixing Enhancement in a Scramjet Combustor Using Fuel Jet Injection Swirl.” 2015. Web. 18 Oct 2019.

Vancouver:

Flesberg S. Mixing Enhancement in a Scramjet Combustor Using Fuel Jet Injection Swirl. [Internet] [Doctoral dissertation]. University of Kansas; 2015. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1808/19380.

Council of Science Editors:

Flesberg S. Mixing Enhancement in a Scramjet Combustor Using Fuel Jet Injection Swirl. [Doctoral Dissertation]. University of Kansas; 2015. Available from: http://hdl.handle.net/1808/19380


University of Kansas

15. Sinn, Thomas. Development of an Adaptive Flap/Flaperon Flight Control System with Shape Memory Alloy Actuation.

Degree: MS, Aerospace Engineering, 2010, University of Kansas

 This thesis discusses the design, manufacturing and testing of a new kind of adaptive airfoil using Shape Memory Alloy (SMA) actuation. An antagonistic arrangement of… (more)

Subjects/Keywords: Aerospace engineering; Adaptive; Airfoil; Flap; Form change; Post-buckling precompressed; Shape memory alloy

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APA (6th Edition):

Sinn, T. (2010). Development of an Adaptive Flap/Flaperon Flight Control System with Shape Memory Alloy Actuation. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/6383

Chicago Manual of Style (16th Edition):

Sinn, Thomas. “Development of an Adaptive Flap/Flaperon Flight Control System with Shape Memory Alloy Actuation.” 2010. Masters Thesis, University of Kansas. Accessed October 18, 2019. http://hdl.handle.net/1808/6383.

MLA Handbook (7th Edition):

Sinn, Thomas. “Development of an Adaptive Flap/Flaperon Flight Control System with Shape Memory Alloy Actuation.” 2010. Web. 18 Oct 2019.

Vancouver:

Sinn T. Development of an Adaptive Flap/Flaperon Flight Control System with Shape Memory Alloy Actuation. [Internet] [Masters thesis]. University of Kansas; 2010. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1808/6383.

Council of Science Editors:

Sinn T. Development of an Adaptive Flap/Flaperon Flight Control System with Shape Memory Alloy Actuation. [Masters Thesis]. University of Kansas; 2010. Available from: http://hdl.handle.net/1808/6383


University of Kansas

16. Brennison, Michael Thomas. Development and Testing of A Low Cost Linear Slot Impulse Turbine.

Degree: MS, Aerospace Engineering, 2010, University of Kansas

 In this thesis, an impulse turbine with geometric characteristics aimed to have significantly lower manufacturing costs than other turbines of the similar scale was investigated.… (more)

Subjects/Keywords: Aerospace engineering; Development; Impusle; Linear; Slot; Testing; Turbine

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APA (6th Edition):

Brennison, M. T. (2010). Development and Testing of A Low Cost Linear Slot Impulse Turbine. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/6728

Chicago Manual of Style (16th Edition):

Brennison, Michael Thomas. “Development and Testing of A Low Cost Linear Slot Impulse Turbine.” 2010. Masters Thesis, University of Kansas. Accessed October 18, 2019. http://hdl.handle.net/1808/6728.

MLA Handbook (7th Edition):

Brennison, Michael Thomas. “Development and Testing of A Low Cost Linear Slot Impulse Turbine.” 2010. Web. 18 Oct 2019.

Vancouver:

Brennison MT. Development and Testing of A Low Cost Linear Slot Impulse Turbine. [Internet] [Masters thesis]. University of Kansas; 2010. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1808/6728.

Council of Science Editors:

Brennison MT. Development and Testing of A Low Cost Linear Slot Impulse Turbine. [Masters Thesis]. University of Kansas; 2010. Available from: http://hdl.handle.net/1808/6728


University of Kansas

17. Arudra, Anoop Kumar. ATMOSPHERIC DENSITY ESTIMATION USING SATELLITE PRECISION ORBIT EPHEMERIDES.

Degree: MS, Aerospace Engineering, 2011, University of Kansas

 The current atmospheric density models are not capable enough to accurately model the atmospheric density, which varies continuously in the upper atmosphere mainly due to… (more)

Subjects/Keywords: Aerospace engineering; Atmospheric density; Atmospheric density models; Orbit determination; Precision orbit ephemerides; Satellite drag; Space weather

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APA (6th Edition):

Arudra, A. K. (2011). ATMOSPHERIC DENSITY ESTIMATION USING SATELLITE PRECISION ORBIT EPHEMERIDES. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/7650

Chicago Manual of Style (16th Edition):

Arudra, Anoop Kumar. “ATMOSPHERIC DENSITY ESTIMATION USING SATELLITE PRECISION ORBIT EPHEMERIDES.” 2011. Masters Thesis, University of Kansas. Accessed October 18, 2019. http://hdl.handle.net/1808/7650.

MLA Handbook (7th Edition):

Arudra, Anoop Kumar. “ATMOSPHERIC DENSITY ESTIMATION USING SATELLITE PRECISION ORBIT EPHEMERIDES.” 2011. Web. 18 Oct 2019.

Vancouver:

Arudra AK. ATMOSPHERIC DENSITY ESTIMATION USING SATELLITE PRECISION ORBIT EPHEMERIDES. [Internet] [Masters thesis]. University of Kansas; 2011. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1808/7650.

Council of Science Editors:

Arudra AK. ATMOSPHERIC DENSITY ESTIMATION USING SATELLITE PRECISION ORBIT EPHEMERIDES. [Masters Thesis]. University of Kansas; 2011. Available from: http://hdl.handle.net/1808/7650


University of Kansas

18. Li, Wen. TIME DOMAIN SIMULATION FOR SOUND PROPAGATION OVER VARIOUS OBJECTS AND UNDER VORTICAL BACKGROUND CONDITIONS.

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

 Acoustic wave propagations have been studied for a long time with both experimental and numerical methods. Most of the analytical solutions for wave propagations are… (more)

Subjects/Keywords: Aerospace engineering

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APA (6th Edition):

Li, W. (2015). TIME DOMAIN SIMULATION FOR SOUND PROPAGATION OVER VARIOUS OBJECTS AND UNDER VORTICAL BACKGROUND CONDITIONS. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/23960

Chicago Manual of Style (16th Edition):

Li, Wen. “TIME DOMAIN SIMULATION FOR SOUND PROPAGATION OVER VARIOUS OBJECTS AND UNDER VORTICAL BACKGROUND CONDITIONS.” 2015. Masters Thesis, University of Kansas. Accessed October 18, 2019. http://hdl.handle.net/1808/23960.

MLA Handbook (7th Edition):

Li, Wen. “TIME DOMAIN SIMULATION FOR SOUND PROPAGATION OVER VARIOUS OBJECTS AND UNDER VORTICAL BACKGROUND CONDITIONS.” 2015. Web. 18 Oct 2019.

Vancouver:

Li W. TIME DOMAIN SIMULATION FOR SOUND PROPAGATION OVER VARIOUS OBJECTS AND UNDER VORTICAL BACKGROUND CONDITIONS. [Internet] [Masters thesis]. University of Kansas; 2015. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1808/23960.

Council of Science Editors:

Li W. TIME DOMAIN SIMULATION FOR SOUND PROPAGATION OVER VARIOUS OBJECTS AND UNDER VORTICAL BACKGROUND CONDITIONS. [Masters Thesis]. University of Kansas; 2015. Available from: http://hdl.handle.net/1808/23960


University of Kansas

19. Hiatt, Andrew Timothy. Deriving Atmospheric Density Estimates Using Satellite Precision Orbit Ephemerides.

Degree: MS, Aerospace Engineering, 2009, University of Kansas

 Current atmospheric models are incapable of properly modeling all of the density variations in the Earth’s upper atmosphere. Precision orbit ephemerides (POE) are utilized in… (more)

Subjects/Keywords: Aerospace engineering; Atmospheric density estimates; Champ; Grace; Orbit determination; Precision orbit ephemerides; Thermospheric and exospheric density

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APA (6th Edition):

Hiatt, A. T. (2009). Deriving Atmospheric Density Estimates Using Satellite Precision Orbit Ephemerides. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/4553

Chicago Manual of Style (16th Edition):

Hiatt, Andrew Timothy. “Deriving Atmospheric Density Estimates Using Satellite Precision Orbit Ephemerides.” 2009. Masters Thesis, University of Kansas. Accessed October 18, 2019. http://hdl.handle.net/1808/4553.

MLA Handbook (7th Edition):

Hiatt, Andrew Timothy. “Deriving Atmospheric Density Estimates Using Satellite Precision Orbit Ephemerides.” 2009. Web. 18 Oct 2019.

Vancouver:

Hiatt AT. Deriving Atmospheric Density Estimates Using Satellite Precision Orbit Ephemerides. [Internet] [Masters thesis]. University of Kansas; 2009. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1808/4553.

Council of Science Editors:

Hiatt AT. Deriving Atmospheric Density Estimates Using Satellite Precision Orbit Ephemerides. [Masters Thesis]. University of Kansas; 2009. Available from: http://hdl.handle.net/1808/4553


University of Kansas

20. LIiu, Yangliu. Vortical Flow Effects on Flow Separation Control.

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

 The effect of Reynolds number, oscillation frequency, amplitude, and the incident angle on flow separation control is studied numerically in this thesis. Two configurations are… (more)

Subjects/Keywords: Aerospace engineering; Engineering; Flow over cylinder and airfoil; Flow over tandem cylinders; Flow separation control; Vortical flow effct

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APA (6th Edition):

LIiu, Y. (2016). Vortical Flow Effects on Flow Separation Control. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/23991

Chicago Manual of Style (16th Edition):

LIiu, Yangliu. “Vortical Flow Effects on Flow Separation Control.” 2016. Masters Thesis, University of Kansas. Accessed October 18, 2019. http://hdl.handle.net/1808/23991.

MLA Handbook (7th Edition):

LIiu, Yangliu. “Vortical Flow Effects on Flow Separation Control.” 2016. Web. 18 Oct 2019.

Vancouver:

LIiu Y. Vortical Flow Effects on Flow Separation Control. [Internet] [Masters thesis]. University of Kansas; 2016. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1808/23991.

Council of Science Editors:

LIiu Y. Vortical Flow Effects on Flow Separation Control. [Masters Thesis]. University of Kansas; 2016. Available from: http://hdl.handle.net/1808/23991


University of Kansas

21. Sweeten, Benjamin Casey. CFD Analysis of UAVs using VORSTAB, FLUENT, and Advanced Aircraft Analysis Software.

Degree: MS, Aerospace Engineering, 2010, University of Kansas

 Aerodynamic analysis of three different UAVs was completed using multiple software programs. Two of the software programs were high fidelity CFD programs, and the other… (more)

Subjects/Keywords: Aerospace engineering

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APA (6th Edition):

Sweeten, B. C. (2010). CFD Analysis of UAVs using VORSTAB, FLUENT, and Advanced Aircraft Analysis Software. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/6292

Chicago Manual of Style (16th Edition):

Sweeten, Benjamin Casey. “CFD Analysis of UAVs using VORSTAB, FLUENT, and Advanced Aircraft Analysis Software.” 2010. Masters Thesis, University of Kansas. Accessed October 18, 2019. http://hdl.handle.net/1808/6292.

MLA Handbook (7th Edition):

Sweeten, Benjamin Casey. “CFD Analysis of UAVs using VORSTAB, FLUENT, and Advanced Aircraft Analysis Software.” 2010. Web. 18 Oct 2019.

Vancouver:

Sweeten BC. CFD Analysis of UAVs using VORSTAB, FLUENT, and Advanced Aircraft Analysis Software. [Internet] [Masters thesis]. University of Kansas; 2010. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1808/6292.

Council of Science Editors:

Sweeten BC. CFD Analysis of UAVs using VORSTAB, FLUENT, and Advanced Aircraft Analysis Software. [Masters Thesis]. University of Kansas; 2010. Available from: http://hdl.handle.net/1808/6292


University of Kansas

22. Hwang, Seung-Jae. Numerical Simulation of Enhanced Mixing in Scramjet Combustor Using Ramp, Tabs and Suction Collar.

Degree: PhD, Aerospace Engineering, 2011, University of Kansas

 Numerical simulations of the scramjet combustor by using the commercial CFD code Fluent with the coupled implicit method with second-order accurate discretization have been obtained… (more)

Subjects/Keywords: Aerospace engineering; Combustor; Enhanced; Mixing; Scramjet; Suction collar; Tabs

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APA (6th Edition):

Hwang, S. (2011). Numerical Simulation of Enhanced Mixing in Scramjet Combustor Using Ramp, Tabs and Suction Collar. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/8080

Chicago Manual of Style (16th Edition):

Hwang, Seung-Jae. “Numerical Simulation of Enhanced Mixing in Scramjet Combustor Using Ramp, Tabs and Suction Collar.” 2011. Doctoral Dissertation, University of Kansas. Accessed October 18, 2019. http://hdl.handle.net/1808/8080.

MLA Handbook (7th Edition):

Hwang, Seung-Jae. “Numerical Simulation of Enhanced Mixing in Scramjet Combustor Using Ramp, Tabs and Suction Collar.” 2011. Web. 18 Oct 2019.

Vancouver:

Hwang S. Numerical Simulation of Enhanced Mixing in Scramjet Combustor Using Ramp, Tabs and Suction Collar. [Internet] [Doctoral dissertation]. University of Kansas; 2011. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1808/8080.

Council of Science Editors:

Hwang S. Numerical Simulation of Enhanced Mixing in Scramjet Combustor Using Ramp, Tabs and Suction Collar. [Doctoral Dissertation]. University of Kansas; 2011. Available from: http://hdl.handle.net/1808/8080


University of Kansas

23. 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 October 18, 2019. 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 Oct 2019.

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 2019 Oct 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

24. 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 October 18, 2019. 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 Oct 2019.

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 2019 Oct 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

25. Li, Yanan. Large-eddy simulations of turbulent flows using the high-order FR/CPR method.

Degree: D.Eng., Aerospace Engineering, 2016, University of Kansas

 Large eddy simulation (LES) was originally proposed for simulating atmospheric flows and then has become one of the most successful methodologies for turbulence simulation for… (more)

Subjects/Keywords: Aerospace engineering; computational fluid dynamics; high-order numerical schemes; large-eddy simulation; shock capturing; turbulence

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APA (6th Edition):

Li, Y. (2016). Large-eddy simulations of turbulent flows using the high-order FR/CPR method. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/24138

Chicago Manual of Style (16th Edition):

Li, Yanan. “Large-eddy simulations of turbulent flows using the high-order FR/CPR method.” 2016. Doctoral Dissertation, University of Kansas. Accessed October 18, 2019. http://hdl.handle.net/1808/24138.

MLA Handbook (7th Edition):

Li, Yanan. “Large-eddy simulations of turbulent flows using the high-order FR/CPR method.” 2016. Web. 18 Oct 2019.

Vancouver:

Li Y. Large-eddy simulations of turbulent flows using the high-order FR/CPR method. [Internet] [Doctoral dissertation]. University of Kansas; 2016. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1808/24138.

Council of Science Editors:

Li Y. Large-eddy simulations of turbulent flows using the high-order FR/CPR method. [Doctoral Dissertation]. University of Kansas; 2016. Available from: http://hdl.handle.net/1808/24138


University of Kansas

26. Bramlette, Richard. Development, Modeling, Simulation, and Testing of a Novel Propane-Fueled Brayton-Gluhareff Cycle Acoustically-Pressurized Ramjet Engine.

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

 In the 1950s, Eugene Gluhareff built the first working “pressure jet” engine, a variation on the classical ramjet engine with a pressurized inlet system relying… (more)

Subjects/Keywords: Aerospace engineering; Mechanical engineering; Chemistry; Chemical Kinetics; Computational Fluid Dynamics; Jet Propulsion; Pressure Jet; Propane Oxidation; Ramjet

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APA (6th Edition):

Bramlette, R. (2016). Development, Modeling, Simulation, and Testing of a Novel Propane-Fueled Brayton-Gluhareff Cycle Acoustically-Pressurized Ramjet Engine. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/23515

Chicago Manual of Style (16th Edition):

Bramlette, Richard. “Development, Modeling, Simulation, and Testing of a Novel Propane-Fueled Brayton-Gluhareff Cycle Acoustically-Pressurized Ramjet Engine.” 2016. Doctoral Dissertation, University of Kansas. Accessed October 18, 2019. http://hdl.handle.net/1808/23515.

MLA Handbook (7th Edition):

Bramlette, Richard. “Development, Modeling, Simulation, and Testing of a Novel Propane-Fueled Brayton-Gluhareff Cycle Acoustically-Pressurized Ramjet Engine.” 2016. Web. 18 Oct 2019.

Vancouver:

Bramlette R. Development, Modeling, Simulation, and Testing of a Novel Propane-Fueled Brayton-Gluhareff Cycle Acoustically-Pressurized Ramjet Engine. [Internet] [Doctoral dissertation]. University of Kansas; 2016. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1808/23515.

Council of Science Editors:

Bramlette R. Development, Modeling, Simulation, and Testing of a Novel Propane-Fueled Brayton-Gluhareff Cycle Acoustically-Pressurized Ramjet Engine. [Doctoral Dissertation]. University of Kansas; 2016. Available from: http://hdl.handle.net/1808/23515


University of Kansas

27. Kim, Kyungpyo. Flexural Stiffnesses of and Dimensional Stability in Circular Quasi-isotropic Laminate Mirrors.

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

 Composite fiber reinforced plastics are being given favorable consideration for emerging applications in large aperture telescopes, such as the Hubble telescope or communication dishes. Many… (more)

Subjects/Keywords: Aerospace engineering; Dimensional stability in composite mirrors; Quasi-isotropic laminate mirrors; Stiffnesses in composite mirrors; Surface deformation in composite mirrors

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APA (6th Edition):

Kim, K. (2009). Flexural Stiffnesses of and Dimensional Stability in Circular Quasi-isotropic Laminate Mirrors. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/4516

Chicago Manual of Style (16th Edition):

Kim, Kyungpyo. “Flexural Stiffnesses of and Dimensional Stability in Circular Quasi-isotropic Laminate Mirrors.” 2009. Doctoral Dissertation, University of Kansas. Accessed October 18, 2019. http://hdl.handle.net/1808/4516.

MLA Handbook (7th Edition):

Kim, Kyungpyo. “Flexural Stiffnesses of and Dimensional Stability in Circular Quasi-isotropic Laminate Mirrors.” 2009. Web. 18 Oct 2019.

Vancouver:

Kim K. Flexural Stiffnesses of and Dimensional Stability in Circular Quasi-isotropic Laminate Mirrors. [Internet] [Doctoral dissertation]. University of Kansas; 2009. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1808/4516.

Council of Science Editors:

Kim K. Flexural Stiffnesses of and Dimensional Stability in Circular Quasi-isotropic Laminate Mirrors. [Doctoral Dissertation]. University of Kansas; 2009. Available from: http://hdl.handle.net/1808/4516


University of Kansas

28. Ma, Yongting. Development of mathematical models and mathematical, computational framework for multi-media interaction processes.

Degree: PhD, Mechanical Engineering, 2011, University of Kansas

 This thesis presents development of mathematical models for multi-media interaction process using Eulerian description and associated computational infrastructure to obtain numerical solution of the initial… (more)

Subjects/Keywords: Mechanical engineering; Computational framework; Finite element method; Mathematical models; Multi-media interaction processes; Rate constitutive theory; Viscous and viscoelastic flow

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APA (6th Edition):

Ma, Y. (2011). Development of mathematical models and mathematical, computational framework for multi-media interaction processes. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/7634

Chicago Manual of Style (16th Edition):

Ma, Yongting. “Development of mathematical models and mathematical, computational framework for multi-media interaction processes.” 2011. Doctoral Dissertation, University of Kansas. Accessed October 18, 2019. http://hdl.handle.net/1808/7634.

MLA Handbook (7th Edition):

Ma, Yongting. “Development of mathematical models and mathematical, computational framework for multi-media interaction processes.” 2011. Web. 18 Oct 2019.

Vancouver:

Ma Y. Development of mathematical models and mathematical, computational framework for multi-media interaction processes. [Internet] [Doctoral dissertation]. University of Kansas; 2011. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1808/7634.

Council of Science Editors:

Ma Y. Development of mathematical models and mathematical, computational framework for multi-media interaction processes. [Doctoral Dissertation]. University of Kansas; 2011. Available from: http://hdl.handle.net/1808/7634


University of Kansas

29. 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 October 18, 2019. 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 Oct 2019.

Vancouver:

Raina AA. IMPACT ON WIND TURBINE BLADE DESIGN AND AERODYNAMIC PERFORMANCE USING INTEGRAL VORTEX GENERATORS. [Internet] [Doctoral dissertation]. University of Kansas; 2016. [cited 2019 Oct 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


University of Kansas

30. Joy, Aaron D. Non-Classical Continuum Theories for Solid and Fluent Continua.

Degree: PhD, Mechanical Engineering, 2017, University of Kansas

 This dissertation presents non-classical continuum theories for solid and fluent con- tinua. In these theories additional physics due to internal rotations and rotation rates arising… (more)

Subjects/Keywords: Mechanics; Cosserat; Polar continua; rotations

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APA (6th Edition):

Joy, A. D. (2017). Non-Classical Continuum Theories for Solid and Fluent Continua. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/26353

Chicago Manual of Style (16th Edition):

Joy, Aaron D. “Non-Classical Continuum Theories for Solid and Fluent Continua.” 2017. Doctoral Dissertation, University of Kansas. Accessed October 18, 2019. http://hdl.handle.net/1808/26353.

MLA Handbook (7th Edition):

Joy, Aaron D. “Non-Classical Continuum Theories for Solid and Fluent Continua.” 2017. Web. 18 Oct 2019.

Vancouver:

Joy AD. Non-Classical Continuum Theories for Solid and Fluent Continua. [Internet] [Doctoral dissertation]. University of Kansas; 2017. [cited 2019 Oct 18]. Available from: http://hdl.handle.net/1808/26353.

Council of Science Editors:

Joy AD. Non-Classical Continuum Theories for Solid and Fluent Continua. [Doctoral Dissertation]. University of Kansas; 2017. Available from: http://hdl.handle.net/1808/26353

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