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You searched for subject:(Systems Engineering AND Multidisciplinary Design Optimization). Showing records 1 – 30 of 272 total matches.

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University of Tennessee – Knoxville

1. Williams, Samuel Vivek. Automating Real-Time Fault Detection for the University of Tennessee Space Institute, Aviation Systems’ Flight Testing and Airborne Science Applications.

Degree: MS, Aviation Systems, 2011, University of Tennessee – Knoxville

  The UTSI Aviation Systems program has conducted many successful airborne science campaigns in collaboration with premier research organizations including NASA and NOAA. Each airborne… (more)

Subjects/Keywords: Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Williams, S. V. (2011). Automating Real-Time Fault Detection for the University of Tennessee Space Institute, Aviation Systems’ Flight Testing and Airborne Science Applications. (Thesis). University of Tennessee – Knoxville. Retrieved from https://trace.tennessee.edu/utk_gradthes/1107

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

Chicago Manual of Style (16th Edition):

Williams, Samuel Vivek. “Automating Real-Time Fault Detection for the University of Tennessee Space Institute, Aviation Systems’ Flight Testing and Airborne Science Applications.” 2011. Thesis, University of Tennessee – Knoxville. Accessed March 01, 2021. https://trace.tennessee.edu/utk_gradthes/1107.

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

MLA Handbook (7th Edition):

Williams, Samuel Vivek. “Automating Real-Time Fault Detection for the University of Tennessee Space Institute, Aviation Systems’ Flight Testing and Airborne Science Applications.” 2011. Web. 01 Mar 2021.

Vancouver:

Williams SV. Automating Real-Time Fault Detection for the University of Tennessee Space Institute, Aviation Systems’ Flight Testing and Airborne Science Applications. [Internet] [Thesis]. University of Tennessee – Knoxville; 2011. [cited 2021 Mar 01]. Available from: https://trace.tennessee.edu/utk_gradthes/1107.

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

Council of Science Editors:

Williams SV. Automating Real-Time Fault Detection for the University of Tennessee Space Institute, Aviation Systems’ Flight Testing and Airborne Science Applications. [Thesis]. University of Tennessee – Knoxville; 2011. Available from: https://trace.tennessee.edu/utk_gradthes/1107

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


Brigham Young University

2. Larson, Bradley Jared. Mathematical Framework for Early System Design Validation Using Multidisciplinary System Models.

Degree: PhD, 2012, Brigham Young University

 A significant challenge in the design of multidisciplinary systems (e.g., airplanes, robots, cell phones) is to predict the effects of design decisions at the time… (more)

Subjects/Keywords: system design; multidisciplinary design optimization; nonlinear systems; model composition; Mechanical Engineering

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APA (6th Edition):

Larson, B. J. (2012). Mathematical Framework for Early System Design Validation Using Multidisciplinary System Models. (Doctoral Dissertation). Brigham Young University. Retrieved from https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=3999&context=etd

Chicago Manual of Style (16th Edition):

Larson, Bradley Jared. “Mathematical Framework for Early System Design Validation Using Multidisciplinary System Models.” 2012. Doctoral Dissertation, Brigham Young University. Accessed March 01, 2021. https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=3999&context=etd.

MLA Handbook (7th Edition):

Larson, Bradley Jared. “Mathematical Framework for Early System Design Validation Using Multidisciplinary System Models.” 2012. Web. 01 Mar 2021.

Vancouver:

Larson BJ. Mathematical Framework for Early System Design Validation Using Multidisciplinary System Models. [Internet] [Doctoral dissertation]. Brigham Young University; 2012. [cited 2021 Mar 01]. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=3999&context=etd.

Council of Science Editors:

Larson BJ. Mathematical Framework for Early System Design Validation Using Multidisciplinary System Models. [Doctoral Dissertation]. Brigham Young University; 2012. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=3999&context=etd


Embry-Riddle Aeronautical University

3. Twahir, Abdulhalim. Preliminary Design of Blade and Disc Fixing for Aerospace Application using Multi-Disciplinary Approach.

Degree: MSin Aerospace Engineering, Aerospace Engineering, 2013, Embry-Riddle Aeronautical University

  The preliminary design phase of a turbine rotor has an important impact on the architecture of a new engine definition, as it sets the… (more)

Subjects/Keywords: Aerospace Engineering; Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Twahir, A. (2013). Preliminary Design of Blade and Disc Fixing for Aerospace Application using Multi-Disciplinary Approach. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/141

Chicago Manual of Style (16th Edition):

Twahir, Abdulhalim. “Preliminary Design of Blade and Disc Fixing for Aerospace Application using Multi-Disciplinary Approach.” 2013. Masters Thesis, Embry-Riddle Aeronautical University. Accessed March 01, 2021. https://commons.erau.edu/edt/141.

MLA Handbook (7th Edition):

Twahir, Abdulhalim. “Preliminary Design of Blade and Disc Fixing for Aerospace Application using Multi-Disciplinary Approach.” 2013. Web. 01 Mar 2021.

Vancouver:

Twahir A. Preliminary Design of Blade and Disc Fixing for Aerospace Application using Multi-Disciplinary Approach. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2013. [cited 2021 Mar 01]. Available from: https://commons.erau.edu/edt/141.

Council of Science Editors:

Twahir A. Preliminary Design of Blade and Disc Fixing for Aerospace Application using Multi-Disciplinary Approach. [Masters Thesis]. Embry-Riddle Aeronautical University; 2013. Available from: https://commons.erau.edu/edt/141


Embry-Riddle Aeronautical University

4. Rocha, Andres E. Perez. Development of Fault Tolerant Adaptive Control Laws for Aerospace Systems.

Degree: PhD, Aerospace Engineering, 2016, Embry-Riddle Aeronautical University

  The main topic of this dissertation is the design, development and implementation of intelligent adaptive control techniques designed to maintain healthy performance of aerospace… (more)

Subjects/Keywords: Aerospace Engineering; Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Rocha, A. E. P. (2016). Development of Fault Tolerant Adaptive Control Laws for Aerospace Systems. (Doctoral Dissertation). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/289

Chicago Manual of Style (16th Edition):

Rocha, Andres E Perez. “Development of Fault Tolerant Adaptive Control Laws for Aerospace Systems.” 2016. Doctoral Dissertation, Embry-Riddle Aeronautical University. Accessed March 01, 2021. https://commons.erau.edu/edt/289.

MLA Handbook (7th Edition):

Rocha, Andres E Perez. “Development of Fault Tolerant Adaptive Control Laws for Aerospace Systems.” 2016. Web. 01 Mar 2021.

Vancouver:

Rocha AEP. Development of Fault Tolerant Adaptive Control Laws for Aerospace Systems. [Internet] [Doctoral dissertation]. Embry-Riddle Aeronautical University; 2016. [cited 2021 Mar 01]. Available from: https://commons.erau.edu/edt/289.

Council of Science Editors:

Rocha AEP. Development of Fault Tolerant Adaptive Control Laws for Aerospace Systems. [Doctoral Dissertation]. Embry-Riddle Aeronautical University; 2016. Available from: https://commons.erau.edu/edt/289


Cal Poly

5. Nugent, Ryan. Integration and Qualification of The P-PODs on The Vega Maiden Flight.

Degree: MS, Aerospace Engineering, 2016, Cal Poly

  On February 13, 2012, California Polytechnic State University, San Luis Obispo flew three Poly-Picosatellite Orbital Deployers (P-PODs), carrying seven European University CubeSats sponsored by… (more)

Subjects/Keywords: P-POD; Vega; CubeSat; Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Nugent, R. (2016). Integration and Qualification of The P-PODs on The Vega Maiden Flight. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1681 ; 10.15368/theses.2016.160

Chicago Manual of Style (16th Edition):

Nugent, Ryan. “Integration and Qualification of The P-PODs on The Vega Maiden Flight.” 2016. Masters Thesis, Cal Poly. Accessed March 01, 2021. https://digitalcommons.calpoly.edu/theses/1681 ; 10.15368/theses.2016.160.

MLA Handbook (7th Edition):

Nugent, Ryan. “Integration and Qualification of The P-PODs on The Vega Maiden Flight.” 2016. Web. 01 Mar 2021.

Vancouver:

Nugent R. Integration and Qualification of The P-PODs on The Vega Maiden Flight. [Internet] [Masters thesis]. Cal Poly; 2016. [cited 2021 Mar 01]. Available from: https://digitalcommons.calpoly.edu/theses/1681 ; 10.15368/theses.2016.160.

Council of Science Editors:

Nugent R. Integration and Qualification of The P-PODs on The Vega Maiden Flight. [Masters Thesis]. Cal Poly; 2016. Available from: https://digitalcommons.calpoly.edu/theses/1681 ; 10.15368/theses.2016.160


Cal Poly

6. Berrian, Joshua. AN AUTOMATED TEST STATION DESIGN USED TO VERIFY AIRCRAFT COMMUNICATION PROTOCOLS.

Degree: MS, Aerospace Engineering, 2011, Cal Poly

  Requirements verification is typically the costliest part of the systems engineering design process. In the commercial aircraft industry, as the software and hardware design(more)

Subjects/Keywords: Automation; Verification; Avionics; Communication; Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Berrian, J. (2011). AN AUTOMATED TEST STATION DESIGN USED TO VERIFY AIRCRAFT COMMUNICATION PROTOCOLS. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/635 ; 10.15368/theses.2011.192

Chicago Manual of Style (16th Edition):

Berrian, Joshua. “AN AUTOMATED TEST STATION DESIGN USED TO VERIFY AIRCRAFT COMMUNICATION PROTOCOLS.” 2011. Masters Thesis, Cal Poly. Accessed March 01, 2021. https://digitalcommons.calpoly.edu/theses/635 ; 10.15368/theses.2011.192.

MLA Handbook (7th Edition):

Berrian, Joshua. “AN AUTOMATED TEST STATION DESIGN USED TO VERIFY AIRCRAFT COMMUNICATION PROTOCOLS.” 2011. Web. 01 Mar 2021.

Vancouver:

Berrian J. AN AUTOMATED TEST STATION DESIGN USED TO VERIFY AIRCRAFT COMMUNICATION PROTOCOLS. [Internet] [Masters thesis]. Cal Poly; 2011. [cited 2021 Mar 01]. Available from: https://digitalcommons.calpoly.edu/theses/635 ; 10.15368/theses.2011.192.

Council of Science Editors:

Berrian J. AN AUTOMATED TEST STATION DESIGN USED TO VERIFY AIRCRAFT COMMUNICATION PROTOCOLS. [Masters Thesis]. Cal Poly; 2011. Available from: https://digitalcommons.calpoly.edu/theses/635 ; 10.15368/theses.2011.192


Iowa State University

7. Kwasa, Benjamin Jekonia. Incorporation of organization design in a value-based systems engineering framework.

Degree: 2017, Iowa State University

 The design of Large-Scale Complex Engineered Systems (LSCESs) is an undertaking that requires large organizations made up of several teams of individuals, often spread over… (more)

Subjects/Keywords: Multidisciplinary Design Optimization; Organization Design; Systems Design; Systems Engineering; Value-Based Systems Engineering; Value-Driven Design; Aerospace Engineering

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APA (6th Edition):

Kwasa, B. J. (2017). Incorporation of organization design in a value-based systems engineering framework. (Thesis). Iowa State University. Retrieved from https://lib.dr.iastate.edu/etd/16062

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

Chicago Manual of Style (16th Edition):

Kwasa, Benjamin Jekonia. “Incorporation of organization design in a value-based systems engineering framework.” 2017. Thesis, Iowa State University. Accessed March 01, 2021. https://lib.dr.iastate.edu/etd/16062.

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

MLA Handbook (7th Edition):

Kwasa, Benjamin Jekonia. “Incorporation of organization design in a value-based systems engineering framework.” 2017. Web. 01 Mar 2021.

Vancouver:

Kwasa BJ. Incorporation of organization design in a value-based systems engineering framework. [Internet] [Thesis]. Iowa State University; 2017. [cited 2021 Mar 01]. Available from: https://lib.dr.iastate.edu/etd/16062.

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

Council of Science Editors:

Kwasa BJ. Incorporation of organization design in a value-based systems engineering framework. [Thesis]. Iowa State University; 2017. Available from: https://lib.dr.iastate.edu/etd/16062

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


Iowa State University

8. Murugaiyan, Suresh. Modeling requirements to value formulation in the design of large-scale complex engineered systems: A satellite system case study.

Degree: 2017, Iowa State University

 Large-scale complex engineered systems (LSCES) are naturally a part of different areas of aerospace engineering and are typically characterized by high cost, high risk and… (more)

Subjects/Keywords: large scale complex engineered systems; Multidisciplinary design optimization; optimization; Requirements; Systems engineering; Value driven design; Aerospace Engineering; Industrial Engineering; Mechanical Engineering

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APA (6th Edition):

Murugaiyan, S. (2017). Modeling requirements to value formulation in the design of large-scale complex engineered systems: A satellite system case study. (Thesis). Iowa State University. Retrieved from https://lib.dr.iastate.edu/etd/16523

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

Chicago Manual of Style (16th Edition):

Murugaiyan, Suresh. “Modeling requirements to value formulation in the design of large-scale complex engineered systems: A satellite system case study.” 2017. Thesis, Iowa State University. Accessed March 01, 2021. https://lib.dr.iastate.edu/etd/16523.

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

MLA Handbook (7th Edition):

Murugaiyan, Suresh. “Modeling requirements to value formulation in the design of large-scale complex engineered systems: A satellite system case study.” 2017. Web. 01 Mar 2021.

Vancouver:

Murugaiyan S. Modeling requirements to value formulation in the design of large-scale complex engineered systems: A satellite system case study. [Internet] [Thesis]. Iowa State University; 2017. [cited 2021 Mar 01]. Available from: https://lib.dr.iastate.edu/etd/16523.

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

Council of Science Editors:

Murugaiyan S. Modeling requirements to value formulation in the design of large-scale complex engineered systems: A satellite system case study. [Thesis]. Iowa State University; 2017. Available from: https://lib.dr.iastate.edu/etd/16523

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


Cal Poly

9. Ralph, Alyssa M. Pathfinding Interplanetary Bus Capability for the Cal Poly CubeSat Laboratory Through the Development of a Phobos-Deimos Mission Concept.

Degree: MS, Aerospace Engineering, 2020, Cal Poly

  With the rise of CubeSats and the demonstration of their many space applications, there is interest in interplanetary CubeSats to act for example as… (more)

Subjects/Keywords: small satellites; planetary; systems engineering; mission architecture; Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Ralph, A. M. (2020). Pathfinding Interplanetary Bus Capability for the Cal Poly CubeSat Laboratory Through the Development of a Phobos-Deimos Mission Concept. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/2209

Chicago Manual of Style (16th Edition):

Ralph, Alyssa M. “Pathfinding Interplanetary Bus Capability for the Cal Poly CubeSat Laboratory Through the Development of a Phobos-Deimos Mission Concept.” 2020. Masters Thesis, Cal Poly. Accessed March 01, 2021. https://digitalcommons.calpoly.edu/theses/2209.

MLA Handbook (7th Edition):

Ralph, Alyssa M. “Pathfinding Interplanetary Bus Capability for the Cal Poly CubeSat Laboratory Through the Development of a Phobos-Deimos Mission Concept.” 2020. Web. 01 Mar 2021.

Vancouver:

Ralph AM. Pathfinding Interplanetary Bus Capability for the Cal Poly CubeSat Laboratory Through the Development of a Phobos-Deimos Mission Concept. [Internet] [Masters thesis]. Cal Poly; 2020. [cited 2021 Mar 01]. Available from: https://digitalcommons.calpoly.edu/theses/2209.

Council of Science Editors:

Ralph AM. Pathfinding Interplanetary Bus Capability for the Cal Poly CubeSat Laboratory Through the Development of a Phobos-Deimos Mission Concept. [Masters Thesis]. Cal Poly; 2020. Available from: https://digitalcommons.calpoly.edu/theses/2209


University of Tennessee – Knoxville

10. Obika, Lumumba Thutmose O. Design of Cessna 210 Radome-Pod Instrument Interface for Flight Testing.

Degree: MS, Aviation Systems, 2012, University of Tennessee – Knoxville

  The purpose of this study was to determine the most appropriate location and design for an instrument interface that can utilize minimum volume within… (more)

Subjects/Keywords: design; Cessna; pod; instrument-interface; flight-testing; Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Obika, L. T. O. (2012). Design of Cessna 210 Radome-Pod Instrument Interface for Flight Testing. (Thesis). University of Tennessee – Knoxville. Retrieved from https://trace.tennessee.edu/utk_gradthes/1322

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

Chicago Manual of Style (16th Edition):

Obika, Lumumba Thutmose O. “Design of Cessna 210 Radome-Pod Instrument Interface for Flight Testing.” 2012. Thesis, University of Tennessee – Knoxville. Accessed March 01, 2021. https://trace.tennessee.edu/utk_gradthes/1322.

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

MLA Handbook (7th Edition):

Obika, Lumumba Thutmose O. “Design of Cessna 210 Radome-Pod Instrument Interface for Flight Testing.” 2012. Web. 01 Mar 2021.

Vancouver:

Obika LTO. Design of Cessna 210 Radome-Pod Instrument Interface for Flight Testing. [Internet] [Thesis]. University of Tennessee – Knoxville; 2012. [cited 2021 Mar 01]. Available from: https://trace.tennessee.edu/utk_gradthes/1322.

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

Council of Science Editors:

Obika LTO. Design of Cessna 210 Radome-Pod Instrument Interface for Flight Testing. [Thesis]. University of Tennessee – Knoxville; 2012. Available from: https://trace.tennessee.edu/utk_gradthes/1322

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


Cal Poly

11. Harper, James M. Pocket Rocket: A 1U+ Propulsion System Design To Enhance CubeSat Capabilities.

Degree: MS, Aerospace Engineering, 2020, Cal Poly

  The research presented provides an overview of a 1U+ form factor propulsion system design developed for the Cal Poly CubeSat Laboratory (CPCL). This design(more)

Subjects/Keywords: Micro-propulsion; Small Satellites; Space Environment; CubeSat Design Specification; Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Harper, J. M. (2020). Pocket Rocket: A 1U+ Propulsion System Design To Enhance CubeSat Capabilities. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/2218

Chicago Manual of Style (16th Edition):

Harper, James M. “Pocket Rocket: A 1U+ Propulsion System Design To Enhance CubeSat Capabilities.” 2020. Masters Thesis, Cal Poly. Accessed March 01, 2021. https://digitalcommons.calpoly.edu/theses/2218.

MLA Handbook (7th Edition):

Harper, James M. “Pocket Rocket: A 1U+ Propulsion System Design To Enhance CubeSat Capabilities.” 2020. Web. 01 Mar 2021.

Vancouver:

Harper JM. Pocket Rocket: A 1U+ Propulsion System Design To Enhance CubeSat Capabilities. [Internet] [Masters thesis]. Cal Poly; 2020. [cited 2021 Mar 01]. Available from: https://digitalcommons.calpoly.edu/theses/2218.

Council of Science Editors:

Harper JM. Pocket Rocket: A 1U+ Propulsion System Design To Enhance CubeSat Capabilities. [Masters Thesis]. Cal Poly; 2020. Available from: https://digitalcommons.calpoly.edu/theses/2218


Embry-Riddle Aeronautical University

12. Vasjaliya, Naishadh G. Fluid-structure Interaction and Multidisciplinary Design Analysis Optimization of Composite Wind Turbine Blade.

Degree: MSin Aerospace Engineering, Aerospace Engineering, 2013, Embry-Riddle Aeronautical University

  A multidisciplinary design analysis optimization (MDAO) process is defined for a composite wind turbine blade to optimize its aerodynamic and structural performance by developing… (more)

Subjects/Keywords: Aerodynamics and Fluid Mechanics; Aerospace Engineering; Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Vasjaliya, N. G. (2013). Fluid-structure Interaction and Multidisciplinary Design Analysis Optimization of Composite Wind Turbine Blade. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/edt/142

Chicago Manual of Style (16th Edition):

Vasjaliya, Naishadh G. “Fluid-structure Interaction and Multidisciplinary Design Analysis Optimization of Composite Wind Turbine Blade.” 2013. Masters Thesis, Embry-Riddle Aeronautical University. Accessed March 01, 2021. https://commons.erau.edu/edt/142.

MLA Handbook (7th Edition):

Vasjaliya, Naishadh G. “Fluid-structure Interaction and Multidisciplinary Design Analysis Optimization of Composite Wind Turbine Blade.” 2013. Web. 01 Mar 2021.

Vancouver:

Vasjaliya NG. Fluid-structure Interaction and Multidisciplinary Design Analysis Optimization of Composite Wind Turbine Blade. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2013. [cited 2021 Mar 01]. Available from: https://commons.erau.edu/edt/142.

Council of Science Editors:

Vasjaliya NG. Fluid-structure Interaction and Multidisciplinary Design Analysis Optimization of Composite Wind Turbine Blade. [Masters Thesis]. Embry-Riddle Aeronautical University; 2013. Available from: https://commons.erau.edu/edt/142


University of Colorado

13. Coolidge, Collin Jennings. Low Pressure Ratio Cascaded Joule-Thomson Cryogenic Coolers.

Degree: PhD, 2017, University of Colorado

 This thesis presents the design, fabrication, and characterization of several coldstages intended to investigate the feasibility of a low pressure ratio three stage cascaded Joule-Thomson… (more)

Subjects/Keywords: cryogenic cooler; low pressure ratio; design optimization; glass capillary; coldstage; Mechanical Engineering; Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Coolidge, C. J. (2017). Low Pressure Ratio Cascaded Joule-Thomson Cryogenic Coolers. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/mcen_gradetds/183

Chicago Manual of Style (16th Edition):

Coolidge, Collin Jennings. “Low Pressure Ratio Cascaded Joule-Thomson Cryogenic Coolers.” 2017. Doctoral Dissertation, University of Colorado. Accessed March 01, 2021. https://scholar.colorado.edu/mcen_gradetds/183.

MLA Handbook (7th Edition):

Coolidge, Collin Jennings. “Low Pressure Ratio Cascaded Joule-Thomson Cryogenic Coolers.” 2017. Web. 01 Mar 2021.

Vancouver:

Coolidge CJ. Low Pressure Ratio Cascaded Joule-Thomson Cryogenic Coolers. [Internet] [Doctoral dissertation]. University of Colorado; 2017. [cited 2021 Mar 01]. Available from: https://scholar.colorado.edu/mcen_gradetds/183.

Council of Science Editors:

Coolidge CJ. Low Pressure Ratio Cascaded Joule-Thomson Cryogenic Coolers. [Doctoral Dissertation]. University of Colorado; 2017. Available from: https://scholar.colorado.edu/mcen_gradetds/183


Cal Poly

14. Lunsford, Ian M. SUBSYSTEM FAILURE ANALYSIS WITHIN THE HORIZON SIMULATION FRAMEWORK.

Degree: MS, Aerospace Engineering, 2016, Cal Poly

  System design is an inherently expensive and time consuming process. Engineers are constantly tasked to investigate new solutions for various programs. Model-based systems engineering(more)

Subjects/Keywords: Horizon Simulation Framework; Model-based Systems Engineering; Simulations; Modeling; Systems Engineering; MBSE; Model-based Engineering; Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Lunsford, I. M. (2016). SUBSYSTEM FAILURE ANALYSIS WITHIN THE HORIZON SIMULATION FRAMEWORK. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1560 ; 10.15368/theses.2016.40

Chicago Manual of Style (16th Edition):

Lunsford, Ian M. “SUBSYSTEM FAILURE ANALYSIS WITHIN THE HORIZON SIMULATION FRAMEWORK.” 2016. Masters Thesis, Cal Poly. Accessed March 01, 2021. https://digitalcommons.calpoly.edu/theses/1560 ; 10.15368/theses.2016.40.

MLA Handbook (7th Edition):

Lunsford, Ian M. “SUBSYSTEM FAILURE ANALYSIS WITHIN THE HORIZON SIMULATION FRAMEWORK.” 2016. Web. 01 Mar 2021.

Vancouver:

Lunsford IM. SUBSYSTEM FAILURE ANALYSIS WITHIN THE HORIZON SIMULATION FRAMEWORK. [Internet] [Masters thesis]. Cal Poly; 2016. [cited 2021 Mar 01]. Available from: https://digitalcommons.calpoly.edu/theses/1560 ; 10.15368/theses.2016.40.

Council of Science Editors:

Lunsford IM. SUBSYSTEM FAILURE ANALYSIS WITHIN THE HORIZON SIMULATION FRAMEWORK. [Masters Thesis]. Cal Poly; 2016. Available from: https://digitalcommons.calpoly.edu/theses/1560 ; 10.15368/theses.2016.40


Florida International University

15. Busam, Arvind Kumar. Optimization of waiting time at toll plazas.

Degree: MS, Please see currently inactive department below., 2005, Florida International University

  Toll plazas have several toll payment types such as manual, automatic coin machines, electronic and mixed lanes. In places with high traffic flow, the… (more)

Subjects/Keywords: Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Busam, A. K. (2005). Optimization of waiting time at toll plazas. (Thesis). Florida International University. Retrieved from https://digitalcommons.fiu.edu/etd/1898 ; 10.25148/etd.FI14051895 ; FI14051895

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

Chicago Manual of Style (16th Edition):

Busam, Arvind Kumar. “Optimization of waiting time at toll plazas.” 2005. Thesis, Florida International University. Accessed March 01, 2021. https://digitalcommons.fiu.edu/etd/1898 ; 10.25148/etd.FI14051895 ; FI14051895.

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

MLA Handbook (7th Edition):

Busam, Arvind Kumar. “Optimization of waiting time at toll plazas.” 2005. Web. 01 Mar 2021.

Vancouver:

Busam AK. Optimization of waiting time at toll plazas. [Internet] [Thesis]. Florida International University; 2005. [cited 2021 Mar 01]. Available from: https://digitalcommons.fiu.edu/etd/1898 ; 10.25148/etd.FI14051895 ; FI14051895.

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

Council of Science Editors:

Busam AK. Optimization of waiting time at toll plazas. [Thesis]. Florida International University; 2005. Available from: https://digitalcommons.fiu.edu/etd/1898 ; 10.25148/etd.FI14051895 ; FI14051895

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


Cal Poly

16. Johnson, Alexander W. CubeSat Astronomy Mission Modeling Using the Horizon Simulation Framework.

Degree: MS, Aerospace Engineering, 2019, Cal Poly

  The CubeSat Astronomy Network is a proposed system of multiple CubeSat spacecraft capable of performing follow-up observations of astronomical targets of interest. The system… (more)

Subjects/Keywords: cubesat; astronomy; horizon; simulation; framework; modeling; Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Johnson, A. W. (2019). CubeSat Astronomy Mission Modeling Using the Horizon Simulation Framework. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/2067 ; 10.15368/theses.2019.94

Chicago Manual of Style (16th Edition):

Johnson, Alexander W. “CubeSat Astronomy Mission Modeling Using the Horizon Simulation Framework.” 2019. Masters Thesis, Cal Poly. Accessed March 01, 2021. https://digitalcommons.calpoly.edu/theses/2067 ; 10.15368/theses.2019.94.

MLA Handbook (7th Edition):

Johnson, Alexander W. “CubeSat Astronomy Mission Modeling Using the Horizon Simulation Framework.” 2019. Web. 01 Mar 2021.

Vancouver:

Johnson AW. CubeSat Astronomy Mission Modeling Using the Horizon Simulation Framework. [Internet] [Masters thesis]. Cal Poly; 2019. [cited 2021 Mar 01]. Available from: https://digitalcommons.calpoly.edu/theses/2067 ; 10.15368/theses.2019.94.

Council of Science Editors:

Johnson AW. CubeSat Astronomy Mission Modeling Using the Horizon Simulation Framework. [Masters Thesis]. Cal Poly; 2019. Available from: https://digitalcommons.calpoly.edu/theses/2067 ; 10.15368/theses.2019.94


Cal Poly

17. Luther, Shaun. SYSML BASED CUBESAT MODEL DESIGN AND INTEGRATION WITH THE HORIZON SIMULATION FRAMEWORK.

Degree: MS, Aerospace Engineering, 2016, Cal Poly

  This thesis examines the feasibility of substituting the system input script of Cal Poly’s Horizon Simulation Framework (HSF) with a Model Based Systems Engineering(more)

Subjects/Keywords: SysML; HSF; CubeSat; Simulation; Model; Space Vehicles; Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Luther, S. (2016). SYSML BASED CUBESAT MODEL DESIGN AND INTEGRATION WITH THE HORIZON SIMULATION FRAMEWORK. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1591 ; 10.15368/theses.2016.63

Chicago Manual of Style (16th Edition):

Luther, Shaun. “SYSML BASED CUBESAT MODEL DESIGN AND INTEGRATION WITH THE HORIZON SIMULATION FRAMEWORK.” 2016. Masters Thesis, Cal Poly. Accessed March 01, 2021. https://digitalcommons.calpoly.edu/theses/1591 ; 10.15368/theses.2016.63.

MLA Handbook (7th Edition):

Luther, Shaun. “SYSML BASED CUBESAT MODEL DESIGN AND INTEGRATION WITH THE HORIZON SIMULATION FRAMEWORK.” 2016. Web. 01 Mar 2021.

Vancouver:

Luther S. SYSML BASED CUBESAT MODEL DESIGN AND INTEGRATION WITH THE HORIZON SIMULATION FRAMEWORK. [Internet] [Masters thesis]. Cal Poly; 2016. [cited 2021 Mar 01]. Available from: https://digitalcommons.calpoly.edu/theses/1591 ; 10.15368/theses.2016.63.

Council of Science Editors:

Luther S. SYSML BASED CUBESAT MODEL DESIGN AND INTEGRATION WITH THE HORIZON SIMULATION FRAMEWORK. [Masters Thesis]. Cal Poly; 2016. Available from: https://digitalcommons.calpoly.edu/theses/1591 ; 10.15368/theses.2016.63


Cal Poly

18. Blocher, Andrew Gene. Alternative Mission Concepts for the Exploration of Outer Planets Using Small Satellite Swarms.

Degree: MS, Aerospace Engineering, 2017, Cal Poly

  Interplanetary space exploration has thus far consisted of single, expensive spacecraft missions. Mission costs are particularly high on missions to the outer planets and… (more)

Subjects/Keywords: Cassini; Saturn; CubeSat; Interplanetary; Architecture; Satellite; Instrumentation; Space Vehicles; Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Blocher, A. G. (2017). Alternative Mission Concepts for the Exploration of Outer Planets Using Small Satellite Swarms. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1820 ; 10.15368/theses.2018.22

Chicago Manual of Style (16th Edition):

Blocher, Andrew Gene. “Alternative Mission Concepts for the Exploration of Outer Planets Using Small Satellite Swarms.” 2017. Masters Thesis, Cal Poly. Accessed March 01, 2021. https://digitalcommons.calpoly.edu/theses/1820 ; 10.15368/theses.2018.22.

MLA Handbook (7th Edition):

Blocher, Andrew Gene. “Alternative Mission Concepts for the Exploration of Outer Planets Using Small Satellite Swarms.” 2017. Web. 01 Mar 2021.

Vancouver:

Blocher AG. Alternative Mission Concepts for the Exploration of Outer Planets Using Small Satellite Swarms. [Internet] [Masters thesis]. Cal Poly; 2017. [cited 2021 Mar 01]. Available from: https://digitalcommons.calpoly.edu/theses/1820 ; 10.15368/theses.2018.22.

Council of Science Editors:

Blocher AG. Alternative Mission Concepts for the Exploration of Outer Planets Using Small Satellite Swarms. [Masters Thesis]. Cal Poly; 2017. Available from: https://digitalcommons.calpoly.edu/theses/1820 ; 10.15368/theses.2018.22


University of Tennessee – Knoxville

19. Croxson, Robert Donald. Integration of the Control Display Navigation Unit (CDNU) Into the EA-6B Block 89A Aircraft and its Impact on Navigation Operations.

Degree: MS, Aviation Systems, 2002, University of Tennessee – Knoxville

  This thesis was to evaluate the attributes of the recent modification and installation of the Control Display Navigation Unit (CDNU) into the EA-6B aircraft.… (more)

Subjects/Keywords: Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Croxson, R. D. (2002). Integration of the Control Display Navigation Unit (CDNU) Into the EA-6B Block 89A Aircraft and its Impact on Navigation Operations. (Thesis). University of Tennessee – Knoxville. Retrieved from https://trace.tennessee.edu/utk_gradthes/2041

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

Chicago Manual of Style (16th Edition):

Croxson, Robert Donald. “Integration of the Control Display Navigation Unit (CDNU) Into the EA-6B Block 89A Aircraft and its Impact on Navigation Operations.” 2002. Thesis, University of Tennessee – Knoxville. Accessed March 01, 2021. https://trace.tennessee.edu/utk_gradthes/2041.

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

MLA Handbook (7th Edition):

Croxson, Robert Donald. “Integration of the Control Display Navigation Unit (CDNU) Into the EA-6B Block 89A Aircraft and its Impact on Navigation Operations.” 2002. Web. 01 Mar 2021.

Vancouver:

Croxson RD. Integration of the Control Display Navigation Unit (CDNU) Into the EA-6B Block 89A Aircraft and its Impact on Navigation Operations. [Internet] [Thesis]. University of Tennessee – Knoxville; 2002. [cited 2021 Mar 01]. Available from: https://trace.tennessee.edu/utk_gradthes/2041.

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

Council of Science Editors:

Croxson RD. Integration of the Control Display Navigation Unit (CDNU) Into the EA-6B Block 89A Aircraft and its Impact on Navigation Operations. [Thesis]. University of Tennessee – Knoxville; 2002. Available from: https://trace.tennessee.edu/utk_gradthes/2041

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


University of Tennessee – Knoxville

20. Clark, Timothy R. Evaluation of a Two-way Datalink for Airborne Surveillance of and Communication with a Remotely Operated Aircraft Operating in the National Airspace System.

Degree: MS, Aviation Systems, 2002, University of Tennessee – Knoxville

  The purpose of this study is to examine the use of a two-way digital datalink to implement the airborne surveillance and communication functions with… (more)

Subjects/Keywords: Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Clark, T. R. (2002). Evaluation of a Two-way Datalink for Airborne Surveillance of and Communication with a Remotely Operated Aircraft Operating in the National Airspace System. (Thesis). University of Tennessee – Knoxville. Retrieved from https://trace.tennessee.edu/utk_gradthes/2044

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

Chicago Manual of Style (16th Edition):

Clark, Timothy R. “Evaluation of a Two-way Datalink for Airborne Surveillance of and Communication with a Remotely Operated Aircraft Operating in the National Airspace System.” 2002. Thesis, University of Tennessee – Knoxville. Accessed March 01, 2021. https://trace.tennessee.edu/utk_gradthes/2044.

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

MLA Handbook (7th Edition):

Clark, Timothy R. “Evaluation of a Two-way Datalink for Airborne Surveillance of and Communication with a Remotely Operated Aircraft Operating in the National Airspace System.” 2002. Web. 01 Mar 2021.

Vancouver:

Clark TR. Evaluation of a Two-way Datalink for Airborne Surveillance of and Communication with a Remotely Operated Aircraft Operating in the National Airspace System. [Internet] [Thesis]. University of Tennessee – Knoxville; 2002. [cited 2021 Mar 01]. Available from: https://trace.tennessee.edu/utk_gradthes/2044.

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

Council of Science Editors:

Clark TR. Evaluation of a Two-way Datalink for Airborne Surveillance of and Communication with a Remotely Operated Aircraft Operating in the National Airspace System. [Thesis]. University of Tennessee – Knoxville; 2002. Available from: https://trace.tennessee.edu/utk_gradthes/2044

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


University of Tennessee – Knoxville

21. Goszkowicz, Brian J. Sidestick Controllers During High Gain Tasks.

Degree: MS, Aviation Systems, 2002, University of Tennessee – Knoxville

  This research attempts to demonstrate the feasibility of a sidestick controller in a high gain environment. The research is assembled from several historical precedents… (more)

Subjects/Keywords: Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Goszkowicz, B. J. (2002). Sidestick Controllers During High Gain Tasks. (Thesis). University of Tennessee – Knoxville. Retrieved from https://trace.tennessee.edu/utk_gradthes/2060

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

Chicago Manual of Style (16th Edition):

Goszkowicz, Brian J. “Sidestick Controllers During High Gain Tasks.” 2002. Thesis, University of Tennessee – Knoxville. Accessed March 01, 2021. https://trace.tennessee.edu/utk_gradthes/2060.

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

MLA Handbook (7th Edition):

Goszkowicz, Brian J. “Sidestick Controllers During High Gain Tasks.” 2002. Web. 01 Mar 2021.

Vancouver:

Goszkowicz BJ. Sidestick Controllers During High Gain Tasks. [Internet] [Thesis]. University of Tennessee – Knoxville; 2002. [cited 2021 Mar 01]. Available from: https://trace.tennessee.edu/utk_gradthes/2060.

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

Council of Science Editors:

Goszkowicz BJ. Sidestick Controllers During High Gain Tasks. [Thesis]. University of Tennessee – Knoxville; 2002. Available from: https://trace.tennessee.edu/utk_gradthes/2060

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


University of Tennessee – Knoxville

22. Bigalk, Gregory D. Implementation of the Digital Communication System in the F/A-18 Aircraft.

Degree: MS, Aviation Systems, 2002, University of Tennessee – Knoxville

  The F/A-18 Hornet is a Navy/Marine Corps carrier-based strike/fighter built by the Boeing Company. The Hornet is a dual role aircraft designed to have… (more)

Subjects/Keywords: Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Bigalk, G. D. (2002). Implementation of the Digital Communication System in the F/A-18 Aircraft. (Thesis). University of Tennessee – Knoxville. Retrieved from https://trace.tennessee.edu/utk_gradthes/2029

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

Chicago Manual of Style (16th Edition):

Bigalk, Gregory D. “Implementation of the Digital Communication System in the F/A-18 Aircraft.” 2002. Thesis, University of Tennessee – Knoxville. Accessed March 01, 2021. https://trace.tennessee.edu/utk_gradthes/2029.

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

MLA Handbook (7th Edition):

Bigalk, Gregory D. “Implementation of the Digital Communication System in the F/A-18 Aircraft.” 2002. Web. 01 Mar 2021.

Vancouver:

Bigalk GD. Implementation of the Digital Communication System in the F/A-18 Aircraft. [Internet] [Thesis]. University of Tennessee – Knoxville; 2002. [cited 2021 Mar 01]. Available from: https://trace.tennessee.edu/utk_gradthes/2029.

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

Council of Science Editors:

Bigalk GD. Implementation of the Digital Communication System in the F/A-18 Aircraft. [Thesis]. University of Tennessee – Knoxville; 2002. Available from: https://trace.tennessee.edu/utk_gradthes/2029

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


Cal Poly

23. Kross, Cory Kenneth. A Method for Evaluating Aircraft Electric Power System Sizing and Failure Resiliency.

Degree: MS, Electrical Engineering, 2017, Cal Poly

  With the More Electric Aircraft paradigm, commercial commuter aircraft are increasing the size and complexity of electrical power systems by increasing the number of… (more)

Subjects/Keywords: Aircraft; Power; Optimization; Reliability; Failure; Reconfiguration; Electrical and Computer Engineering; Power and Energy; Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Kross, C. K. (2017). A Method for Evaluating Aircraft Electric Power System Sizing and Failure Resiliency. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1709 ; 10.15368/theses.2017.14

Chicago Manual of Style (16th Edition):

Kross, Cory Kenneth. “A Method for Evaluating Aircraft Electric Power System Sizing and Failure Resiliency.” 2017. Masters Thesis, Cal Poly. Accessed March 01, 2021. https://digitalcommons.calpoly.edu/theses/1709 ; 10.15368/theses.2017.14.

MLA Handbook (7th Edition):

Kross, Cory Kenneth. “A Method for Evaluating Aircraft Electric Power System Sizing and Failure Resiliency.” 2017. Web. 01 Mar 2021.

Vancouver:

Kross CK. A Method for Evaluating Aircraft Electric Power System Sizing and Failure Resiliency. [Internet] [Masters thesis]. Cal Poly; 2017. [cited 2021 Mar 01]. Available from: https://digitalcommons.calpoly.edu/theses/1709 ; 10.15368/theses.2017.14.

Council of Science Editors:

Kross CK. A Method for Evaluating Aircraft Electric Power System Sizing and Failure Resiliency. [Masters Thesis]. Cal Poly; 2017. Available from: https://digitalcommons.calpoly.edu/theses/1709 ; 10.15368/theses.2017.14


Iowa State University

24. Kannan, Hanumanthrao. An MDO augmented value-based systems engineering approach to holistic design decision-making: a satellite system case study.

Degree: 2015, Iowa State University

 The design of large scale complex engineered systems (LSCES) involves hundreds or thousands of designers making decisions at different levels of an organizational hierarchy. Traditionally,… (more)

Subjects/Keywords: Aerospace Engineering; Decision Analysis (DA); Multidisciplinary Design Optimization (MDO); Satellite system design; Spacecraft design; Value-Based Systems Engineering (VBSE); Value-Driven Design (VDD); Aerospace Engineering; Industrial Engineering; Systems Engineering; Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Kannan, H. (2015). An MDO augmented value-based systems engineering approach to holistic design decision-making: a satellite system case study. (Thesis). Iowa State University. Retrieved from https://lib.dr.iastate.edu/etd/14843

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

Chicago Manual of Style (16th Edition):

Kannan, Hanumanthrao. “An MDO augmented value-based systems engineering approach to holistic design decision-making: a satellite system case study.” 2015. Thesis, Iowa State University. Accessed March 01, 2021. https://lib.dr.iastate.edu/etd/14843.

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

MLA Handbook (7th Edition):

Kannan, Hanumanthrao. “An MDO augmented value-based systems engineering approach to holistic design decision-making: a satellite system case study.” 2015. Web. 01 Mar 2021.

Vancouver:

Kannan H. An MDO augmented value-based systems engineering approach to holistic design decision-making: a satellite system case study. [Internet] [Thesis]. Iowa State University; 2015. [cited 2021 Mar 01]. Available from: https://lib.dr.iastate.edu/etd/14843.

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

Council of Science Editors:

Kannan H. An MDO augmented value-based systems engineering approach to holistic design decision-making: a satellite system case study. [Thesis]. Iowa State University; 2015. Available from: https://lib.dr.iastate.edu/etd/14843

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


Kennesaw State University

25. Sisson, Taylor Jay. The Context of Tool Control in an Aircraft Assembly Environment Related to Productivity.

Degree: 2016, Kennesaw State University

  The aircraft industry focuses a large portion of its resources on tool control during the assembly of aircraft. Tool control is a strict process… (more)

Subjects/Keywords: tool control; industrial engineering; optimization; aircraft manufacturing; Other Operations Research, Systems Engineering and Industrial Engineering; Systems Engineering; Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Sisson, T. J. (2016). The Context of Tool Control in an Aircraft Assembly Environment Related to Productivity. (Thesis). Kennesaw State University. Retrieved from https://digitalcommons.kennesaw.edu/honors_etd/3

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

Chicago Manual of Style (16th Edition):

Sisson, Taylor Jay. “The Context of Tool Control in an Aircraft Assembly Environment Related to Productivity.” 2016. Thesis, Kennesaw State University. Accessed March 01, 2021. https://digitalcommons.kennesaw.edu/honors_etd/3.

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

MLA Handbook (7th Edition):

Sisson, Taylor Jay. “The Context of Tool Control in an Aircraft Assembly Environment Related to Productivity.” 2016. Web. 01 Mar 2021.

Vancouver:

Sisson TJ. The Context of Tool Control in an Aircraft Assembly Environment Related to Productivity. [Internet] [Thesis]. Kennesaw State University; 2016. [cited 2021 Mar 01]. Available from: https://digitalcommons.kennesaw.edu/honors_etd/3.

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

Council of Science Editors:

Sisson TJ. The Context of Tool Control in an Aircraft Assembly Environment Related to Productivity. [Thesis]. Kennesaw State University; 2016. Available from: https://digitalcommons.kennesaw.edu/honors_etd/3

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


University of Cincinnati

26. Houshmand, Arian. Multidisciplinary Dynamic System Design Optimization of Hybrid Electric Vehicle Powertrains.

Degree: MS, Engineering and Applied Science: Mechanical Engineering, 2016, University of Cincinnati

 The design of large-scale, complex systems such as plug-in hybrid electric vehicles (PHEVs) motivates the use of formal optimization methods from both multidisciplinary design optimization(more)

Subjects/Keywords: Mechanical Engineering; Mechanics; combined design and control optimization; multidisciplinary dynamic system design optimizati; large-scale systems; plug-in hybrid electric vehicles

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APA (6th Edition):

Houshmand, A. (2016). Multidisciplinary Dynamic System Design Optimization of Hybrid Electric Vehicle Powertrains. (Masters Thesis). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1479822276400281

Chicago Manual of Style (16th Edition):

Houshmand, Arian. “Multidisciplinary Dynamic System Design Optimization of Hybrid Electric Vehicle Powertrains.” 2016. Masters Thesis, University of Cincinnati. Accessed March 01, 2021. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1479822276400281.

MLA Handbook (7th Edition):

Houshmand, Arian. “Multidisciplinary Dynamic System Design Optimization of Hybrid Electric Vehicle Powertrains.” 2016. Web. 01 Mar 2021.

Vancouver:

Houshmand A. Multidisciplinary Dynamic System Design Optimization of Hybrid Electric Vehicle Powertrains. [Internet] [Masters thesis]. University of Cincinnati; 2016. [cited 2021 Mar 01]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1479822276400281.

Council of Science Editors:

Houshmand A. Multidisciplinary Dynamic System Design Optimization of Hybrid Electric Vehicle Powertrains. [Masters Thesis]. University of Cincinnati; 2016. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1479822276400281


Florida International University

27. Reddy, Sohail. Many-Objective Hybrid Optimization Under Uncertainty With Applications.

Degree: PhD, Mechanical Engineering, 2019, Florida International University

  A novel method for solving many-objective optimization problems under uncertainty was developed. It is well known that no single optimization algorithm performs best for… (more)

Subjects/Keywords: Hybrid Optimization; Uncertainty Quantification; Many-Objective Optimization; Fast Multipole Method; Aerodynamic Optimization; Aerodynamics and Fluid Mechanics; Other Mechanical Engineering; Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Reddy, S. (2019). Many-Objective Hybrid Optimization Under Uncertainty With Applications. (Doctoral Dissertation). Florida International University. Retrieved from https://digitalcommons.fiu.edu/etd/4369 ; FIDC008890

Chicago Manual of Style (16th Edition):

Reddy, Sohail. “Many-Objective Hybrid Optimization Under Uncertainty With Applications.” 2019. Doctoral Dissertation, Florida International University. Accessed March 01, 2021. https://digitalcommons.fiu.edu/etd/4369 ; FIDC008890.

MLA Handbook (7th Edition):

Reddy, Sohail. “Many-Objective Hybrid Optimization Under Uncertainty With Applications.” 2019. Web. 01 Mar 2021.

Vancouver:

Reddy S. Many-Objective Hybrid Optimization Under Uncertainty With Applications. [Internet] [Doctoral dissertation]. Florida International University; 2019. [cited 2021 Mar 01]. Available from: https://digitalcommons.fiu.edu/etd/4369 ; FIDC008890.

Council of Science Editors:

Reddy S. Many-Objective Hybrid Optimization Under Uncertainty With Applications. [Doctoral Dissertation]. Florida International University; 2019. Available from: https://digitalcommons.fiu.edu/etd/4369 ; FIDC008890


Embry-Riddle Aeronautical University

28. Kazeneh, Ali. Development of Automatic CFD Grid Generation for the Design of the Preliminary Wing Sweep Schedule for the Gulfstream Quiet Supersonic Jet.

Degree: Master of Aerospace Engineering, Aerospace Engineering, 2008, Embry-Riddle Aeronautical University

  The wing sweep schedule for the Gulfstream Quiet Supersonic Jet (wing and body) was investigated using CFD analysis methods. The use of automating the… (more)

Subjects/Keywords: Aerospace Engineering; Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Kazeneh, A. (2008). Development of Automatic CFD Grid Generation for the Design of the Preliminary Wing Sweep Schedule for the Gulfstream Quiet Supersonic Jet. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/db-theses/95

Chicago Manual of Style (16th Edition):

Kazeneh, Ali. “Development of Automatic CFD Grid Generation for the Design of the Preliminary Wing Sweep Schedule for the Gulfstream Quiet Supersonic Jet.” 2008. Masters Thesis, Embry-Riddle Aeronautical University. Accessed March 01, 2021. https://commons.erau.edu/db-theses/95.

MLA Handbook (7th Edition):

Kazeneh, Ali. “Development of Automatic CFD Grid Generation for the Design of the Preliminary Wing Sweep Schedule for the Gulfstream Quiet Supersonic Jet.” 2008. Web. 01 Mar 2021.

Vancouver:

Kazeneh A. Development of Automatic CFD Grid Generation for the Design of the Preliminary Wing Sweep Schedule for the Gulfstream Quiet Supersonic Jet. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2008. [cited 2021 Mar 01]. Available from: https://commons.erau.edu/db-theses/95.

Council of Science Editors:

Kazeneh A. Development of Automatic CFD Grid Generation for the Design of the Preliminary Wing Sweep Schedule for the Gulfstream Quiet Supersonic Jet. [Masters Thesis]. Embry-Riddle Aeronautical University; 2008. Available from: https://commons.erau.edu/db-theses/95


Embry-Riddle Aeronautical University

29. Kertesz, Steve, Jr. A comparison of Pseudo 3-Dimensional Collision Avoidance-Predictor Displays for Free Flight.

Degree: Master of Aeronautical Science, Aeronautical Science, 1998, Embry-Riddle Aeronautical University

  This study was the second of two studies to evaluate the use of a pseudo threedimensional display to present information about future possible conflicts.… (more)

Subjects/Keywords: Aerospace Engineering; Aviation; Systems Engineering and Multidisciplinary Design Optimization

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

APA (6th Edition):

Kertesz, Steve, J. (1998). A comparison of Pseudo 3-Dimensional Collision Avoidance-Predictor Displays for Free Flight. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/db-theses/96

Chicago Manual of Style (16th Edition):

Kertesz, Steve, Jr. “A comparison of Pseudo 3-Dimensional Collision Avoidance-Predictor Displays for Free Flight.” 1998. Masters Thesis, Embry-Riddle Aeronautical University. Accessed March 01, 2021. https://commons.erau.edu/db-theses/96.

MLA Handbook (7th Edition):

Kertesz, Steve, Jr. “A comparison of Pseudo 3-Dimensional Collision Avoidance-Predictor Displays for Free Flight.” 1998. Web. 01 Mar 2021.

Vancouver:

Kertesz, Steve J. A comparison of Pseudo 3-Dimensional Collision Avoidance-Predictor Displays for Free Flight. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 1998. [cited 2021 Mar 01]. Available from: https://commons.erau.edu/db-theses/96.

Council of Science Editors:

Kertesz, Steve J. A comparison of Pseudo 3-Dimensional Collision Avoidance-Predictor Displays for Free Flight. [Masters Thesis]. Embry-Riddle Aeronautical University; 1998. Available from: https://commons.erau.edu/db-theses/96


Embry-Riddle Aeronautical University

30. Tada, Hiroko. An Intermittent-Combustion General Aviation Aircraft Engine Exhaust Noise prediction Algorithm.

Degree: MSin Aerospace Engineering, Aerospace Engineering, 1999, Embry-Riddle Aeronautical University

  From an environmental point of view, the reduction of aircraft noise has become an important factor recently. There are two factors that make airplane… (more)

Subjects/Keywords: Aerospace Engineering; Systems Engineering and Multidisciplinary Design Optimization

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

APA (6th Edition):

Tada, H. (1999). An Intermittent-Combustion General Aviation Aircraft Engine Exhaust Noise prediction Algorithm. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/db-theses/195

Chicago Manual of Style (16th Edition):

Tada, Hiroko. “An Intermittent-Combustion General Aviation Aircraft Engine Exhaust Noise prediction Algorithm.” 1999. Masters Thesis, Embry-Riddle Aeronautical University. Accessed March 01, 2021. https://commons.erau.edu/db-theses/195.

MLA Handbook (7th Edition):

Tada, Hiroko. “An Intermittent-Combustion General Aviation Aircraft Engine Exhaust Noise prediction Algorithm.” 1999. Web. 01 Mar 2021.

Vancouver:

Tada H. An Intermittent-Combustion General Aviation Aircraft Engine Exhaust Noise prediction Algorithm. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 1999. [cited 2021 Mar 01]. Available from: https://commons.erau.edu/db-theses/195.

Council of Science Editors:

Tada H. An Intermittent-Combustion General Aviation Aircraft Engine Exhaust Noise prediction Algorithm. [Masters Thesis]. Embry-Riddle Aeronautical University; 1999. Available from: https://commons.erau.edu/db-theses/195

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