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You searched for +publisher:"University of Kansas" +contributor:("Hale, Richard"). Showing records 1 – 30 of 31 total matches.

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University of Kansas

1. 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 January 22, 2021. http://hdl.handle.net/1808/7876.

MLA Handbook (7th Edition):

Vatti, Kranthi. “Damping Estimation of Plates for Statistical Energy Analysis.” 2011. Web. 22 Jan 2021.

Vancouver:

Vatti K. Damping Estimation of Plates for Statistical Energy Analysis. [Internet] [Masters thesis]. University of Kansas; 2011. [cited 2021 Jan 22]. 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

2. Katipally, Akhilesh Chandra Reddy. DAMPING ESTIMATION OF PLATES JOINED AT A POINT USING STATISTICAL ENERGY ANALYSIS.

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

 The loss factors and coupling loss factors of a 2-plate, coupled system were estimated using the Statistical Energy Analysis methodology. In particular the Power Input… (more)

Subjects/Keywords: Aerospace engineering; Damping; Frequency resolution; Negative loss factors; Power input method; Statistical energy analysis; Transient sea

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APA (6th Edition):

Katipally, A. C. R. (2011). DAMPING ESTIMATION OF PLATES JOINED AT A POINT USING STATISTICAL ENERGY ANALYSIS. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/8141

Chicago Manual of Style (16th Edition):

Katipally, Akhilesh Chandra Reddy. “DAMPING ESTIMATION OF PLATES JOINED AT A POINT USING STATISTICAL ENERGY ANALYSIS.” 2011. Masters Thesis, University of Kansas. Accessed January 22, 2021. http://hdl.handle.net/1808/8141.

MLA Handbook (7th Edition):

Katipally, Akhilesh Chandra Reddy. “DAMPING ESTIMATION OF PLATES JOINED AT A POINT USING STATISTICAL ENERGY ANALYSIS.” 2011. Web. 22 Jan 2021.

Vancouver:

Katipally ACR. DAMPING ESTIMATION OF PLATES JOINED AT A POINT USING STATISTICAL ENERGY ANALYSIS. [Internet] [Masters thesis]. University of Kansas; 2011. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1808/8141.

Council of Science Editors:

Katipally ACR. DAMPING ESTIMATION OF PLATES JOINED AT A POINT USING STATISTICAL ENERGY ANALYSIS. [Masters Thesis]. University of Kansas; 2011. Available from: http://hdl.handle.net/1808/8141


University of Kansas

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

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

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Lykins, Ryan. “Unsteady Aerodynamic and Dynamic Analysis of the Meridian UAS in a Rolling-Yawing Motion.” 2014. Masters Thesis, University of Kansas. Accessed January 22, 2021. http://hdl.handle.net/1808/14605.

MLA Handbook (7th Edition):

Lykins, Ryan. “Unsteady Aerodynamic and Dynamic Analysis of the Meridian UAS in a Rolling-Yawing Motion.” 2014. Web. 22 Jan 2021.

Vancouver:

Lykins R. Unsteady Aerodynamic and Dynamic Analysis of the Meridian UAS in a Rolling-Yawing Motion. [Internet] [Masters thesis]. University of Kansas; 2014. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1808/14605.

Council of Science Editors:

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


University of Kansas

4. Patil, Ankur Santaji. An Improved Gain Wing-Integrated Antenna Design for Meridian UAS and Sensor-Driven Wing Sizing Approach.

Degree: M.E., Aerospace Engineering, 2017, University of Kansas

 Ice sheets in Antarctic and Arctic regions are undergoing rapid changes, causing a rise in sea level with direct impacts on society and the global… (more)

Subjects/Keywords: Aerospace engineering

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APA (6th Edition):

Patil, A. S. (2017). An Improved Gain Wing-Integrated Antenna Design for Meridian UAS and Sensor-Driven Wing Sizing Approach. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/25863

Chicago Manual of Style (16th Edition):

Patil, Ankur Santaji. “An Improved Gain Wing-Integrated Antenna Design for Meridian UAS and Sensor-Driven Wing Sizing Approach.” 2017. Masters Thesis, University of Kansas. Accessed January 22, 2021. http://hdl.handle.net/1808/25863.

MLA Handbook (7th Edition):

Patil, Ankur Santaji. “An Improved Gain Wing-Integrated Antenna Design for Meridian UAS and Sensor-Driven Wing Sizing Approach.” 2017. Web. 22 Jan 2021.

Vancouver:

Patil AS. An Improved Gain Wing-Integrated Antenna Design for Meridian UAS and Sensor-Driven Wing Sizing Approach. [Internet] [Masters thesis]. University of Kansas; 2017. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1808/25863.

Council of Science Editors:

Patil AS. An Improved Gain Wing-Integrated Antenna Design for Meridian UAS and Sensor-Driven Wing Sizing Approach. [Masters Thesis]. University of Kansas; 2017. Available from: http://hdl.handle.net/1808/25863


University of Kansas

5. Brown, Kenneth Dewayne. A Mobile Wireless Channel State Recognition Algorihm: Introduction, Definition, and Verification - Sensing for Cognitive Environmental Awareness.

Degree: PhD, Electrical Engineering & Computer Science, 2013, University of Kansas

 This research includes mobile wireless systems limited by time and frequency dispersive channels. A blind mobile wireless channel (MWC) state recognition (CSR) algorithm that detects… (more)

Subjects/Keywords: Electrical engineering; Hidden Markov model; Mobile wireless channel state estimation; Mobile wireless channel state model; Mobile wireless channel state recognition; Mobile wireless channel state recognition algorithhm

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APA (6th Edition):

Brown, K. D. (2013). A Mobile Wireless Channel State Recognition Algorihm: Introduction, Definition, and Verification - Sensing for Cognitive Environmental Awareness. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/14843

Chicago Manual of Style (16th Edition):

Brown, Kenneth Dewayne. “A Mobile Wireless Channel State Recognition Algorihm: Introduction, Definition, and Verification - Sensing for Cognitive Environmental Awareness.” 2013. Doctoral Dissertation, University of Kansas. Accessed January 22, 2021. http://hdl.handle.net/1808/14843.

MLA Handbook (7th Edition):

Brown, Kenneth Dewayne. “A Mobile Wireless Channel State Recognition Algorihm: Introduction, Definition, and Verification - Sensing for Cognitive Environmental Awareness.” 2013. Web. 22 Jan 2021.

Vancouver:

Brown KD. A Mobile Wireless Channel State Recognition Algorihm: Introduction, Definition, and Verification - Sensing for Cognitive Environmental Awareness. [Internet] [Doctoral dissertation]. University of Kansas; 2013. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1808/14843.

Council of Science Editors:

Brown KD. A Mobile Wireless Channel State Recognition Algorihm: Introduction, Definition, and Verification - Sensing for Cognitive Environmental Awareness. [Doctoral Dissertation]. University of Kansas; 2013. Available from: http://hdl.handle.net/1808/14843


University of Kansas

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

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

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Stastny, Thomas James. “Collision Avoidance for Fixed-Wing Unmanned Aerial Systems Using Morphing Potential Field Navigation with Robust and Predictive Control.” 2014. Masters Thesis, University of Kansas. Accessed January 22, 2021. http://hdl.handle.net/1808/19613.

MLA Handbook (7th Edition):

Stastny, Thomas James. “Collision Avoidance for Fixed-Wing Unmanned Aerial Systems Using Morphing Potential Field Navigation with Robust and Predictive Control.” 2014. Web. 22 Jan 2021.

Vancouver:

Stastny TJ. Collision Avoidance for Fixed-Wing Unmanned Aerial Systems Using Morphing Potential Field Navigation with Robust and Predictive Control. [Internet] [Masters thesis]. University of Kansas; 2014. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1808/19613.

Council of Science Editors:

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


University of Kansas

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

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

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Bowman, Alec Davis. “Gain-Scheduled H-Infinity Control and Analysis of a Nonlinear Generic Hypersonic Vehicle.” 2016. Masters Thesis, University of Kansas. Accessed January 22, 2021. http://hdl.handle.net/1808/22339.

MLA Handbook (7th Edition):

Bowman, Alec Davis. “Gain-Scheduled H-Infinity Control and Analysis of a Nonlinear Generic Hypersonic Vehicle.” 2016. Web. 22 Jan 2021.

Vancouver:

Bowman AD. Gain-Scheduled H-Infinity Control and Analysis of a Nonlinear Generic Hypersonic Vehicle. [Internet] [Masters thesis]. University of Kansas; 2016. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1808/22339.

Council of Science Editors:

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


University of Kansas

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

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

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Kim, A Ram. “Intelligent Guidance, Navigation and Control of Multi-Agent UASs with Validation and Verification.” 2018. Doctoral Dissertation, University of Kansas. Accessed January 22, 2021. http://hdl.handle.net/1808/27816.

MLA Handbook (7th Edition):

Kim, A Ram. “Intelligent Guidance, Navigation and Control of Multi-Agent UASs with Validation and Verification.” 2018. Web. 22 Jan 2021.

Vancouver:

Kim AR. Intelligent Guidance, Navigation and Control of Multi-Agent UASs with Validation and Verification. [Internet] [Doctoral dissertation]. University of Kansas; 2018. [cited 2021 Jan 22]. 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

9. Frazer, Lance. Subchondral Bone Cysts - Filling the Void.

Degree: PhD, Bioengineering, 2019, University of Kansas

 Subchondral bone cysts (SBCs) are voids that can occur in the bones of young horses, especially horses intended for performance. Believed to be caused by… (more)

Subjects/Keywords: Biomechanics; Veterinary science; Health sciences; Equine Stifle; Finite Element Analysis; Knee; Osteoarthritis; Subchondral Bone Cysts; Transcondylar Screw

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APA (6th Edition):

Frazer, L. (2019). Subchondral Bone Cysts - Filling the Void. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/29652

Chicago Manual of Style (16th Edition):

Frazer, Lance. “Subchondral Bone Cysts - Filling the Void.” 2019. Doctoral Dissertation, University of Kansas. Accessed January 22, 2021. http://hdl.handle.net/1808/29652.

MLA Handbook (7th Edition):

Frazer, Lance. “Subchondral Bone Cysts - Filling the Void.” 2019. Web. 22 Jan 2021.

Vancouver:

Frazer L. Subchondral Bone Cysts - Filling the Void. [Internet] [Doctoral dissertation]. University of Kansas; 2019. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1808/29652.

Council of Science Editors:

Frazer L. Subchondral Bone Cysts - Filling the Void. [Doctoral Dissertation]. University of Kansas; 2019. Available from: http://hdl.handle.net/1808/29652


University of Kansas

10. 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 January 22, 2021. 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. 22 Jan 2021.

Vancouver:

Flesberg S. Mixing Enhancement in a Scramjet Combustor Using Fuel Jet Injection Swirl. [Internet] [Doctoral dissertation]. University of Kansas; 2015. [cited 2021 Jan 22]. 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

11. Grorud, Dustin. Wing Mounted Ice Penetrating Radar Array for a Medium Altitude Long Endurance Remote Aircraft.

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

 A wing mounted ice penetrating radar array for remote sensing is presented. The structure is designed to carry radar antennas on a representative unmanned aircraft… (more)

Subjects/Keywords: Aerospace engineering; Climate change; Remote sensing; Airborne sounding; Glaciers; Radar; Structural analysis; Uav

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APA (6th Edition):

Grorud, D. (2012). Wing Mounted Ice Penetrating Radar Array for a Medium Altitude Long Endurance Remote Aircraft. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/10660

Chicago Manual of Style (16th Edition):

Grorud, Dustin. “Wing Mounted Ice Penetrating Radar Array for a Medium Altitude Long Endurance Remote Aircraft.” 2012. Masters Thesis, University of Kansas. Accessed January 22, 2021. http://hdl.handle.net/1808/10660.

MLA Handbook (7th Edition):

Grorud, Dustin. “Wing Mounted Ice Penetrating Radar Array for a Medium Altitude Long Endurance Remote Aircraft.” 2012. Web. 22 Jan 2021.

Vancouver:

Grorud D. Wing Mounted Ice Penetrating Radar Array for a Medium Altitude Long Endurance Remote Aircraft. [Internet] [Masters thesis]. University of Kansas; 2012. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1808/10660.

Council of Science Editors:

Grorud D. Wing Mounted Ice Penetrating Radar Array for a Medium Altitude Long Endurance Remote Aircraft. [Masters Thesis]. University of Kansas; 2012. Available from: http://hdl.handle.net/1808/10660

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

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

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

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

…particular interest at the University of Kansas, where the Center for Remote Sensing of Ice Sheets… …University of Kansas, which is based on an existing Ultra-Wideband (UWB) antenna design… …of Kansas. The Multichannel Coherent Radar Depth Sounder (MCoRDS) antenna array… …shows an example of a wing-integrated antenna array developed by the CReSIS at the University… 

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Mendoza Strilchuk, Pedro. “Structural-Electromagnetic Simulation Coupling and Conformal Antenna Design Tool.” 2018. Masters Thesis, University of Kansas. Accessed January 22, 2021. http://hdl.handle.net/1808/27597.

MLA Handbook (7th Edition):

Mendoza Strilchuk, Pedro. “Structural-Electromagnetic Simulation Coupling and Conformal Antenna Design Tool.” 2018. Web. 22 Jan 2021.

Vancouver:

Mendoza Strilchuk P. Structural-Electromagnetic Simulation Coupling and Conformal Antenna Design Tool. [Internet] [Masters thesis]. University of Kansas; 2018. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1808/27597.

Council of Science Editors:

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

13. Escalera Mendoza, Alejandra Stefania. Radome Design and Curvature Effects on Antenna Performance, with Application to Radar Array Installation in Transonic Aircraft.

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

 Significant and fast changes in the cryosphere have been observed and monitored using radioglaciology and remote sensing technology. A fuselage mounted Ultrawideband Multichannel Coherent Radar… (more)

Subjects/Keywords: Aerospace engineering; Electrical engineering; Remote sensing; aircraft; conformal; radar; radome; transonic; ultrawideband

…High Frequency High Frequency Structure Simulator University of Kansas Low Frequency Margin… …Description and Technology Background The University of Kansas (KU) CReSIS team proposed… 

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APA (6th Edition):

Escalera Mendoza, A. S. (2019). Radome Design and Curvature Effects on Antenna Performance, with Application to Radar Array Installation in Transonic Aircraft. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/29701

Chicago Manual of Style (16th Edition):

Escalera Mendoza, Alejandra Stefania. “Radome Design and Curvature Effects on Antenna Performance, with Application to Radar Array Installation in Transonic Aircraft.” 2019. Masters Thesis, University of Kansas. Accessed January 22, 2021. http://hdl.handle.net/1808/29701.

MLA Handbook (7th Edition):

Escalera Mendoza, Alejandra Stefania. “Radome Design and Curvature Effects on Antenna Performance, with Application to Radar Array Installation in Transonic Aircraft.” 2019. Web. 22 Jan 2021.

Vancouver:

Escalera Mendoza AS. Radome Design and Curvature Effects on Antenna Performance, with Application to Radar Array Installation in Transonic Aircraft. [Internet] [Masters thesis]. University of Kansas; 2019. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1808/29701.

Council of Science Editors:

Escalera Mendoza AS. Radome Design and Curvature Effects on Antenna Performance, with Application to Radar Array Installation in Transonic Aircraft. [Masters Thesis]. University of Kansas; 2019. Available from: http://hdl.handle.net/1808/29701

14. Walther, Hans Wolfgang. Development of a Lightweight Laminated Composite Wheel for Formula SAE Race Vehicles.

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

 Reducing the weight of a racing vehicle can substantially improve its acceleration and general performance abilities. More specifically, reduction of the unsprung corner weight can… (more)

Subjects/Keywords: Mechanical engineering; Automotive engineering; Automotive; Composite; Finite Element Analysis; Formula SAE; Rim; Wheel

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APA (6th Edition):

Walther, H. W. (2016). Development of a Lightweight Laminated Composite Wheel for Formula SAE Race Vehicles. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/21984

Chicago Manual of Style (16th Edition):

Walther, Hans Wolfgang. “Development of a Lightweight Laminated Composite Wheel for Formula SAE Race Vehicles.” 2016. Masters Thesis, University of Kansas. Accessed January 22, 2021. http://hdl.handle.net/1808/21984.

MLA Handbook (7th Edition):

Walther, Hans Wolfgang. “Development of a Lightweight Laminated Composite Wheel for Formula SAE Race Vehicles.” 2016. Web. 22 Jan 2021.

Vancouver:

Walther HW. Development of a Lightweight Laminated Composite Wheel for Formula SAE Race Vehicles. [Internet] [Masters thesis]. University of Kansas; 2016. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1808/21984.

Council of Science Editors:

Walther HW. Development of a Lightweight Laminated Composite Wheel for Formula SAE Race Vehicles. [Masters Thesis]. University of Kansas; 2016. Available from: http://hdl.handle.net/1808/21984

15. Dande, Himanshu Amol. Evaluation of Loss Factor Estimation Techniques for Free Hanging Flat Panels Excited Mechanically.

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

 To establish the "best" technique to estimate a damping loss factor for mechanically-excited panels, three loss factor estimation techniques – PIM, IRDM, and RDT – are compared.… (more)

Subjects/Keywords: Aerospace engineering; Flat panel; Impulse response decay method; Power input method; Radius of direct field; Random decrement technique; Reverberant field

…matrix KUAE The University of Kansas, Department of Aerospace Engineering xxii k… 

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APA (6th Edition):

Dande, H. A. (2013). Evaluation of Loss Factor Estimation Techniques for Free Hanging Flat Panels Excited Mechanically. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/11681

Chicago Manual of Style (16th Edition):

Dande, Himanshu Amol. “Evaluation of Loss Factor Estimation Techniques for Free Hanging Flat Panels Excited Mechanically.” 2013. Doctoral Dissertation, University of Kansas. Accessed January 22, 2021. http://hdl.handle.net/1808/11681.

MLA Handbook (7th Edition):

Dande, Himanshu Amol. “Evaluation of Loss Factor Estimation Techniques for Free Hanging Flat Panels Excited Mechanically.” 2013. Web. 22 Jan 2021.

Vancouver:

Dande HA. Evaluation of Loss Factor Estimation Techniques for Free Hanging Flat Panels Excited Mechanically. [Internet] [Doctoral dissertation]. University of Kansas; 2013. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1808/11681.

Council of Science Editors:

Dande HA. Evaluation of Loss Factor Estimation Techniques for Free Hanging Flat Panels Excited Mechanically. [Doctoral Dissertation]. University of Kansas; 2013. Available from: http://hdl.handle.net/1808/11681

16. Abd. Rahim, Mohd. Razi. Numerical Simulation/Analysis and Computer Aided Engineering for Virtual Protyping of Heavy Ground Vehicle.

Degree: D.Eng., Mechanical Engineering, 2010, University of Kansas

 This doctoral project dissertation deals with the investigation of simulation/analysis in the product development process of specialized heavy ground vehicle engineering which posts some of… (more)

Subjects/Keywords: Mechanical engineering; Heavy ground vehicle; Virtual prototyping

…45 Figure 2.4. Virtual prototype of University of Kansas Formula SAE car - full vehicle… 

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APA (6th Edition):

Abd. Rahim, M. R. (2010). Numerical Simulation/Analysis and Computer Aided Engineering for Virtual Protyping of Heavy Ground Vehicle. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/7013

Chicago Manual of Style (16th Edition):

Abd. Rahim, Mohd Razi. “Numerical Simulation/Analysis and Computer Aided Engineering for Virtual Protyping of Heavy Ground Vehicle.” 2010. Doctoral Dissertation, University of Kansas. Accessed January 22, 2021. http://hdl.handle.net/1808/7013.

MLA Handbook (7th Edition):

Abd. Rahim, Mohd Razi. “Numerical Simulation/Analysis and Computer Aided Engineering for Virtual Protyping of Heavy Ground Vehicle.” 2010. Web. 22 Jan 2021.

Vancouver:

Abd. Rahim MR. Numerical Simulation/Analysis and Computer Aided Engineering for Virtual Protyping of Heavy Ground Vehicle. [Internet] [Doctoral dissertation]. University of Kansas; 2010. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1808/7013.

Council of Science Editors:

Abd. Rahim MR. Numerical Simulation/Analysis and Computer Aided Engineering for Virtual Protyping of Heavy Ground Vehicle. [Doctoral Dissertation]. University of Kansas; 2010. Available from: http://hdl.handle.net/1808/7013

17. Arnold, Emily J. Development and Improvement of Airborne Remote Sensing Radar Platforms.

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

 With the recent record ice melt in the Arctic as well as the dramatic changes occurring in the Antarctic, the need and urgency to characterize… (more)

Subjects/Keywords: Aerospace engineering; Airborne radar; Antenna arrays; Remote sensing

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APA (6th Edition):

Arnold, E. J. (2013). Development and Improvement of Airborne Remote Sensing Radar Platforms. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/12182

Chicago Manual of Style (16th Edition):

Arnold, Emily J. “Development and Improvement of Airborne Remote Sensing Radar Platforms.” 2013. Doctoral Dissertation, University of Kansas. Accessed January 22, 2021. http://hdl.handle.net/1808/12182.

MLA Handbook (7th Edition):

Arnold, Emily J. “Development and Improvement of Airborne Remote Sensing Radar Platforms.” 2013. Web. 22 Jan 2021.

Vancouver:

Arnold EJ. Development and Improvement of Airborne Remote Sensing Radar Platforms. [Internet] [Doctoral dissertation]. University of Kansas; 2013. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1808/12182.

Council of Science Editors:

Arnold EJ. Development and Improvement of Airborne Remote Sensing Radar Platforms. [Doctoral Dissertation]. University of Kansas; 2013. Available from: http://hdl.handle.net/1808/12182

18. Garcia, Gonzalo. DECENTRALIZED ROBUST NONLINEAR MODEL PREDICTIVE CONTROLLER FOR UNMANNED AERIAL SYSTEMS.

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

 The nonlinear and unsteady nature of aircraft aerodynamics together with limited practical range of controls and state variables make the use of the linear control… (more)

Subjects/Keywords: Aerospace engineering; Aircraft; Autopilot; Control; Nonlinear; Predictive; Robust

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APA (6th Edition):

Garcia, G. (2013). DECENTRALIZED ROBUST NONLINEAR MODEL PREDICTIVE CONTROLLER FOR UNMANNED AERIAL SYSTEMS. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/11454

Chicago Manual of Style (16th Edition):

Garcia, Gonzalo. “DECENTRALIZED ROBUST NONLINEAR MODEL PREDICTIVE CONTROLLER FOR UNMANNED AERIAL SYSTEMS.” 2013. Doctoral Dissertation, University of Kansas. Accessed January 22, 2021. http://hdl.handle.net/1808/11454.

MLA Handbook (7th Edition):

Garcia, Gonzalo. “DECENTRALIZED ROBUST NONLINEAR MODEL PREDICTIVE CONTROLLER FOR UNMANNED AERIAL SYSTEMS.” 2013. Web. 22 Jan 2021.

Vancouver:

Garcia G. DECENTRALIZED ROBUST NONLINEAR MODEL PREDICTIVE CONTROLLER FOR UNMANNED AERIAL SYSTEMS. [Internet] [Doctoral dissertation]. University of Kansas; 2013. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1808/11454.

Council of Science Editors:

Garcia G. DECENTRALIZED ROBUST NONLINEAR MODEL PREDICTIVE CONTROLLER FOR UNMANNED AERIAL SYSTEMS. [Doctoral Dissertation]. University of Kansas; 2013. Available from: http://hdl.handle.net/1808/11454

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

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

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Legursky, Katrina. “System Identification and the Modeling of Sailing Yachts.” 2013. Doctoral Dissertation, University of Kansas. Accessed January 22, 2021. http://hdl.handle.net/1808/14198.

MLA Handbook (7th Edition):

Legursky, Katrina. “System Identification and the Modeling of Sailing Yachts.” 2013. Web. 22 Jan 2021.

Vancouver:

Legursky K. System Identification and the Modeling of Sailing Yachts. [Internet] [Doctoral dissertation]. University of Kansas; 2013. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1808/14198.

Council of Science Editors:

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


University of Kansas

20. Jager, Rylan Walter. Test and Evaluation of the Piccolo Autopilot System on a One-Third Scale Yak-54.

Degree: MS, Aerospace Engineering, 2008, University of Kansas

 To gain a better understanding of the dynamics of the great ice sheets the National Science Foundation established the Center for Remote Sensing of Ice… (more)

Subjects/Keywords: Aerospace engineering

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APA (6th Edition):

Jager, R. W. (2008). Test and Evaluation of the Piccolo Autopilot System on a One-Third Scale Yak-54. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/3997

Chicago Manual of Style (16th Edition):

Jager, Rylan Walter. “Test and Evaluation of the Piccolo Autopilot System on a One-Third Scale Yak-54.” 2008. Masters Thesis, University of Kansas. Accessed January 22, 2021. http://hdl.handle.net/1808/3997.

MLA Handbook (7th Edition):

Jager, Rylan Walter. “Test and Evaluation of the Piccolo Autopilot System on a One-Third Scale Yak-54.” 2008. Web. 22 Jan 2021.

Vancouver:

Jager RW. Test and Evaluation of the Piccolo Autopilot System on a One-Third Scale Yak-54. [Internet] [Masters thesis]. University of Kansas; 2008. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1808/3997.

Council of Science Editors:

Jager RW. Test and Evaluation of the Piccolo Autopilot System on a One-Third Scale Yak-54. [Masters Thesis]. University of Kansas; 2008. Available from: http://hdl.handle.net/1808/3997


University of Kansas

21. Donovan, William. The Design of an Uninhabited Air Vehicle for Remote Sensing in the Cryosphere.

Degree: MS, Aerospace Engineering, 2007, University of Kansas

 This document summarizes the results of the preliminary design of an Uninhabited Air Vehicle (UAV) for use in Cryospheric research. This includes the development of… (more)

Subjects/Keywords: Aerospace engineering; Uav; Uas; Remote sensing; Unamnned aircraft; Aircraft design

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APA (6th Edition):

Donovan, W. (2007). The Design of an Uninhabited Air Vehicle for Remote Sensing in the Cryosphere. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/1989

Chicago Manual of Style (16th Edition):

Donovan, William. “The Design of an Uninhabited Air Vehicle for Remote Sensing in the Cryosphere.” 2007. Masters Thesis, University of Kansas. Accessed January 22, 2021. http://hdl.handle.net/1808/1989.

MLA Handbook (7th Edition):

Donovan, William. “The Design of an Uninhabited Air Vehicle for Remote Sensing in the Cryosphere.” 2007. Web. 22 Jan 2021.

Vancouver:

Donovan W. The Design of an Uninhabited Air Vehicle for Remote Sensing in the Cryosphere. [Internet] [Masters thesis]. University of Kansas; 2007. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1808/1989.

Council of Science Editors:

Donovan W. The Design of an Uninhabited Air Vehicle for Remote Sensing in the Cryosphere. [Masters Thesis]. University of Kansas; 2007. Available from: http://hdl.handle.net/1808/1989


University of Kansas

22. 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 January 22, 2021. 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. 22 Jan 2021.

Vancouver:

Kim K. Flexural Stiffnesses of and Dimensional Stability in Circular Quasi-isotropic Laminate Mirrors. [Internet] [Doctoral dissertation]. University of Kansas; 2009. [cited 2021 Jan 22]. 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

23. Tom, Jonathan. Planning, Execution, and Analysis of the Meridian UAS Flight Test Program Including System and Parameter Identification.

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

 The purpose of this Master Thesis is to present the flight test procedures, planning, and analysis including system identification, parameter identification, and drag calculations of… (more)

Subjects/Keywords: Aerospace engineering; Drag analysis; Flight test; Meridian; Parameter identification; System identification; Uav

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APA (6th Edition):

Tom, J. (2010). Planning, Execution, and Analysis of the Meridian UAS Flight Test Program Including System and Parameter Identification. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/6274

Chicago Manual of Style (16th Edition):

Tom, Jonathan. “Planning, Execution, and Analysis of the Meridian UAS Flight Test Program Including System and Parameter Identification.” 2010. Masters Thesis, University of Kansas. Accessed January 22, 2021. http://hdl.handle.net/1808/6274.

MLA Handbook (7th Edition):

Tom, Jonathan. “Planning, Execution, and Analysis of the Meridian UAS Flight Test Program Including System and Parameter Identification.” 2010. Web. 22 Jan 2021.

Vancouver:

Tom J. Planning, Execution, and Analysis of the Meridian UAS Flight Test Program Including System and Parameter Identification. [Internet] [Masters thesis]. University of Kansas; 2010. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1808/6274.

Council of Science Editors:

Tom J. Planning, Execution, and Analysis of the Meridian UAS Flight Test Program Including System and Parameter Identification. [Masters Thesis]. University of Kansas; 2010. Available from: http://hdl.handle.net/1808/6274


University of Kansas

24. 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 January 22, 2021. 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. 22 Jan 2021.

Vancouver:

Dande HA. Panel Damping Loss Factor Estimation Using The Random Decrement Technique. [Internet] [Masters thesis]. University of Kansas; 2010. [cited 2021 Jan 22]. 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

25. Liu, Wanbo. Experimental and Analytical Estimation of Damping in Beams and Plates with Damping Treatments.

Degree: PhD, Aerospace Engineering, 2008, University of Kansas

 The research presented in this dissertation is devoted to the problem of damping estimation in engineering structures, especially beams and plates with passive damping treatments.… (more)

Subjects/Keywords: Aerospace engineering; Mechanical engineering; Damping loss factor estimation; Damping measurement; Dynamic vibration; Experimental analytical; Finite element method; Power input method

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APA (6th Edition):

Liu, W. (2008). Experimental and Analytical Estimation of Damping in Beams and Plates with Damping Treatments. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/4362

Chicago Manual of Style (16th Edition):

Liu, Wanbo. “Experimental and Analytical Estimation of Damping in Beams and Plates with Damping Treatments.” 2008. Doctoral Dissertation, University of Kansas. Accessed January 22, 2021. http://hdl.handle.net/1808/4362.

MLA Handbook (7th Edition):

Liu, Wanbo. “Experimental and Analytical Estimation of Damping in Beams and Plates with Damping Treatments.” 2008. Web. 22 Jan 2021.

Vancouver:

Liu W. Experimental and Analytical Estimation of Damping in Beams and Plates with Damping Treatments. [Internet] [Doctoral dissertation]. University of Kansas; 2008. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1808/4362.

Council of Science Editors:

Liu W. Experimental and Analytical Estimation of Damping in Beams and Plates with Damping Treatments. [Doctoral Dissertation]. University of Kansas; 2008. Available from: http://hdl.handle.net/1808/4362


University of Kansas

26. Royer, David Andrew. Design of an Automatic Landing System for the Meridian UAV using Fuzzy Logic.

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

 This document describes the design of an automatic landing system for the Meridian unmanned aerial vehicle (UAV) in development for glacial ice research. The Center… (more)

Subjects/Keywords: Aerospace engineering; Autoland; Fuzzy logic; Sensitivity analysis; Uav; Wepilot

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APA (6th Edition):

Royer, D. A. (2010). Design of an Automatic Landing System for the Meridian UAV using Fuzzy Logic. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/6290

Chicago Manual of Style (16th Edition):

Royer, David Andrew. “Design of an Automatic Landing System for the Meridian UAV using Fuzzy Logic.” 2010. Masters Thesis, University of Kansas. Accessed January 22, 2021. http://hdl.handle.net/1808/6290.

MLA Handbook (7th Edition):

Royer, David Andrew. “Design of an Automatic Landing System for the Meridian UAV using Fuzzy Logic.” 2010. Web. 22 Jan 2021.

Vancouver:

Royer DA. Design of an Automatic Landing System for the Meridian UAV using Fuzzy Logic. [Internet] [Masters thesis]. University of Kansas; 2010. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1808/6290.

Council of Science Editors:

Royer DA. Design of an Automatic Landing System for the Meridian UAV using Fuzzy Logic. [Masters Thesis]. University of Kansas; 2010. Available from: http://hdl.handle.net/1808/6290


University of Kansas

27. 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 January 22, 2021. 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. 22 Jan 2021.

Vancouver:

Sweeten BC. CFD Analysis of UAVs using VORSTAB, FLUENT, and Advanced Aircraft Analysis Software. [Internet] [Masters thesis]. University of Kansas; 2010. [cited 2021 Jan 22]. 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

28. Lusk, Jonathan Thomas. Wing and Fuselage Optimization Considering Alternative Material.

Degree: MS, Aerospace Engineering, 2008, University of Kansas

 This study is a sensitivity analysis to compare weight benefits for a transport aircraft airframe from potential mechanical property enhancements of CFRP (Carbon Fiber Reinforced… (more)

Subjects/Keywords: Aerospace engineering; Materials science engineering; Industrial engineering; Composite

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APA (6th Edition):

Lusk, J. T. (2008). Wing and Fuselage Optimization Considering Alternative Material. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/4015

Chicago Manual of Style (16th Edition):

Lusk, Jonathan Thomas. “Wing and Fuselage Optimization Considering Alternative Material.” 2008. Masters Thesis, University of Kansas. Accessed January 22, 2021. http://hdl.handle.net/1808/4015.

MLA Handbook (7th Edition):

Lusk, Jonathan Thomas. “Wing and Fuselage Optimization Considering Alternative Material.” 2008. Web. 22 Jan 2021.

Vancouver:

Lusk JT. Wing and Fuselage Optimization Considering Alternative Material. [Internet] [Masters thesis]. University of Kansas; 2008. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1808/4015.

Council of Science Editors:

Lusk JT. Wing and Fuselage Optimization Considering Alternative Material. [Masters Thesis]. University of Kansas; 2008. Available from: http://hdl.handle.net/1808/4015


University of Kansas

29. Nunez, Daniel. J-integral Computations for Linear Elastic Fracture Mechanics in h,p,k Mathematical and Computational Framework.

Degree: MS, Aerospace Engineering, 2008, University of Kansas

 This thesis presents an infrastructure for computations of the J-integral for mode I linear elastic fracture mechanics in h,p,k mathematical and computational framework using finite… (more)

Subjects/Keywords: Aerospace engineering; Mechanical engineering; J-integral; Galerkin method with weak form; Least squares processes; Linear elastic fracture mechanics

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APA (6th Edition):

Nunez, D. (2008). J-integral Computations for Linear Elastic Fracture Mechanics in h,p,k Mathematical and Computational Framework. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/4045

Chicago Manual of Style (16th Edition):

Nunez, Daniel. “J-integral Computations for Linear Elastic Fracture Mechanics in h,p,k Mathematical and Computational Framework.” 2008. Masters Thesis, University of Kansas. Accessed January 22, 2021. http://hdl.handle.net/1808/4045.

MLA Handbook (7th Edition):

Nunez, Daniel. “J-integral Computations for Linear Elastic Fracture Mechanics in h,p,k Mathematical and Computational Framework.” 2008. Web. 22 Jan 2021.

Vancouver:

Nunez D. J-integral Computations for Linear Elastic Fracture Mechanics in h,p,k Mathematical and Computational Framework. [Internet] [Masters thesis]. University of Kansas; 2008. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1808/4045.

Council of Science Editors:

Nunez D. J-integral Computations for Linear Elastic Fracture Mechanics in h,p,k Mathematical and Computational Framework. [Masters Thesis]. University of Kansas; 2008. Available from: http://hdl.handle.net/1808/4045


University of Kansas

30. Vos, Roelof. Mechanics and Applications of Pressure Adaptive Honeycomb.

Degree: PhD, American Studies, 2009, University of Kansas

 A pressure-adaptive wing structure is presented that relies on the pressure-altitude relation to adapt the wing shape to the various flight conditions (e.g. landing and… (more)

Subjects/Keywords: Aerospace engineering; Adaptive; Honeycomb; Morphing; Structure

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APA (6th Edition):

Vos, R. (2009). Mechanics and Applications of Pressure Adaptive Honeycomb. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/6024

Chicago Manual of Style (16th Edition):

Vos, Roelof. “Mechanics and Applications of Pressure Adaptive Honeycomb.” 2009. Doctoral Dissertation, University of Kansas. Accessed January 22, 2021. http://hdl.handle.net/1808/6024.

MLA Handbook (7th Edition):

Vos, Roelof. “Mechanics and Applications of Pressure Adaptive Honeycomb.” 2009. Web. 22 Jan 2021.

Vancouver:

Vos R. Mechanics and Applications of Pressure Adaptive Honeycomb. [Internet] [Doctoral dissertation]. University of Kansas; 2009. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1808/6024.

Council of Science Editors:

Vos R. Mechanics and Applications of Pressure Adaptive Honeycomb. [Doctoral Dissertation]. University of Kansas; 2009. Available from: http://hdl.handle.net/1808/6024

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