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You searched for +publisher:"University of Kansas" +contributor:("Farokhi, Saeed"). Showing records 1 – 30 of 40 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 July 15, 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. 15 Jul 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 Jul 15]. 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. Vatti, Kranthi. Damping Estimation of Plates for Statistical Energy Analysis.

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

 The Power Input Method (P.I.M.) and the Impulse Response Decay Method (I.R.D.M.) are used to evaluate how the accuracy of damping loss factor estimation for… (more)

Subjects/Keywords: Aerospace engineering; Mechanics; Acoustics; Frequency response analysis; High frequency analysis; Plate vibration; Statistical energy analysis; Vibration

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APA (6th Edition):

Vatti, K. (2011). Damping Estimation of Plates for Statistical Energy Analysis. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/7876

Chicago Manual of Style (16th Edition):

Vatti, Kranthi. “Damping Estimation of Plates for Statistical Energy Analysis.” 2011. Masters Thesis, University of Kansas. Accessed July 15, 2019. http://hdl.handle.net/1808/7876.

MLA Handbook (7th Edition):

Vatti, Kranthi. “Damping Estimation of Plates for Statistical Energy Analysis.” 2011. Web. 15 Jul 2019.

Vancouver:

Vatti K. Damping Estimation of Plates for Statistical Energy Analysis. [Internet] [Masters thesis]. University of Kansas; 2011. [cited 2019 Jul 15]. Available from: http://hdl.handle.net/1808/7876.

Council of Science Editors:

Vatti K. Damping Estimation of Plates for Statistical Energy Analysis. [Masters Thesis]. University of Kansas; 2011. Available from: http://hdl.handle.net/1808/7876


University of Kansas

3. 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 July 15, 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. 15 Jul 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 Jul 15]. 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

4. 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 July 15, 2019. http://hdl.handle.net/1808/14597.

MLA Handbook (7th Edition):

Carroll, Jonathan. “Diffuser Augmented Wind Turbine Analysis Code.” 2014. Web. 15 Jul 2019.

Vancouver:

Carroll J. Diffuser Augmented Wind Turbine Analysis Code. [Internet] [Masters thesis]. University of Kansas; 2014. [cited 2019 Jul 15]. 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

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 July 15, 2019. http://hdl.handle.net/1808/19426.

MLA Handbook (7th Edition):

Burns, Aaron. “Turbine Tip Clearance Control Using Fluidic Oscillators.” 2015. Web. 15 Jul 2019.

Vancouver:

Burns A. Turbine Tip Clearance Control Using Fluidic Oscillators. [Internet] [Masters thesis]. University of Kansas; 2015. [cited 2019 Jul 15]. 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 July 15, 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. 15 Jul 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 Jul 15]. 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 July 15, 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. 15 Jul 2019.

Vancouver:

Lee AKC. Evaluation of Protruding Centerbody on the Novel Airdata Sensor. [Internet] [Masters thesis]. University of Kansas; 2016. [cited 2019 Jul 15]. 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 July 15, 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. 15 Jul 2019.

Vancouver:

Mullick S. IMPACT OF NEW CHEVRON CONFIGURATIONS ON MIXING ENHANCEMENT IN SUBSONIC JETS. [Internet] [Masters thesis]. University of Kansas; 2017. [cited 2019 Jul 15]. 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 July 15, 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. 15 Jul 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 Jul 15]. 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 July 15, 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. 15 Jul 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 Jul 15]. 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 July 15, 2019. http://hdl.handle.net/1808/24146.

MLA Handbook (7th Edition):

D'Silva, Adam. “Investigation on Entropy Signature of Objects.” 2017. Web. 15 Jul 2019.

Vancouver:

D'Silva A. Investigation on Entropy Signature of Objects. [Internet] [Masters thesis]. University of Kansas; 2017. [cited 2019 Jul 15]. 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. 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 July 15, 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. 15 Jul 2019.

Vancouver:

Valleru V. Aeroacoustic Analysis of a Wind Turbine with Sinusoidal Leading-Edge Blade. [Internet] [Masters thesis]. University of Kansas; 2018. [cited 2019 Jul 15]. 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

13. 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 July 15, 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. 15 Jul 2019.

Vancouver:

Flesberg S. Mixing Enhancement in a Scramjet Combustor Using Fuel Jet Injection Swirl. [Internet] [Doctoral dissertation]. University of Kansas; 2015. [cited 2019 Jul 15]. 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

14. Lechtenberg, Travis Francis. DERIVATION AND OBSERVABILITY OF UPPER ATMOSPHERIC DENSITY VARIATIONS UTILIZING PRECISION ORBIT EPHEMERIDES.

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

 Several models of atmospheric density exist in today's world, yet most possess significant errors when compared to data determined from actual satellite measurements. This research… (more)

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

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APA (6th Edition):

Lechtenberg, T. F. (2010). DERIVATION AND OBSERVABILITY OF UPPER ATMOSPHERIC DENSITY VARIATIONS UTILIZING PRECISION ORBIT EPHEMERIDES. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/6295

Chicago Manual of Style (16th Edition):

Lechtenberg, Travis Francis. “DERIVATION AND OBSERVABILITY OF UPPER ATMOSPHERIC DENSITY VARIATIONS UTILIZING PRECISION ORBIT EPHEMERIDES.” 2010. Masters Thesis, University of Kansas. Accessed July 15, 2019. http://hdl.handle.net/1808/6295.

MLA Handbook (7th Edition):

Lechtenberg, Travis Francis. “DERIVATION AND OBSERVABILITY OF UPPER ATMOSPHERIC DENSITY VARIATIONS UTILIZING PRECISION ORBIT EPHEMERIDES.” 2010. Web. 15 Jul 2019.

Vancouver:

Lechtenberg TF. DERIVATION AND OBSERVABILITY OF UPPER ATMOSPHERIC DENSITY VARIATIONS UTILIZING PRECISION ORBIT EPHEMERIDES. [Internet] [Masters thesis]. University of Kansas; 2010. [cited 2019 Jul 15]. Available from: http://hdl.handle.net/1808/6295.

Council of Science Editors:

Lechtenberg TF. DERIVATION AND OBSERVABILITY OF UPPER ATMOSPHERIC DENSITY VARIATIONS UTILIZING PRECISION ORBIT EPHEMERIDES. [Masters Thesis]. University of Kansas; 2010. Available from: http://hdl.handle.net/1808/6295


University of Kansas

15. Fattig, Eric. Comparison of Precision Orbit Derived Density Estimates for CHAMP and GRACE Satellites.

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

 Current atmospheric density models cannot adequately represent the density variations observed by satellites in Low Earth Orbit (LEO). Using an optimal orbit determination process, precision… (more)

Subjects/Keywords: Aerospace engineering; Atmospheric density; Champ satellite; Grace satellites; Orbit determination; Precision orbit data; Solar and geomagnetic activity

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APA (6th Edition):

Fattig, E. (2011). Comparison of Precision Orbit Derived Density Estimates for CHAMP and GRACE Satellites. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/7653

Chicago Manual of Style (16th Edition):

Fattig, Eric. “Comparison of Precision Orbit Derived Density Estimates for CHAMP and GRACE Satellites.” 2011. Masters Thesis, University of Kansas. Accessed July 15, 2019. http://hdl.handle.net/1808/7653.

MLA Handbook (7th Edition):

Fattig, Eric. “Comparison of Precision Orbit Derived Density Estimates for CHAMP and GRACE Satellites.” 2011. Web. 15 Jul 2019.

Vancouver:

Fattig E. Comparison of Precision Orbit Derived Density Estimates for CHAMP and GRACE Satellites. [Internet] [Masters thesis]. University of Kansas; 2011. [cited 2019 Jul 15]. Available from: http://hdl.handle.net/1808/7653.

Council of Science Editors:

Fattig E. Comparison of Precision Orbit Derived Density Estimates for CHAMP and GRACE Satellites. [Masters Thesis]. University of Kansas; 2011. Available from: http://hdl.handle.net/1808/7653


University of Kansas

16. 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 July 15, 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. 15 Jul 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 Jul 15]. 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

17. 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 July 15, 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. 15 Jul 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 Jul 15]. 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

18. 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 July 15, 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. 15 Jul 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 Jul 15]. 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

19. 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 July 15, 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. 15 Jul 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 Jul 15]. 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

20. 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 July 15, 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. 15 Jul 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 Jul 15]. 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

21. 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 July 15, 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. 15 Jul 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 Jul 15]. 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

22. 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 July 15, 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. 15 Jul 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 Jul 15]. 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

23. Dande, Himanshu Amol. Panel Damping Loss Factor Estimation Using The Random Decrement Technique.

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

 The use of the Random Decrement Technique (RDT) for estimating panel damping loss factors ranging from 1% to 10% is examined in a systematic way,… (more)

Subjects/Keywords: Aerospace engineering; Frequency domain filtering; Impulse response decay method irdm; Random decrement technique; Time domain filtering; Triggering scheme

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APA (6th Edition):

Dande, H. A. (2010). Panel Damping Loss Factor Estimation Using The Random Decrement Technique. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/7752

Chicago Manual of Style (16th Edition):

Dande, Himanshu Amol. “Panel Damping Loss Factor Estimation Using The Random Decrement Technique.” 2010. Masters Thesis, University of Kansas. Accessed July 15, 2019. http://hdl.handle.net/1808/7752.

MLA Handbook (7th Edition):

Dande, Himanshu Amol. “Panel Damping Loss Factor Estimation Using The Random Decrement Technique.” 2010. Web. 15 Jul 2019.

Vancouver:

Dande HA. Panel Damping Loss Factor Estimation Using The Random Decrement Technique. [Internet] [Masters thesis]. University of Kansas; 2010. [cited 2019 Jul 15]. Available from: http://hdl.handle.net/1808/7752.

Council of Science Editors:

Dande HA. Panel Damping Loss Factor Estimation Using The Random Decrement Technique. [Masters Thesis]. University of Kansas; 2010. Available from: http://hdl.handle.net/1808/7752


University of Kansas

24. 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 July 15, 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. 15 Jul 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 Jul 15]. 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

25. 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 July 15, 2019. 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. 15 Jul 2019.

Vancouver:

Underwood SC. Aerothermodynamics of Impingement and Film Cooling in a Gas Turbine Blade. [Internet] [Doctoral dissertation]. University of Kansas; 2018. [cited 2019 Jul 15]. 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

26. 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 July 15, 2019. 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. 15 Jul 2019.

Vancouver:

Kim AR. Intelligent Guidance, Navigation and Control of Multi-Agent UASs with Validation and Verification. [Internet] [Doctoral dissertation]. University of Kansas; 2018. [cited 2019 Jul 15]. 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

27. Jin, Wonjin. A Computational Study of Icing Effects on the Performance of an S-Duct Inlet.

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

 The performance of a diffusing S-duct inlet (M2129) is computationally studied for the effects of inlet icing. Different ice accretion shapes, predicted by numerical analysis… (more)

Subjects/Keywords: Aerospace engineering; Mechanical engineering; Diffusing s-duct; Dynamic distortion; Icing; Inlet; Temperature distortion; Total pressure distortion

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APA (6th Edition):

Jin, W. (2009). A Computational Study of Icing Effects on the Performance of an S-Duct Inlet. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/5242

Chicago Manual of Style (16th Edition):

Jin, Wonjin. “A Computational Study of Icing Effects on the Performance of an S-Duct Inlet.” 2009. Doctoral Dissertation, University of Kansas. Accessed July 15, 2019. http://hdl.handle.net/1808/5242.

MLA Handbook (7th Edition):

Jin, Wonjin. “A Computational Study of Icing Effects on the Performance of an S-Duct Inlet.” 2009. Web. 15 Jul 2019.

Vancouver:

Jin W. A Computational Study of Icing Effects on the Performance of an S-Duct Inlet. [Internet] [Doctoral dissertation]. University of Kansas; 2009. [cited 2019 Jul 15]. Available from: http://hdl.handle.net/1808/5242.

Council of Science Editors:

Jin W. A Computational Study of Icing Effects on the Performance of an S-Duct Inlet. [Doctoral Dissertation]. University of Kansas; 2009. Available from: http://hdl.handle.net/1808/5242


University of Kansas

28. Shi, Lei. Adaptive High-Order Differential Formulation for the Compressible Navier-Stokes Equations.

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

 High-order methods have the potential to achieve higher accuracy at lower cost than lower order methods. This potential has been demonstrated conclusively for smooth problems… (more)

Subjects/Keywords: Aerospace engineering; Adaptive Method; Adjoint-based Adaptation; Computational Fluid Dynamics; High-order Method; Navier-Stokes Equations

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APA (6th Edition):

Shi, L. (2014). Adaptive High-Order Differential Formulation for the Compressible Navier-Stokes Equations. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/27533

Chicago Manual of Style (16th Edition):

Shi, Lei. “Adaptive High-Order Differential Formulation for the Compressible Navier-Stokes Equations.” 2014. Doctoral Dissertation, University of Kansas. Accessed July 15, 2019. http://hdl.handle.net/1808/27533.

MLA Handbook (7th Edition):

Shi, Lei. “Adaptive High-Order Differential Formulation for the Compressible Navier-Stokes Equations.” 2014. Web. 15 Jul 2019.

Vancouver:

Shi L. Adaptive High-Order Differential Formulation for the Compressible Navier-Stokes Equations. [Internet] [Doctoral dissertation]. University of Kansas; 2014. [cited 2019 Jul 15]. Available from: http://hdl.handle.net/1808/27533.

Council of Science Editors:

Shi L. Adaptive High-Order Differential Formulation for the Compressible Navier-Stokes Equations. [Doctoral Dissertation]. University of Kansas; 2014. Available from: http://hdl.handle.net/1808/27533

29. Kulhanek, Sarah Logan. Design, Analysis, and Simulation of Rocket Propulsion System.

Degree: MS, Aerospace Engineering, 2012, University of Kansas

 This document details the functionality of a software program used to streamline a rocket propulsion system design, analysis and simulation effort. The program aids in… (more)

Subjects/Keywords: Aerospace engineering; Design; Program; Propulsion system; Rocket

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APA (6th Edition):

Kulhanek, S. L. (2012). Design, Analysis, and Simulation of Rocket Propulsion System. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/10198

Chicago Manual of Style (16th Edition):

Kulhanek, Sarah Logan. “Design, Analysis, and Simulation of Rocket Propulsion System.” 2012. Masters Thesis, University of Kansas. Accessed July 15, 2019. http://hdl.handle.net/1808/10198.

MLA Handbook (7th Edition):

Kulhanek, Sarah Logan. “Design, Analysis, and Simulation of Rocket Propulsion System.” 2012. Web. 15 Jul 2019.

Vancouver:

Kulhanek SL. Design, Analysis, and Simulation of Rocket Propulsion System. [Internet] [Masters thesis]. University of Kansas; 2012. [cited 2019 Jul 15]. Available from: http://hdl.handle.net/1808/10198.

Council of Science Editors:

Kulhanek SL. Design, Analysis, and Simulation of Rocket Propulsion System. [Masters Thesis]. University of Kansas; 2012. Available from: http://hdl.handle.net/1808/10198

30. 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 July 15, 2019. http://hdl.handle.net/1808/21976.

MLA Handbook (7th Edition):

Giridhar, Rohith. “Prediction of Aerodynamic Noise Generated By Wind Turbine Blades.” 2016. Web. 15 Jul 2019.

Vancouver:

Giridhar R. Prediction of Aerodynamic Noise Generated By Wind Turbine Blades. [Internet] [Masters thesis]. University of Kansas; 2016. [cited 2019 Jul 15]. 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

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