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Dept: Aerospace Engineering

You searched for subject:(HOUSING DESIGN ARCHITECTURE ). Showing records 1 – 30 of 320 total matches.

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Cal Poly

1. 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

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 October 17, 2019. https://digitalcommons.calpoly.edu/theses/1820.

MLA Handbook (7th Edition):

Blocher, Andrew Gene. “Alternative Mission Concepts for the Exploration of Outer Planets Using Small Satellite Swarms.” 2017. Web. 17 Oct 2019.

Vancouver:

Blocher AG. Alternative Mission Concepts for the Exploration of Outer Planets Using Small Satellite Swarms. [Internet] [Masters thesis]. Cal Poly; 2017. [cited 2019 Oct 17]. Available from: https://digitalcommons.calpoly.edu/theses/1820.

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

2. Sharma, Jonathan. STASE: set theory-influenced architecture space exploration.

Degree: PhD, Aerospace Engineering, 2014, Georgia Tech

 The first of NASA's high-level strategic goals is to extend and sustain human activities across the solar system. As the United States moves into the… (more)

Subjects/Keywords: Set theory; Architecture space exploration; Method; Early design; Systems engineering

Architecture Space to Design Space . . . . 111 7 Canonical Example MOA… …the Mappings Between the Architecture Space and Design Space… …Description . . . . . . . . . . . 189 23 Point Design ID 47517 Architecture Space Description… …Mappings Between Architecture Space and Design Space . . . . . . . 82 49 Varying Design… …Alternative Representation of an Individual System Architecture in the Design Space… 

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APA (6th Edition):

Sharma, J. (2014). STASE: set theory-influenced architecture space exploration. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/52330

Chicago Manual of Style (16th Edition):

Sharma, Jonathan. “STASE: set theory-influenced architecture space exploration.” 2014. Doctoral Dissertation, Georgia Tech. Accessed October 17, 2019. http://hdl.handle.net/1853/52330.

MLA Handbook (7th Edition):

Sharma, Jonathan. “STASE: set theory-influenced architecture space exploration.” 2014. Web. 17 Oct 2019.

Vancouver:

Sharma J. STASE: set theory-influenced architecture space exploration. [Internet] [Doctoral dissertation]. Georgia Tech; 2014. [cited 2019 Oct 17]. Available from: http://hdl.handle.net/1853/52330.

Council of Science Editors:

Sharma J. STASE: set theory-influenced architecture space exploration. [Doctoral Dissertation]. Georgia Tech; 2014. Available from: http://hdl.handle.net/1853/52330


Georgia Tech

3. Young, David Anthony. An Innovative Methodology for Allocating Reliability and Cost in a Lunar Exploration Architecture.

Degree: PhD, Aerospace Engineering, 2007, Georgia Tech

 In January 2005, President Bush announced the Vision for Space Exploration. This vision involved a progressive expansion of human capabilities beyond Low Earth Orbit beginning… (more)

Subjects/Keywords: Lunar Architecture; Cost; Reliability; Apollo; ESAS; Allocation; Optimization; Space vehicles Design and construction; Multidisciplinary design optimization; Decision making

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APA (6th Edition):

Young, D. A. (2007). An Innovative Methodology for Allocating Reliability and Cost in a Lunar Exploration Architecture. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/14498

Chicago Manual of Style (16th Edition):

Young, David Anthony. “An Innovative Methodology for Allocating Reliability and Cost in a Lunar Exploration Architecture.” 2007. Doctoral Dissertation, Georgia Tech. Accessed October 17, 2019. http://hdl.handle.net/1853/14498.

MLA Handbook (7th Edition):

Young, David Anthony. “An Innovative Methodology for Allocating Reliability and Cost in a Lunar Exploration Architecture.” 2007. Web. 17 Oct 2019.

Vancouver:

Young DA. An Innovative Methodology for Allocating Reliability and Cost in a Lunar Exploration Architecture. [Internet] [Doctoral dissertation]. Georgia Tech; 2007. [cited 2019 Oct 17]. Available from: http://hdl.handle.net/1853/14498.

Council of Science Editors:

Young DA. An Innovative Methodology for Allocating Reliability and Cost in a Lunar Exploration Architecture. [Doctoral Dissertation]. Georgia Tech; 2007. Available from: http://hdl.handle.net/1853/14498

4. Nairouz, Bassem R. Conceptual design methodology of distributed intelligence large scale systems.

Degree: PhD, Aerospace Engineering, 2013, Georgia Tech

 Distributed intelligence systems are starting to gain dominance in the field of large-scale complex systems. These systems are characterized by nonlinear behavior patterns that are… (more)

Subjects/Keywords: Systems design; Control architecture; Architecture; Metamodel; Meta-model; Conceptual design; Expert systems (Computer science); Electronic data processing Distributed processing; Systems engineering

…Physical Design B - Two Link Design . . . . . . . . . . . . 133 Control Architecture Analysis… …ARCHITECTURE DESIGN OF A MULTINETWORK COMPLEX SYSTEM . . . . . . . . . . . . . . . . . . . . . 187… …Hybrid Design Process . . . . . . . . . . 248 Control Architecture Meta-model… …Architecture Design Efforts . . . . . . . . . . . . . . 18 8 Challenges of Intelligent Systems… …Design Steps . . . . . . . . . . . . . . . . . . . 81 29 Control Architecture Requires Three… 

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APA (6th Edition):

Nairouz, B. R. (2013). Conceptual design methodology of distributed intelligence large scale systems. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/49077

Chicago Manual of Style (16th Edition):

Nairouz, Bassem R. “Conceptual design methodology of distributed intelligence large scale systems.” 2013. Doctoral Dissertation, Georgia Tech. Accessed October 17, 2019. http://hdl.handle.net/1853/49077.

MLA Handbook (7th Edition):

Nairouz, Bassem R. “Conceptual design methodology of distributed intelligence large scale systems.” 2013. Web. 17 Oct 2019.

Vancouver:

Nairouz BR. Conceptual design methodology of distributed intelligence large scale systems. [Internet] [Doctoral dissertation]. Georgia Tech; 2013. [cited 2019 Oct 17]. Available from: http://hdl.handle.net/1853/49077.

Council of Science Editors:

Nairouz BR. Conceptual design methodology of distributed intelligence large scale systems. [Doctoral Dissertation]. Georgia Tech; 2013. Available from: http://hdl.handle.net/1853/49077

5. Armstrong, Michael James. A process for function based architecture definition and modeling.

Degree: MS, Aerospace Engineering, 2008, Georgia Tech

 Developments in electric technologies have the potential to increase the efficiency and performance of commercial aircraft. However, without proper architecture innovation, technology developments at the… (more)

Subjects/Keywords: Architecture; Design; Architecting; Architecture design environment; Induced function; Morphological matrix; Simulation; Functional decomposition; Complex system; Modeling; Integrated system; Function; Functions; Airplanes – Performance; Airframes

…109 8. Aircraft Architecture Design Space Definition… …172 Appendix C: Architecture Design Environment (ADENII)… …63 Figure 29: Architecture Design Tools… …129 Figure 65: Architecture Design Space… …innovative architectural elements. A function-based process for innovative architecture design was… 

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APA (6th Edition):

Armstrong, M. J. (2008). A process for function based architecture definition and modeling. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/26631

Chicago Manual of Style (16th Edition):

Armstrong, Michael James. “A process for function based architecture definition and modeling.” 2008. Masters Thesis, Georgia Tech. Accessed October 17, 2019. http://hdl.handle.net/1853/26631.

MLA Handbook (7th Edition):

Armstrong, Michael James. “A process for function based architecture definition and modeling.” 2008. Web. 17 Oct 2019.

Vancouver:

Armstrong MJ. A process for function based architecture definition and modeling. [Internet] [Masters thesis]. Georgia Tech; 2008. [cited 2019 Oct 17]. Available from: http://hdl.handle.net/1853/26631.

Council of Science Editors:

Armstrong MJ. A process for function based architecture definition and modeling. [Masters Thesis]. Georgia Tech; 2008. Available from: http://hdl.handle.net/1853/26631

6. Patterson, Frank H. Fuzzy framework for robust architecture identification in concept selection.

Degree: PhD, Aerospace Engineering, 2015, Georgia Tech

 An evolving set of modern physics-based, multi-disciplinary conceptual design methods seek to explore the feasibility of a new generation of systems, with new capabilities, capable… (more)

Subjects/Keywords: Systems engineering; Concept selection; Engineering design; Fuzzy; Decision making; Systems architecture; Knowledge based engineering

…Optimization Parameters (NSGA-II) 24 Identified Architecture Families… …Identified Alternatives 196 ix LIST OF FIGURES 1 Phases of Design [74]… …3 Robust Design Simulation [97] . . . . . . . . . . . . . . . . . . . . . . 4… …and Spaces in Axiomatic Design [114] . . . . . . . 18 10 Gaps in Current… …Mapping Historical First Order Design Parameters to Criteria (adapted from [31]… 

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APA (6th Edition):

Patterson, F. H. (2015). Fuzzy framework for robust architecture identification in concept selection. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/54413

Chicago Manual of Style (16th Edition):

Patterson, Frank H. “Fuzzy framework for robust architecture identification in concept selection.” 2015. Doctoral Dissertation, Georgia Tech. Accessed October 17, 2019. http://hdl.handle.net/1853/54413.

MLA Handbook (7th Edition):

Patterson, Frank H. “Fuzzy framework for robust architecture identification in concept selection.” 2015. Web. 17 Oct 2019.

Vancouver:

Patterson FH. Fuzzy framework for robust architecture identification in concept selection. [Internet] [Doctoral dissertation]. Georgia Tech; 2015. [cited 2019 Oct 17]. Available from: http://hdl.handle.net/1853/54413.

Council of Science Editors:

Patterson FH. Fuzzy framework for robust architecture identification in concept selection. [Doctoral Dissertation]. Georgia Tech; 2015. Available from: http://hdl.handle.net/1853/54413


Georgia Tech

7. Edwards, Stephen James. A methodology for risk-informed launch vehicle architecture selection.

Degree: PhD, Aerospace Engineering, 2017, Georgia Tech

 Modern society in the 21st century has become inseparably dependent on human mastery of the near-Earth regions of space. Billions of dollars in on-orbit assets… (more)

Subjects/Keywords: Launch vehicle design; Probabilistic design

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APA (6th Edition):

Edwards, S. J. (2017). A methodology for risk-informed launch vehicle architecture selection. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/60706

Chicago Manual of Style (16th Edition):

Edwards, Stephen James. “A methodology for risk-informed launch vehicle architecture selection.” 2017. Doctoral Dissertation, Georgia Tech. Accessed October 17, 2019. http://hdl.handle.net/1853/60706.

MLA Handbook (7th Edition):

Edwards, Stephen James. “A methodology for risk-informed launch vehicle architecture selection.” 2017. Web. 17 Oct 2019.

Vancouver:

Edwards SJ. A methodology for risk-informed launch vehicle architecture selection. [Internet] [Doctoral dissertation]. Georgia Tech; 2017. [cited 2019 Oct 17]. Available from: http://hdl.handle.net/1853/60706.

Council of Science Editors:

Edwards SJ. A methodology for risk-informed launch vehicle architecture selection. [Doctoral Dissertation]. Georgia Tech; 2017. Available from: http://hdl.handle.net/1853/60706

8. Armstrong, Michael James. Identification of emergent off-nominal operational requirements during conceptual architecting of the more electric aircraft.

Degree: PhD, Aerospace Engineering, 2011, Georgia Tech

 With the current increased emphasis on the development of energy optimized vehicle systems architectures during the early phases in aircraft conceptual design, accurate predictions of… (more)

Subjects/Keywords: Systems architecture; Systems engineering; Aircraft Systems Design; More electric aircraft; Reliability; Load shedding; Fault tolerance; Off-design; Reliability (Engineering); Fault tolerance (Engineering)

…Emergent Operational Requirements During Architecture Design, SONOMA… …Emergent Operational Requirements During Architecture Design, SONOMA… …accurate definition of load shedding strategies during architecture exploratory design. Formally… …architecture design and lead to inaccurate vehicle systems architecture. estimation of unit level… …intractability of the aircraft systems architecture design space, it can be safely classified as a… 

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APA (6th Edition):

Armstrong, M. J. (2011). Identification of emergent off-nominal operational requirements during conceptual architecting of the more electric aircraft. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/42872

Chicago Manual of Style (16th Edition):

Armstrong, Michael James. “Identification of emergent off-nominal operational requirements during conceptual architecting of the more electric aircraft.” 2011. Doctoral Dissertation, Georgia Tech. Accessed October 17, 2019. http://hdl.handle.net/1853/42872.

MLA Handbook (7th Edition):

Armstrong, Michael James. “Identification of emergent off-nominal operational requirements during conceptual architecting of the more electric aircraft.” 2011. Web. 17 Oct 2019.

Vancouver:

Armstrong MJ. Identification of emergent off-nominal operational requirements during conceptual architecting of the more electric aircraft. [Internet] [Doctoral dissertation]. Georgia Tech; 2011. [cited 2019 Oct 17]. Available from: http://hdl.handle.net/1853/42872.

Council of Science Editors:

Armstrong MJ. Identification of emergent off-nominal operational requirements during conceptual architecting of the more electric aircraft. [Doctoral Dissertation]. Georgia Tech; 2011. Available from: http://hdl.handle.net/1853/42872

9. Cinar, Gokcin. A methodology for dynamic sizing of electric power generation and distribution architectures.

Degree: PhD, Aerospace Engineering, 2018, Georgia Tech

 Electric and hybrid electric aircraft pose a significant architecture challenge, as these concepts not only deal with considerably high electrical loads, but also are extremely… (more)

Subjects/Keywords: Aircraft design; Electric propulsion; Hybrid propulsion; Electric aircraft; Hybrid aircraft; Subsystem design; Subsystem architecture; Transient analysis; Sizing and synthesis; Power management optimization

…bringing the subsystem and architecture considerations into the aircraft conceptual design stage… …design, propulsion system, architecture and the energy storage type? • What capabilities are… …Literature Review on the EA/HEA Conceptual Design and Feasibility Studies 10 2.3.1 NASA SCEPTOR… …18 A Look From the Architecture Perspective . . . . . . . . . . . . . . . . . . 19 2.4.1… …Objective Function . . . . . . . . . . . . . . . . . . . 79 4.2.2 Design and Control Variables… 

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APA (6th Edition):

Cinar, G. (2018). A methodology for dynamic sizing of electric power generation and distribution architectures. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/60754

Chicago Manual of Style (16th Edition):

Cinar, Gokcin. “A methodology for dynamic sizing of electric power generation and distribution architectures.” 2018. Doctoral Dissertation, Georgia Tech. Accessed October 17, 2019. http://hdl.handle.net/1853/60754.

MLA Handbook (7th Edition):

Cinar, Gokcin. “A methodology for dynamic sizing of electric power generation and distribution architectures.” 2018. Web. 17 Oct 2019.

Vancouver:

Cinar G. A methodology for dynamic sizing of electric power generation and distribution architectures. [Internet] [Doctoral dissertation]. Georgia Tech; 2018. [cited 2019 Oct 17]. Available from: http://hdl.handle.net/1853/60754.

Council of Science Editors:

Cinar G. A methodology for dynamic sizing of electric power generation and distribution architectures. [Doctoral Dissertation]. Georgia Tech; 2018. Available from: http://hdl.handle.net/1853/60754


Georgia Tech

10. Trent, Douglas James. Integrated architecture analysis and technology evaluation for systems of systems modeled at the subsystem level.

Degree: PhD, Aerospace Engineering, 2017, Georgia Tech

 A lack of knowledge during conceptual design results in two primary challenges: overruns in cost and schedule due to frequent design changes and combinatorial explosion… (more)

Subjects/Keywords: Systems of systems; Architecture; Technology; Space transportation; Space architecture

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APA (6th Edition):

Trent, D. J. (2017). Integrated architecture analysis and technology evaluation for systems of systems modeled at the subsystem level. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/59264

Chicago Manual of Style (16th Edition):

Trent, Douglas James. “Integrated architecture analysis and technology evaluation for systems of systems modeled at the subsystem level.” 2017. Doctoral Dissertation, Georgia Tech. Accessed October 17, 2019. http://hdl.handle.net/1853/59264.

MLA Handbook (7th Edition):

Trent, Douglas James. “Integrated architecture analysis and technology evaluation for systems of systems modeled at the subsystem level.” 2017. Web. 17 Oct 2019.

Vancouver:

Trent DJ. Integrated architecture analysis and technology evaluation for systems of systems modeled at the subsystem level. [Internet] [Doctoral dissertation]. Georgia Tech; 2017. [cited 2019 Oct 17]. Available from: http://hdl.handle.net/1853/59264.

Council of Science Editors:

Trent DJ. Integrated architecture analysis and technology evaluation for systems of systems modeled at the subsystem level. [Doctoral Dissertation]. Georgia Tech; 2017. Available from: http://hdl.handle.net/1853/59264


Arizona State University

11. Anderson, Benjamin Kyle. Conceptual Fuselage Design with Direct CAD Modeling.

Degree: Aerospace Engineering, 2017, Arizona State University

 In today’s day and age, the use of automated technology is becoming increasingly prevalent. Throughout the aerospace industry, we see the use of automated systems… (more)

Subjects/Keywords: Aerospace engineering; Design

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APA (6th Edition):

Anderson, B. K. (2017). Conceptual Fuselage Design with Direct CAD Modeling. (Masters Thesis). Arizona State University. Retrieved from http://repository.asu.edu/items/44011

Chicago Manual of Style (16th Edition):

Anderson, Benjamin Kyle. “Conceptual Fuselage Design with Direct CAD Modeling.” 2017. Masters Thesis, Arizona State University. Accessed October 17, 2019. http://repository.asu.edu/items/44011.

MLA Handbook (7th Edition):

Anderson, Benjamin Kyle. “Conceptual Fuselage Design with Direct CAD Modeling.” 2017. Web. 17 Oct 2019.

Vancouver:

Anderson BK. Conceptual Fuselage Design with Direct CAD Modeling. [Internet] [Masters thesis]. Arizona State University; 2017. [cited 2019 Oct 17]. Available from: http://repository.asu.edu/items/44011.

Council of Science Editors:

Anderson BK. Conceptual Fuselage Design with Direct CAD Modeling. [Masters Thesis]. Arizona State University; 2017. Available from: http://repository.asu.edu/items/44011


Georgia Tech

12. Hart, Peter Bartholomew. A plm implementation for aerospace systems engineering-conceptual rotorcraft design.

Degree: MS, Aerospace Engineering, 2009, Georgia Tech

 The thesis will discuss the Systems Engineering phase of an original Conceptual Design Engineering Methodology for Aerospace Engineering-Vehicle Synthesis. This iterative phase is shown to… (more)

Subjects/Keywords: Teamcenter systems engineering; Teamcenter community; Teamcenter unified; Teamcenter engineering; Teamcenter manufacturing; CATIA V5; Rotorcraft design; Boeing; AHS; Joint heavy lift; VPLM; MBOM; EBOM; Product change control; Product definition; Configuration management; Product structure architecture; Design engineering; Aerospace engineering; System engineering; PLM; CIE; IDE; SE; Affordability; Cost savings; Executive helicopter; Joint chiefs of staff; Marine; CAE; CAD; CAM; CAA; MDO; RSM; DOE; Consulting; Engineering management; Perfect storm; Engineering software; Requirements data management; CATIA V4; NX; Engineering communications; RFP; Digitization; Air Force; Navy; Army; BAMS; FIPER; ACSYNT; Sikorsky; Bell; Georgia Tech; Engineering methodology; Requirements engineering; System engineering; Business process re-engineering conceptual design; Search; Rescue; IDE; Integrated digital environment; Kingfisher; Search and rescue; Helicopter; Helicopter engineering; QFD; Legacy design; IPPD; Quality engineering; Defense systems acquisition; Coast Guard; Decision support systems; Rotors (Helicopters) Design; Concurrent engineering

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APA (6th Edition):

Hart, P. B. (2009). A plm implementation for aerospace systems engineering-conceptual rotorcraft design. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/28278

Chicago Manual of Style (16th Edition):

Hart, Peter Bartholomew. “A plm implementation for aerospace systems engineering-conceptual rotorcraft design.” 2009. Masters Thesis, Georgia Tech. Accessed October 17, 2019. http://hdl.handle.net/1853/28278.

MLA Handbook (7th Edition):

Hart, Peter Bartholomew. “A plm implementation for aerospace systems engineering-conceptual rotorcraft design.” 2009. Web. 17 Oct 2019.

Vancouver:

Hart PB. A plm implementation for aerospace systems engineering-conceptual rotorcraft design. [Internet] [Masters thesis]. Georgia Tech; 2009. [cited 2019 Oct 17]. Available from: http://hdl.handle.net/1853/28278.

Council of Science Editors:

Hart PB. A plm implementation for aerospace systems engineering-conceptual rotorcraft design. [Masters Thesis]. Georgia Tech; 2009. Available from: http://hdl.handle.net/1853/28278


Georgia Tech

13. Scott, Robert C. A new rotorcraft design framework based on reliability and cost.

Degree: PhD, Aerospace Engineering, 2016, Georgia Tech

 Helicopters provide essential services in civil and military applications due to their multirole capability and operational flexibility, but the combination of the disparate performance conditions… (more)

Subjects/Keywords: Rotorcraft design; Aircraft design; Rotorcraft assessment; Conceptual design and assessment; Life-cycle cost; Reliability; Maintainability

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APA (6th Edition):

Scott, R. C. (2016). A new rotorcraft design framework based on reliability and cost. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/55640

Chicago Manual of Style (16th Edition):

Scott, Robert C. “A new rotorcraft design framework based on reliability and cost.” 2016. Doctoral Dissertation, Georgia Tech. Accessed October 17, 2019. http://hdl.handle.net/1853/55640.

MLA Handbook (7th Edition):

Scott, Robert C. “A new rotorcraft design framework based on reliability and cost.” 2016. Web. 17 Oct 2019.

Vancouver:

Scott RC. A new rotorcraft design framework based on reliability and cost. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2019 Oct 17]. Available from: http://hdl.handle.net/1853/55640.

Council of Science Editors:

Scott RC. A new rotorcraft design framework based on reliability and cost. [Doctoral Dissertation]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/55640


Virginia Tech

14. Allison, Darcy L. Multidisciplinary Analysis and Design Optimization of an Efficient Supersonic Air Vehicle.

Degree: PhD, Aerospace Engineering, 2013, Virginia Tech

 This work seeks to develop multidisciplinary design optimization (MDO) methods to find the optimal design of a particular aircraft called an Efficient Supersonic Air Vehicle… (more)

Subjects/Keywords: aircraft design; multidisciplinary design optimization; supersonic military aircraft; design of computer experiments

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APA (6th Edition):

Allison, D. L. (2013). Multidisciplinary Analysis and Design Optimization of an Efficient Supersonic Air Vehicle. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/24187

Chicago Manual of Style (16th Edition):

Allison, Darcy L. “Multidisciplinary Analysis and Design Optimization of an Efficient Supersonic Air Vehicle.” 2013. Doctoral Dissertation, Virginia Tech. Accessed October 17, 2019. http://hdl.handle.net/10919/24187.

MLA Handbook (7th Edition):

Allison, Darcy L. “Multidisciplinary Analysis and Design Optimization of an Efficient Supersonic Air Vehicle.” 2013. Web. 17 Oct 2019.

Vancouver:

Allison DL. Multidisciplinary Analysis and Design Optimization of an Efficient Supersonic Air Vehicle. [Internet] [Doctoral dissertation]. Virginia Tech; 2013. [cited 2019 Oct 17]. Available from: http://hdl.handle.net/10919/24187.

Council of Science Editors:

Allison DL. Multidisciplinary Analysis and Design Optimization of an Efficient Supersonic Air Vehicle. [Doctoral Dissertation]. Virginia Tech; 2013. Available from: http://hdl.handle.net/10919/24187


Georgia Tech

15. Patterson, Michael Dobson. Conceptual Design of High-Lift Propeller Systems for Small Electric Aircraft.

Degree: PhD, Aerospace Engineering, 2016, Georgia Tech

 The maturation of electric propulsion technologies presents intriguing new degrees of freedom for aircraft designers including the ability to distribute many small propellers upstream of… (more)

Subjects/Keywords: distributed electric propulsion; high-lift propellers; aircraft design; aircraft performance; design method; propeller design

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APA (6th Edition):

Patterson, M. D. (2016). Conceptual Design of High-Lift Propeller Systems for Small Electric Aircraft. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/55569

Chicago Manual of Style (16th Edition):

Patterson, Michael Dobson. “Conceptual Design of High-Lift Propeller Systems for Small Electric Aircraft.” 2016. Doctoral Dissertation, Georgia Tech. Accessed October 17, 2019. http://hdl.handle.net/1853/55569.

MLA Handbook (7th Edition):

Patterson, Michael Dobson. “Conceptual Design of High-Lift Propeller Systems for Small Electric Aircraft.” 2016. Web. 17 Oct 2019.

Vancouver:

Patterson MD. Conceptual Design of High-Lift Propeller Systems for Small Electric Aircraft. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2019 Oct 17]. Available from: http://hdl.handle.net/1853/55569.

Council of Science Editors:

Patterson MD. Conceptual Design of High-Lift Propeller Systems for Small Electric Aircraft. [Doctoral Dissertation]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/55569


Georgia Tech

16. Kizer, Justin Raymond. Aircraft conceptual design enabled by a set-based approach for the exploration and bounding of non-hypercubic design spaces.

Degree: PhD, Aerospace Engineering, 2016, Georgia Tech

 With the increasing reliance upon advanced computational methods for engineering analyses, there is a need for the efficient exploration of experimental design spaces. Contemporary methods… (more)

Subjects/Keywords: Design space exploration; Aircraft design; Conceptual design; Adaptive sampling; Non-hypercubic; Set-based design; Mutual information; Machine learning

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APA (6th Edition):

Kizer, J. R. (2016). Aircraft conceptual design enabled by a set-based approach for the exploration and bounding of non-hypercubic design spaces. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/55622

Chicago Manual of Style (16th Edition):

Kizer, Justin Raymond. “Aircraft conceptual design enabled by a set-based approach for the exploration and bounding of non-hypercubic design spaces.” 2016. Doctoral Dissertation, Georgia Tech. Accessed October 17, 2019. http://hdl.handle.net/1853/55622.

MLA Handbook (7th Edition):

Kizer, Justin Raymond. “Aircraft conceptual design enabled by a set-based approach for the exploration and bounding of non-hypercubic design spaces.” 2016. Web. 17 Oct 2019.

Vancouver:

Kizer JR. Aircraft conceptual design enabled by a set-based approach for the exploration and bounding of non-hypercubic design spaces. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2019 Oct 17]. Available from: http://hdl.handle.net/1853/55622.

Council of Science Editors:

Kizer JR. Aircraft conceptual design enabled by a set-based approach for the exploration and bounding of non-hypercubic design spaces. [Doctoral Dissertation]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/55622


Georgia Tech

17. Tetik, Halil Sahin. A framework for value-driven aircraft family design for dynamic market systems under uncertainty and strategic competition.

Degree: PhD, Aerospace Engineering, 2016, Georgia Tech

 Aircraft family design and production is a complicated process that includes numerous decisions across various disciplines, where these decisions should be made in a coordinated… (more)

Subjects/Keywords: Product family design; Aircraft design; Value-driven design; Competition; Industrial organization; Microeconomics; Market entry; Derivative design

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APA (6th Edition):

Tetik, H. S. (2016). A framework for value-driven aircraft family design for dynamic market systems under uncertainty and strategic competition. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/56352

Chicago Manual of Style (16th Edition):

Tetik, Halil Sahin. “A framework for value-driven aircraft family design for dynamic market systems under uncertainty and strategic competition.” 2016. Doctoral Dissertation, Georgia Tech. Accessed October 17, 2019. http://hdl.handle.net/1853/56352.

MLA Handbook (7th Edition):

Tetik, Halil Sahin. “A framework for value-driven aircraft family design for dynamic market systems under uncertainty and strategic competition.” 2016. Web. 17 Oct 2019.

Vancouver:

Tetik HS. A framework for value-driven aircraft family design for dynamic market systems under uncertainty and strategic competition. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2019 Oct 17]. Available from: http://hdl.handle.net/1853/56352.

Council of Science Editors:

Tetik HS. A framework for value-driven aircraft family design for dynamic market systems under uncertainty and strategic competition. [Doctoral Dissertation]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/56352


Georgia Tech

18. Corman, Jason A. A methodology for structural technology performance characterization to enable reduction of structural uncertainty.

Degree: PhD, Aerospace Engineering, 2017, Georgia Tech

 Government programs have been established to identify solutions that will significantly reduce the impact of aviation on the environment in the upcoming generations. Airframe structural… (more)

Subjects/Keywords: Aircraft design; Airframe structural technology

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APA (6th Edition):

Corman, J. A. (2017). A methodology for structural technology performance characterization to enable reduction of structural uncertainty. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/59795

Chicago Manual of Style (16th Edition):

Corman, Jason A. “A methodology for structural technology performance characterization to enable reduction of structural uncertainty.” 2017. Doctoral Dissertation, Georgia Tech. Accessed October 17, 2019. http://hdl.handle.net/1853/59795.

MLA Handbook (7th Edition):

Corman, Jason A. “A methodology for structural technology performance characterization to enable reduction of structural uncertainty.” 2017. Web. 17 Oct 2019.

Vancouver:

Corman JA. A methodology for structural technology performance characterization to enable reduction of structural uncertainty. [Internet] [Doctoral dissertation]. Georgia Tech; 2017. [cited 2019 Oct 17]. Available from: http://hdl.handle.net/1853/59795.

Council of Science Editors:

Corman JA. A methodology for structural technology performance characterization to enable reduction of structural uncertainty. [Doctoral Dissertation]. Georgia Tech; 2017. Available from: http://hdl.handle.net/1853/59795


Georgia Tech

19. Fleming Lindsley, Elizabeth. Design knowledge coordination: Enhancing novice aerospace engineers' design skills through coordinated decision-making.

Degree: PhD, Aerospace Engineering, 2016, Georgia Tech

 This research contributes to both the aerospace engineering design community and the aerospace engineering education community by defining key indicators of design knowledge coordination as… (more)

Subjects/Keywords: Aerospace engineering design; Engineering education; Case study research; Design knowledge coordination

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APA (6th Edition):

Fleming Lindsley, E. (2016). Design knowledge coordination: Enhancing novice aerospace engineers' design skills through coordinated decision-making. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/55614

Chicago Manual of Style (16th Edition):

Fleming Lindsley, Elizabeth. “Design knowledge coordination: Enhancing novice aerospace engineers' design skills through coordinated decision-making.” 2016. Doctoral Dissertation, Georgia Tech. Accessed October 17, 2019. http://hdl.handle.net/1853/55614.

MLA Handbook (7th Edition):

Fleming Lindsley, Elizabeth. “Design knowledge coordination: Enhancing novice aerospace engineers' design skills through coordinated decision-making.” 2016. Web. 17 Oct 2019.

Vancouver:

Fleming Lindsley E. Design knowledge coordination: Enhancing novice aerospace engineers' design skills through coordinated decision-making. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2019 Oct 17]. Available from: http://hdl.handle.net/1853/55614.

Council of Science Editors:

Fleming Lindsley E. Design knowledge coordination: Enhancing novice aerospace engineers' design skills through coordinated decision-making. [Doctoral Dissertation]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/55614


Cal Poly

20. Daniel, Jason Lloyd. Whitespace Exploration.

Degree: MS, Aerospace Engineering, 2017, Cal Poly

  As engineering systems grow in complexity so too must the design tools that we use evolve and allow for decision makers to efficiently ask… (more)

Subjects/Keywords: optimization; design; Computational Engineering; Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Daniel, J. L. (2017). Whitespace Exploration. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1791

Chicago Manual of Style (16th Edition):

Daniel, Jason Lloyd. “Whitespace Exploration.” 2017. Masters Thesis, Cal Poly. Accessed October 17, 2019. https://digitalcommons.calpoly.edu/theses/1791.

MLA Handbook (7th Edition):

Daniel, Jason Lloyd. “Whitespace Exploration.” 2017. Web. 17 Oct 2019.

Vancouver:

Daniel JL. Whitespace Exploration. [Internet] [Masters thesis]. Cal Poly; 2017. [cited 2019 Oct 17]. Available from: https://digitalcommons.calpoly.edu/theses/1791.

Council of Science Editors:

Daniel JL. Whitespace Exploration. [Masters Thesis]. Cal Poly; 2017. Available from: https://digitalcommons.calpoly.edu/theses/1791


Arizona State University

21. Verbin, Andrew Joseph. Detailed Design of a Pulsed Plasma Thrust Stand.

Degree: Aerospace Engineering, 2017, Arizona State University

 This thesis gives a detailed design process for a pulsed type thruster. The thrust stand designed in this paper is for a Pulsed Plasma Thruster… (more)

Subjects/Keywords: Aerospace engineering; Design; Engineering; Design; Plasma; Pulsed; Thrust; Thruster

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APA (6th Edition):

Verbin, A. J. (2017). Detailed Design of a Pulsed Plasma Thrust Stand. (Masters Thesis). Arizona State University. Retrieved from http://repository.asu.edu/items/44012

Chicago Manual of Style (16th Edition):

Verbin, Andrew Joseph. “Detailed Design of a Pulsed Plasma Thrust Stand.” 2017. Masters Thesis, Arizona State University. Accessed October 17, 2019. http://repository.asu.edu/items/44012.

MLA Handbook (7th Edition):

Verbin, Andrew Joseph. “Detailed Design of a Pulsed Plasma Thrust Stand.” 2017. Web. 17 Oct 2019.

Vancouver:

Verbin AJ. Detailed Design of a Pulsed Plasma Thrust Stand. [Internet] [Masters thesis]. Arizona State University; 2017. [cited 2019 Oct 17]. Available from: http://repository.asu.edu/items/44012.

Council of Science Editors:

Verbin AJ. Detailed Design of a Pulsed Plasma Thrust Stand. [Masters Thesis]. Arizona State University; 2017. Available from: http://repository.asu.edu/items/44012


Georgia Tech

22. Mines, John Mark. A bi-Level framework for aircraft design uncertainty quantification and management.

Degree: PhD, Aerospace Engineering, 2019, Georgia Tech

 Aircraft design and development is a high-risk process. The recent obstacles with the Boeing 787 Dreamliner and Lockheed Martin F-35 show that the level of… (more)

Subjects/Keywords: Aircraft design; Uncertainty quantification; Optimization; Risk assessment; Reliability-based design optimization; Finite element modeling; Aircraft wing design; Uncertainty propagation; Conceptual design selection; Design decision-making

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APA (6th Edition):

Mines, J. M. (2019). A bi-Level framework for aircraft design uncertainty quantification and management. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/61281

Chicago Manual of Style (16th Edition):

Mines, John Mark. “A bi-Level framework for aircraft design uncertainty quantification and management.” 2019. Doctoral Dissertation, Georgia Tech. Accessed October 17, 2019. http://hdl.handle.net/1853/61281.

MLA Handbook (7th Edition):

Mines, John Mark. “A bi-Level framework for aircraft design uncertainty quantification and management.” 2019. Web. 17 Oct 2019.

Vancouver:

Mines JM. A bi-Level framework for aircraft design uncertainty quantification and management. [Internet] [Doctoral dissertation]. Georgia Tech; 2019. [cited 2019 Oct 17]. Available from: http://hdl.handle.net/1853/61281.

Council of Science Editors:

Mines JM. A bi-Level framework for aircraft design uncertainty quantification and management. [Doctoral Dissertation]. Georgia Tech; 2019. Available from: http://hdl.handle.net/1853/61281


Georgia Tech

23. Coso, Alexandra Emelina. Preparing students to incorporate stakeholder requirements in aerospace vehicle design.

Degree: PhD, Aerospace Engineering, 2014, Georgia Tech

 The design of an aerospace vehicle system is a complex integration process driven by technological developments, stakeholder and mission needs, cost, and schedule. The vehicle… (more)

Subjects/Keywords: Aerospace vehicle design; Engineering design education; Stakeholder considerations; Space vehicles; Design; Group decision making; Multiple criteria decision making

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APA (6th Edition):

Coso, A. E. (2014). Preparing students to incorporate stakeholder requirements in aerospace vehicle design. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/51885

Chicago Manual of Style (16th Edition):

Coso, Alexandra Emelina. “Preparing students to incorporate stakeholder requirements in aerospace vehicle design.” 2014. Doctoral Dissertation, Georgia Tech. Accessed October 17, 2019. http://hdl.handle.net/1853/51885.

MLA Handbook (7th Edition):

Coso, Alexandra Emelina. “Preparing students to incorporate stakeholder requirements in aerospace vehicle design.” 2014. Web. 17 Oct 2019.

Vancouver:

Coso AE. Preparing students to incorporate stakeholder requirements in aerospace vehicle design. [Internet] [Doctoral dissertation]. Georgia Tech; 2014. [cited 2019 Oct 17]. Available from: http://hdl.handle.net/1853/51885.

Council of Science Editors:

Coso AE. Preparing students to incorporate stakeholder requirements in aerospace vehicle design. [Doctoral Dissertation]. Georgia Tech; 2014. Available from: http://hdl.handle.net/1853/51885


Georgia Tech

24. Ghosh, Sayan. Concurrent optimization using probabilistic analysis of distributed multidisciplinary architectures for design under uncertainty.

Degree: PhD, Aerospace Engineering, 2016, Georgia Tech

 Uncertainty based Multidisciplinary Optimization (UMDO) relies on propagation of uncertainties across several disciplines. A typical aircraft design process involves collaboration of multiple and diverse teams… (more)

Subjects/Keywords: Uncertainty quantification; Multidisciplinary design optimization; MDO; Design optimization; Quantile regression; Copula; Statistical dependence; Design under uncertainty; Concurrent optimization

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APA (6th Edition):

Ghosh, S. (2016). Concurrent optimization using probabilistic analysis of distributed multidisciplinary architectures for design under uncertainty. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/56302

Chicago Manual of Style (16th Edition):

Ghosh, Sayan. “Concurrent optimization using probabilistic analysis of distributed multidisciplinary architectures for design under uncertainty.” 2016. Doctoral Dissertation, Georgia Tech. Accessed October 17, 2019. http://hdl.handle.net/1853/56302.

MLA Handbook (7th Edition):

Ghosh, Sayan. “Concurrent optimization using probabilistic analysis of distributed multidisciplinary architectures for design under uncertainty.” 2016. Web. 17 Oct 2019.

Vancouver:

Ghosh S. Concurrent optimization using probabilistic analysis of distributed multidisciplinary architectures for design under uncertainty. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2019 Oct 17]. Available from: http://hdl.handle.net/1853/56302.

Council of Science Editors:

Ghosh S. Concurrent optimization using probabilistic analysis of distributed multidisciplinary architectures for design under uncertainty. [Doctoral Dissertation]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/56302


University of Illinois – Urbana-Champaign

25. Conlan-Smith, Cian James. Design of functionally graded compliant mechanisms using topology optimization.

Degree: MS, Aerospace Engineering, 2017, University of Illinois – Urbana-Champaign

 This research applies topology optimization to create feasible functionally graded complaint mechanism designs with the aim of improving structural performance compared to traditional homogeneous compliant… (more)

Subjects/Keywords: Topology optimization; Bio-inspired design; Compliant mechanism design; Functionally graded materials; Geometric non-linearity; Stress constrained design

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APA (6th Edition):

Conlan-Smith, C. J. (2017). Design of functionally graded compliant mechanisms using topology optimization. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/97500

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):

Conlan-Smith, Cian James. “Design of functionally graded compliant mechanisms using topology optimization.” 2017. Thesis, University of Illinois – Urbana-Champaign. Accessed October 17, 2019. http://hdl.handle.net/2142/97500.

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

MLA Handbook (7th Edition):

Conlan-Smith, Cian James. “Design of functionally graded compliant mechanisms using topology optimization.” 2017. Web. 17 Oct 2019.

Vancouver:

Conlan-Smith CJ. Design of functionally graded compliant mechanisms using topology optimization. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2017. [cited 2019 Oct 17]. Available from: http://hdl.handle.net/2142/97500.

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

Council of Science Editors:

Conlan-Smith CJ. Design of functionally graded compliant mechanisms using topology optimization. [Thesis]. University of Illinois – Urbana-Champaign; 2017. Available from: http://hdl.handle.net/2142/97500

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


University of Kansas

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

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

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Schueler, Samantha Katelyn. “A Study in Aircraft Efficiency Enhancements via Prandtl-Tailored Dynamically Aerocompliant Wingtip Extensions.” 2014. Masters Thesis, University of Kansas. Accessed October 17, 2019. http://hdl.handle.net/1808/19593.

MLA Handbook (7th Edition):

Schueler, Samantha Katelyn. “A Study in Aircraft Efficiency Enhancements via Prandtl-Tailored Dynamically Aerocompliant Wingtip Extensions.” 2014. Web. 17 Oct 2019.

Vancouver:

Schueler SK. A Study in Aircraft Efficiency Enhancements via Prandtl-Tailored Dynamically Aerocompliant Wingtip Extensions. [Internet] [Masters thesis]. University of Kansas; 2014. [cited 2019 Oct 17]. Available from: http://hdl.handle.net/1808/19593.

Council of Science Editors:

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


Georgia Tech

27. Miller, Michael Z. A decision support framework for aircraft conceptual design in the presence of competition.

Degree: PhD, Aerospace Engineering, 2016, Georgia Tech

 Most conceptual design techniques for aircraft implicitly assume that the aircraft manufacturer operates in a monopoly. This is because these techniques do not directly account… (more)

Subjects/Keywords: Aircraft; Conceptual design; Uncertainty; Competition; Probabilistic

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APA (6th Edition):

Miller, M. Z. (2016). A decision support framework for aircraft conceptual design in the presence of competition. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/55585

Chicago Manual of Style (16th Edition):

Miller, Michael Z. “A decision support framework for aircraft conceptual design in the presence of competition.” 2016. Doctoral Dissertation, Georgia Tech. Accessed October 17, 2019. http://hdl.handle.net/1853/55585.

MLA Handbook (7th Edition):

Miller, Michael Z. “A decision support framework for aircraft conceptual design in the presence of competition.” 2016. Web. 17 Oct 2019.

Vancouver:

Miller MZ. A decision support framework for aircraft conceptual design in the presence of competition. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2019 Oct 17]. Available from: http://hdl.handle.net/1853/55585.

Council of Science Editors:

Miller MZ. A decision support framework for aircraft conceptual design in the presence of competition. [Doctoral Dissertation]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/55585


Georgia Tech

28. Noevere, August T. Rapid determination of mass and stiffness distribution on primary skin-stiffener structures.

Degree: PhD, Aerospace Engineering, 2016, Georgia Tech

 In modern conceptual/preliminary design of aerospace vehicles it is common for a large number of concepts and configurations to be rapidly explored. For each configuration,… (more)

Subjects/Keywords: Structural optimization; Stiffened panel optimization; Conceptual design

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APA (6th Edition):

Noevere, A. T. (2016). Rapid determination of mass and stiffness distribution on primary skin-stiffener structures. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/55638

Chicago Manual of Style (16th Edition):

Noevere, August T. “Rapid determination of mass and stiffness distribution on primary skin-stiffener structures.” 2016. Doctoral Dissertation, Georgia Tech. Accessed October 17, 2019. http://hdl.handle.net/1853/55638.

MLA Handbook (7th Edition):

Noevere, August T. “Rapid determination of mass and stiffness distribution on primary skin-stiffener structures.” 2016. Web. 17 Oct 2019.

Vancouver:

Noevere AT. Rapid determination of mass and stiffness distribution on primary skin-stiffener structures. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2019 Oct 17]. Available from: http://hdl.handle.net/1853/55638.

Council of Science Editors:

Noevere AT. Rapid determination of mass and stiffness distribution on primary skin-stiffener structures. [Doctoral Dissertation]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/55638

29. Simon, Matthew. Evaluation and automation of space habitat interior layouts.

Degree: PhD, Aerospace Engineering, 2016, Georgia Tech

 Future human exploration missions beyond Earth vicinity will be demanding, requiring highly efficient, mass-constrained systems to reduce overall mission costs and complexity. Additionally, long duration… (more)

Subjects/Keywords: Habitat design; Interior layout; Evaluation; Habitability; Habitation; Conceptual design; Space vehicle; Space; Exploration

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APA (6th Edition):

Simon, M. (2016). Evaluation and automation of space habitat interior layouts. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/54938

Chicago Manual of Style (16th Edition):

Simon, Matthew. “Evaluation and automation of space habitat interior layouts.” 2016. Doctoral Dissertation, Georgia Tech. Accessed October 17, 2019. http://hdl.handle.net/1853/54938.

MLA Handbook (7th Edition):

Simon, Matthew. “Evaluation and automation of space habitat interior layouts.” 2016. Web. 17 Oct 2019.

Vancouver:

Simon M. Evaluation and automation of space habitat interior layouts. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2019 Oct 17]. Available from: http://hdl.handle.net/1853/54938.

Council of Science Editors:

Simon M. Evaluation and automation of space habitat interior layouts. [Doctoral Dissertation]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/54938


Georgia Tech

30. Borer, Nicholas Keith. Decision Making Strategies for Probabilistic Aerospace Systems Design.

Degree: PhD, Aerospace Engineering, 2006, Georgia Tech

 Modern aerospace systems design problems are often characterized by the necessity to identify and enable multiple tradeoffs. This can be accomplished by transformation of the… (more)

Subjects/Keywords: Decision making; Probabilistic design; Systems design

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APA (6th Edition):

Borer, N. K. (2006). Decision Making Strategies for Probabilistic Aerospace Systems Design. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/10469

Chicago Manual of Style (16th Edition):

Borer, Nicholas Keith. “Decision Making Strategies for Probabilistic Aerospace Systems Design.” 2006. Doctoral Dissertation, Georgia Tech. Accessed October 17, 2019. http://hdl.handle.net/1853/10469.

MLA Handbook (7th Edition):

Borer, Nicholas Keith. “Decision Making Strategies for Probabilistic Aerospace Systems Design.” 2006. Web. 17 Oct 2019.

Vancouver:

Borer NK. Decision Making Strategies for Probabilistic Aerospace Systems Design. [Internet] [Doctoral dissertation]. Georgia Tech; 2006. [cited 2019 Oct 17]. Available from: http://hdl.handle.net/1853/10469.

Council of Science Editors:

Borer NK. Decision Making Strategies for Probabilistic Aerospace Systems Design. [Doctoral Dissertation]. Georgia Tech; 2006. Available from: http://hdl.handle.net/1853/10469

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