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You searched for +publisher:"Georgia Tech" +contributor:("Wilhite, Alan"). Showing records 1 – 22 of 22 total matches.

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Georgia Tech

1. Kutty, Prasad M. Reconstruction and uncertainty quantification of entry, descent and landing trajectories using vehicle aerodynamics.

Degree: MS, Aerospace Engineering, 2014, Georgia Tech

 The reconstruction of entry, descent and landing (EDL) trajectories is significantly affected by the knowledge of the atmospheric conditions during flight. Away from Earth, this… (more)

Subjects/Keywords: Trajectory reconstruction; Entry, descent and landing; Space vehicles; Space trajectories; Space vehicles Atmospheric entry; Algorithms

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APA (6th Edition):

Kutty, P. M. (2014). Reconstruction and uncertainty quantification of entry, descent and landing trajectories using vehicle aerodynamics. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/51893

Chicago Manual of Style (16th Edition):

Kutty, Prasad M. “Reconstruction and uncertainty quantification of entry, descent and landing trajectories using vehicle aerodynamics.” 2014. Masters Thesis, Georgia Tech. Accessed August 08, 2020. http://hdl.handle.net/1853/51893.

MLA Handbook (7th Edition):

Kutty, Prasad M. “Reconstruction and uncertainty quantification of entry, descent and landing trajectories using vehicle aerodynamics.” 2014. Web. 08 Aug 2020.

Vancouver:

Kutty PM. Reconstruction and uncertainty quantification of entry, descent and landing trajectories using vehicle aerodynamics. [Internet] [Masters thesis]. Georgia Tech; 2014. [cited 2020 Aug 08]. Available from: http://hdl.handle.net/1853/51893.

Council of Science Editors:

Kutty PM. Reconstruction and uncertainty quantification of entry, descent and landing trajectories using vehicle aerodynamics. [Masters Thesis]. Georgia Tech; 2014. Available from: http://hdl.handle.net/1853/51893

2. 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 August 08, 2020. http://hdl.handle.net/1853/54938.

MLA Handbook (7th Edition):

Simon, Matthew. “Evaluation and automation of space habitat interior layouts.” 2016. Web. 08 Aug 2020.

Vancouver:

Simon M. Evaluation and automation of space habitat interior layouts. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2020 Aug 08]. 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

3. Jones, Christopher A. Risk-value optimization of performance and cost for propellant production on Mars.

Degree: PhD, Aerospace Engineering, 2016, Georgia Tech

 The nominal two-and-a-half year round-trip Mars mission requires extensive infrastructure to transport and safeguard its human crew, thus requiring large amounts of Initial Mass in… (more)

Subjects/Keywords: Human Mars architectures; In-situ resource utilization

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APA (6th Edition):

Jones, C. A. (2016). Risk-value optimization of performance and cost for propellant production on Mars. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/55584

Chicago Manual of Style (16th Edition):

Jones, Christopher A. “Risk-value optimization of performance and cost for propellant production on Mars.” 2016. Doctoral Dissertation, Georgia Tech. Accessed August 08, 2020. http://hdl.handle.net/1853/55584.

MLA Handbook (7th Edition):

Jones, Christopher A. “Risk-value optimization of performance and cost for propellant production on Mars.” 2016. Web. 08 Aug 2020.

Vancouver:

Jones CA. Risk-value optimization of performance and cost for propellant production on Mars. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2020 Aug 08]. Available from: http://hdl.handle.net/1853/55584.

Council of Science Editors:

Jones CA. Risk-value optimization of performance and cost for propellant production on Mars. [Doctoral Dissertation]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/55584

4. 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 August 08, 2020. 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. 08 Aug 2020.

Vancouver:

Noevere AT. Rapid determination of mass and stiffness distribution on primary skin-stiffener structures. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2020 Aug 08]. 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

5. Rowell, Amy F. Calibrating the inertial coordinate system of the miniature inertial measurement unit on SAGE III ISS.

Degree: MS, Aerospace Engineering, 2016, Georgia Tech

 The Stratospheric Aerosol and Gas Experiment III (SAGE III) on the International Space Station (ISS) will extend NASA Langley Research Center's long legacy of satellite… (more)

Subjects/Keywords: Attitude determination; Coordinate system calibration; Disturbance monitoring package; SAGE III; Multiplicative extended Kalman filter; ISS attitude

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APA (6th Edition):

Rowell, A. F. (2016). Calibrating the inertial coordinate system of the miniature inertial measurement unit on SAGE III ISS. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/56370

Chicago Manual of Style (16th Edition):

Rowell, Amy F. “Calibrating the inertial coordinate system of the miniature inertial measurement unit on SAGE III ISS.” 2016. Masters Thesis, Georgia Tech. Accessed August 08, 2020. http://hdl.handle.net/1853/56370.

MLA Handbook (7th Edition):

Rowell, Amy F. “Calibrating the inertial coordinate system of the miniature inertial measurement unit on SAGE III ISS.” 2016. Web. 08 Aug 2020.

Vancouver:

Rowell AF. Calibrating the inertial coordinate system of the miniature inertial measurement unit on SAGE III ISS. [Internet] [Masters thesis]. Georgia Tech; 2016. [cited 2020 Aug 08]. Available from: http://hdl.handle.net/1853/56370.

Council of Science Editors:

Rowell AF. Calibrating the inertial coordinate system of the miniature inertial measurement unit on SAGE III ISS. [Masters Thesis]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/56370


Georgia Tech

6. Chai, Patrick R. Stochastic feasibility assessments of orbital propellant depot and commercial launch enabled space exploration architectures.

Degree: PhD, Aerospace Engineering, 2014, Georgia Tech

 The 2010 National Space Policy of the United State of America introduced by President Obama directed NASA to set far reaching exploration milestones that included… (more)

Subjects/Keywords: Exploration architecture; Propellant depots; Launch reliability; Cryogenic thermal management; Space mission analysis; System analysis; Bayesian launch reliability

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APA (6th Edition):

Chai, P. R. (2014). Stochastic feasibility assessments of orbital propellant depot and commercial launch enabled space exploration architectures. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/54291

Chicago Manual of Style (16th Edition):

Chai, Patrick R. “Stochastic feasibility assessments of orbital propellant depot and commercial launch enabled space exploration architectures.” 2014. Doctoral Dissertation, Georgia Tech. Accessed August 08, 2020. http://hdl.handle.net/1853/54291.

MLA Handbook (7th Edition):

Chai, Patrick R. “Stochastic feasibility assessments of orbital propellant depot and commercial launch enabled space exploration architectures.” 2014. Web. 08 Aug 2020.

Vancouver:

Chai PR. Stochastic feasibility assessments of orbital propellant depot and commercial launch enabled space exploration architectures. [Internet] [Doctoral dissertation]. Georgia Tech; 2014. [cited 2020 Aug 08]. Available from: http://hdl.handle.net/1853/54291.

Council of Science Editors:

Chai PR. Stochastic feasibility assessments of orbital propellant depot and commercial launch enabled space exploration architectures. [Doctoral Dissertation]. Georgia Tech; 2014. Available from: http://hdl.handle.net/1853/54291

7. Williams, Logan Todd. Ion acceleration mechanisms of helicon thrusters.

Degree: PhD, Aerospace Engineering, 2013, Georgia Tech

 A helicon plasma source is a device that can efficiently ionize a gas to create high density, low temperature plasma. There is growing interest in… (more)

Subjects/Keywords: Ion acceleration; Ion engine; Helicon; Ion accelerators; Particle accelerators; Propulsion systems; Helicons (Electromagnetism)

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APA (6th Edition):

Williams, L. T. (2013). Ion acceleration mechanisms of helicon thrusters. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/47691

Chicago Manual of Style (16th Edition):

Williams, Logan Todd. “Ion acceleration mechanisms of helicon thrusters.” 2013. Doctoral Dissertation, Georgia Tech. Accessed August 08, 2020. http://hdl.handle.net/1853/47691.

MLA Handbook (7th Edition):

Williams, Logan Todd. “Ion acceleration mechanisms of helicon thrusters.” 2013. Web. 08 Aug 2020.

Vancouver:

Williams LT. Ion acceleration mechanisms of helicon thrusters. [Internet] [Doctoral dissertation]. Georgia Tech; 2013. [cited 2020 Aug 08]. Available from: http://hdl.handle.net/1853/47691.

Council of Science Editors:

Williams LT. Ion acceleration mechanisms of helicon thrusters. [Doctoral Dissertation]. Georgia Tech; 2013. Available from: http://hdl.handle.net/1853/47691

8. Arney, Dale Curtis. Rule-based graph theory to enable exploration of the space system architecture design space.

Degree: PhD, Aerospace Engineering, 2012, Georgia Tech

 NASA's current plans for human spaceflight include an evolutionary series of missions based on a steady increase in capability to explore cis-lunar space, the Moon,… (more)

Subjects/Keywords: Ant colony optimization; Space systems; Graph theory; System architecture; Mathematical analysis; Systems engineering

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APA (6th Edition):

Arney, D. C. (2012). Rule-based graph theory to enable exploration of the space system architecture design space. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/44840

Chicago Manual of Style (16th Edition):

Arney, Dale Curtis. “Rule-based graph theory to enable exploration of the space system architecture design space.” 2012. Doctoral Dissertation, Georgia Tech. Accessed August 08, 2020. http://hdl.handle.net/1853/44840.

MLA Handbook (7th Edition):

Arney, Dale Curtis. “Rule-based graph theory to enable exploration of the space system architecture design space.” 2012. Web. 08 Aug 2020.

Vancouver:

Arney DC. Rule-based graph theory to enable exploration of the space system architecture design space. [Internet] [Doctoral dissertation]. Georgia Tech; 2012. [cited 2020 Aug 08]. Available from: http://hdl.handle.net/1853/44840.

Council of Science Editors:

Arney DC. Rule-based graph theory to enable exploration of the space system architecture design space. [Doctoral Dissertation]. Georgia Tech; 2012. Available from: http://hdl.handle.net/1853/44840

9. Singh, Lake Austin. Very low earth orbit propellant collection feasibility assessment.

Degree: PhD, Aerospace Engineering, 2014, Georgia Tech

 This work focuses on the concept of sustainable propellant collection. The concept consists of gathering ambient gas while on-orbit and using it as propellant. Propellant… (more)

Subjects/Keywords: Propellant collection; Electric propulsion; Air-breathing propulsion

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APA (6th Edition):

Singh, L. A. (2014). Very low earth orbit propellant collection feasibility assessment. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/53039

Chicago Manual of Style (16th Edition):

Singh, Lake Austin. “Very low earth orbit propellant collection feasibility assessment.” 2014. Doctoral Dissertation, Georgia Tech. Accessed August 08, 2020. http://hdl.handle.net/1853/53039.

MLA Handbook (7th Edition):

Singh, Lake Austin. “Very low earth orbit propellant collection feasibility assessment.” 2014. Web. 08 Aug 2020.

Vancouver:

Singh LA. Very low earth orbit propellant collection feasibility assessment. [Internet] [Doctoral dissertation]. Georgia Tech; 2014. [cited 2020 Aug 08]. Available from: http://hdl.handle.net/1853/53039.

Council of Science Editors:

Singh LA. Very low earth orbit propellant collection feasibility assessment. [Doctoral Dissertation]. Georgia Tech; 2014. Available from: http://hdl.handle.net/1853/53039

10. Wagner, John Joseph. An adaptive atmospheric prediction algorithm to improve density forecasting for aerocapture guidance processes.

Degree: PhD, Aerospace Engineering, 2014, Georgia Tech

 Many modern entry guidance systems depend on predictions of atmospheric parameters, notably atmospheric density, in order to guide the entry vehicle to some desired final… (more)

Subjects/Keywords: Atmospheric density prediction; Entry vehicle guidance; Ensemble forecasting; Atmospheric density estimator

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APA (6th Edition):

Wagner, J. J. (2014). An adaptive atmospheric prediction algorithm to improve density forecasting for aerocapture guidance processes. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/53046

Chicago Manual of Style (16th Edition):

Wagner, John Joseph. “An adaptive atmospheric prediction algorithm to improve density forecasting for aerocapture guidance processes.” 2014. Doctoral Dissertation, Georgia Tech. Accessed August 08, 2020. http://hdl.handle.net/1853/53046.

MLA Handbook (7th Edition):

Wagner, John Joseph. “An adaptive atmospheric prediction algorithm to improve density forecasting for aerocapture guidance processes.” 2014. Web. 08 Aug 2020.

Vancouver:

Wagner JJ. An adaptive atmospheric prediction algorithm to improve density forecasting for aerocapture guidance processes. [Internet] [Doctoral dissertation]. Georgia Tech; 2014. [cited 2020 Aug 08]. Available from: http://hdl.handle.net/1853/53046.

Council of Science Editors:

Wagner JJ. An adaptive atmospheric prediction algorithm to improve density forecasting for aerocapture guidance processes. [Doctoral Dissertation]. Georgia Tech; 2014. Available from: http://hdl.handle.net/1853/53046

11. Kay, Luciano. How do prizes induce innovation? learning from the Google Lunar X-prize.

Degree: PhD, Public Policy, 2011, Georgia Tech

 Inducement prizes-where cash rewards are given to motivate the attainment of targets – have been long used to encourage scientific research, develop technological innovations, or stimulate… (more)

Subjects/Keywords: Inducement prizes; Innovation policy; Northrop Grumman Lunar Lander Challenge; Ansari X Prize; Google Lunar X Prize; Aerospace industry; Lunar robotic exploration; Incentive mechanisms; Technological innovation; Incentive awards; Technological innovations

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APA (6th Edition):

Kay, L. (2011). How do prizes induce innovation? learning from the Google Lunar X-prize. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/41193

Chicago Manual of Style (16th Edition):

Kay, Luciano. “How do prizes induce innovation? learning from the Google Lunar X-prize.” 2011. Doctoral Dissertation, Georgia Tech. Accessed August 08, 2020. http://hdl.handle.net/1853/41193.

MLA Handbook (7th Edition):

Kay, Luciano. “How do prizes induce innovation? learning from the Google Lunar X-prize.” 2011. Web. 08 Aug 2020.

Vancouver:

Kay L. How do prizes induce innovation? learning from the Google Lunar X-prize. [Internet] [Doctoral dissertation]. Georgia Tech; 2011. [cited 2020 Aug 08]. Available from: http://hdl.handle.net/1853/41193.

Council of Science Editors:

Kay L. How do prizes induce innovation? learning from the Google Lunar X-prize. [Doctoral Dissertation]. Georgia Tech; 2011. Available from: http://hdl.handle.net/1853/41193

12. Young, James Jamy. A value proposition for lunar architectures utilizing on-orbit propellant refueling.

Degree: PhD, Aerospace Engineering, 2009, Georgia Tech

 In 2004, President Bush addressed the nation and presented NASA's new vision for space exploration. This vision included the completion of the International Space Station,… (more)

Subjects/Keywords: NASA; Refueling; Depot; ESAS; Young; Propellants; Artificial satellites

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APA (6th Edition):

Young, J. J. (2009). A value proposition for lunar architectures utilizing on-orbit propellant refueling. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/28149

Chicago Manual of Style (16th Edition):

Young, James Jamy. “A value proposition for lunar architectures utilizing on-orbit propellant refueling.” 2009. Doctoral Dissertation, Georgia Tech. Accessed August 08, 2020. http://hdl.handle.net/1853/28149.

MLA Handbook (7th Edition):

Young, James Jamy. “A value proposition for lunar architectures utilizing on-orbit propellant refueling.” 2009. Web. 08 Aug 2020.

Vancouver:

Young JJ. A value proposition for lunar architectures utilizing on-orbit propellant refueling. [Internet] [Doctoral dissertation]. Georgia Tech; 2009. [cited 2020 Aug 08]. Available from: http://hdl.handle.net/1853/28149.

Council of Science Editors:

Young JJ. A value proposition for lunar architectures utilizing on-orbit propellant refueling. [Doctoral Dissertation]. Georgia Tech; 2009. Available from: http://hdl.handle.net/1853/28149

13. Axdahl, Erik Lee. A study of premixed, shock-induced combustion with application to hypervelocity flight.

Degree: PhD, Aerospace Engineering, 2013, Georgia Tech

 One of the current goals of research in hypersonic, airbreathing propulsion is access to higher Mach numbers. A strong driver of this goal is the… (more)

Subjects/Keywords: PMSIC; Combustion; Hypervelocity; Hypersonic; Injection; Hypersonic planes; Aerodynamics, Hypersonic; Combustion; Mach number; Aerodynamics; Aerodynamics, Supersonic; Airplanes Scramjet engines

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APA (6th Edition):

Axdahl, E. L. (2013). A study of premixed, shock-induced combustion with application to hypervelocity flight. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/50290

Chicago Manual of Style (16th Edition):

Axdahl, Erik Lee. “A study of premixed, shock-induced combustion with application to hypervelocity flight.” 2013. Doctoral Dissertation, Georgia Tech. Accessed August 08, 2020. http://hdl.handle.net/1853/50290.

MLA Handbook (7th Edition):

Axdahl, Erik Lee. “A study of premixed, shock-induced combustion with application to hypervelocity flight.” 2013. Web. 08 Aug 2020.

Vancouver:

Axdahl EL. A study of premixed, shock-induced combustion with application to hypervelocity flight. [Internet] [Doctoral dissertation]. Georgia Tech; 2013. [cited 2020 Aug 08]. Available from: http://hdl.handle.net/1853/50290.

Council of Science Editors:

Axdahl EL. A study of premixed, shock-induced combustion with application to hypervelocity flight. [Doctoral Dissertation]. Georgia Tech; 2013. Available from: http://hdl.handle.net/1853/50290

14. Romaniw, Yuriy Alexander. The relationship between light-weighting with carbon fiber reinforced polymers and the life cycle environmental impacts of orbital launch rockets.

Degree: PhD, Mechanical Engineering, 2013, Georgia Tech

 A study was undertaken to determine if light-weighting orbital launch vehicles (rockets) improves lifetime environmental impacts of the vehicle. Light-weighting is performed by a material… (more)

Subjects/Keywords: Carbon fiber reinforced polymer; CFRP; Carbon fiber; Rocket; Orbital launch vehicle; Environmental impact; Life cycle assessment; LCA; Launch vehicles (Astronautics); Carbon fiber-reinforced plastics; Life cycle costing; Environmental impact analysis

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APA (6th Edition):

Romaniw, Y. A. (2013). The relationship between light-weighting with carbon fiber reinforced polymers and the life cycle environmental impacts of orbital launch rockets. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/50298

Chicago Manual of Style (16th Edition):

Romaniw, Yuriy Alexander. “The relationship between light-weighting with carbon fiber reinforced polymers and the life cycle environmental impacts of orbital launch rockets.” 2013. Doctoral Dissertation, Georgia Tech. Accessed August 08, 2020. http://hdl.handle.net/1853/50298.

MLA Handbook (7th Edition):

Romaniw, Yuriy Alexander. “The relationship between light-weighting with carbon fiber reinforced polymers and the life cycle environmental impacts of orbital launch rockets.” 2013. Web. 08 Aug 2020.

Vancouver:

Romaniw YA. The relationship between light-weighting with carbon fiber reinforced polymers and the life cycle environmental impacts of orbital launch rockets. [Internet] [Doctoral dissertation]. Georgia Tech; 2013. [cited 2020 Aug 08]. Available from: http://hdl.handle.net/1853/50298.

Council of Science Editors:

Romaniw YA. The relationship between light-weighting with carbon fiber reinforced polymers and the life cycle environmental impacts of orbital launch rockets. [Doctoral Dissertation]. Georgia Tech; 2013. Available from: http://hdl.handle.net/1853/50298

15. Cordell, Christopher E. Computational fluid dynamics and analytical modeling of supersonic retropropulsion flowfield structures across a wide range of potential vehicle configurations.

Degree: PhD, Aerospace Engineering, 2013, Georgia Tech

 For the past four decades, Mars missions have relied on Viking heritage technology for supersonic descent. Extending the use of propulsion, which is required for… (more)

Subjects/Keywords: Supersonic retropropulsion; Computational fluid dynamics; Analytical modeling; Plume structure; Propulsion systems; Computational fluid dynamics; Space vehicles; Space vehicles Landing

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APA (6th Edition):

Cordell, C. E. (2013). Computational fluid dynamics and analytical modeling of supersonic retropropulsion flowfield structures across a wide range of potential vehicle configurations. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/50355

Chicago Manual of Style (16th Edition):

Cordell, Christopher E. “Computational fluid dynamics and analytical modeling of supersonic retropropulsion flowfield structures across a wide range of potential vehicle configurations.” 2013. Doctoral Dissertation, Georgia Tech. Accessed August 08, 2020. http://hdl.handle.net/1853/50355.

MLA Handbook (7th Edition):

Cordell, Christopher E. “Computational fluid dynamics and analytical modeling of supersonic retropropulsion flowfield structures across a wide range of potential vehicle configurations.” 2013. Web. 08 Aug 2020.

Vancouver:

Cordell CE. Computational fluid dynamics and analytical modeling of supersonic retropropulsion flowfield structures across a wide range of potential vehicle configurations. [Internet] [Doctoral dissertation]. Georgia Tech; 2013. [cited 2020 Aug 08]. Available from: http://hdl.handle.net/1853/50355.

Council of Science Editors:

Cordell CE. Computational fluid dynamics and analytical modeling of supersonic retropropulsion flowfield structures across a wide range of potential vehicle configurations. [Doctoral Dissertation]. Georgia Tech; 2013. Available from: http://hdl.handle.net/1853/50355

16. Pathak, Mihir Gaurang. Periodic flow physics in porous media of regenerative cryocoolers.

Degree: PhD, Mechanical Engineering, 2013, Georgia Tech

 Pulse tube cryocoolers (PTC) are a class of rugged and high-endurance refrigeration systems that operate without moving parts at their low temperature ends, and are… (more)

Subjects/Keywords: Regenerator; ErPr; Nusselt; Porous media; Pore level; Periodic flow; Oscillatory flow; Darcy permeability; Forchheimer; Hydrodynamic; Thermal dispersion; Conjugate; Heat transfer; CFD; Pulse tube; Cryocooler; Cryogenics; Physics; Rare-Earth; Steady flow; Low temperature engineering; Materials at low temperatures; Porous materials Thermal properties; Porous materials

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APA (6th Edition):

Pathak, M. G. (2013). Periodic flow physics in porous media of regenerative cryocoolers. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/49056

Chicago Manual of Style (16th Edition):

Pathak, Mihir Gaurang. “Periodic flow physics in porous media of regenerative cryocoolers.” 2013. Doctoral Dissertation, Georgia Tech. Accessed August 08, 2020. http://hdl.handle.net/1853/49056.

MLA Handbook (7th Edition):

Pathak, Mihir Gaurang. “Periodic flow physics in porous media of regenerative cryocoolers.” 2013. Web. 08 Aug 2020.

Vancouver:

Pathak MG. Periodic flow physics in porous media of regenerative cryocoolers. [Internet] [Doctoral dissertation]. Georgia Tech; 2013. [cited 2020 Aug 08]. Available from: http://hdl.handle.net/1853/49056.

Council of Science Editors:

Pathak MG. Periodic flow physics in porous media of regenerative cryocoolers. [Doctoral Dissertation]. Georgia Tech; 2013. Available from: http://hdl.handle.net/1853/49056


Georgia Tech

17. 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 August 08, 2020. 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. 08 Aug 2020.

Vancouver:

Hart PB. A plm implementation for aerospace systems engineering-conceptual rotorcraft design. [Internet] [Masters thesis]. Georgia Tech; 2009. [cited 2020 Aug 08]. 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

18. 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 August 08, 2020. http://hdl.handle.net/1853/10469.

MLA Handbook (7th Edition):

Borer, Nicholas Keith. “Decision Making Strategies for Probabilistic Aerospace Systems Design.” 2006. Web. 08 Aug 2020.

Vancouver:

Borer NK. Decision Making Strategies for Probabilistic Aerospace Systems Design. [Internet] [Doctoral dissertation]. Georgia Tech; 2006. [cited 2020 Aug 08]. 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


Georgia Tech

19. McDonald, Robert Alan. Error Propagation and Metamodeling for a Fidelity Tradeoff Capability in Complex Systems Design.

Degree: PhD, Aerospace Engineering, 2006, Georgia Tech

 Complex man-made systems are ubiquitous in modern technological society. The national air transportation infrastructure and the aircraft that operate within it, the highways stretching coast-to-coast… (more)

Subjects/Keywords: Error propagation; Metamodeling; Gaussian processes; Systems design; Design; Complex systems; Systems engineering; Error analysis (Mathematics); Decision support systems

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APA (6th Edition):

McDonald, R. A. (2006). Error Propagation and Metamodeling for a Fidelity Tradeoff Capability in Complex Systems Design. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/11568

Chicago Manual of Style (16th Edition):

McDonald, Robert Alan. “Error Propagation and Metamodeling for a Fidelity Tradeoff Capability in Complex Systems Design.” 2006. Doctoral Dissertation, Georgia Tech. Accessed August 08, 2020. http://hdl.handle.net/1853/11568.

MLA Handbook (7th Edition):

McDonald, Robert Alan. “Error Propagation and Metamodeling for a Fidelity Tradeoff Capability in Complex Systems Design.” 2006. Web. 08 Aug 2020.

Vancouver:

McDonald RA. Error Propagation and Metamodeling for a Fidelity Tradeoff Capability in Complex Systems Design. [Internet] [Doctoral dissertation]. Georgia Tech; 2006. [cited 2020 Aug 08]. Available from: http://hdl.handle.net/1853/11568.

Council of Science Editors:

McDonald RA. Error Propagation and Metamodeling for a Fidelity Tradeoff Capability in Complex Systems Design. [Doctoral Dissertation]. Georgia Tech; 2006. Available from: http://hdl.handle.net/1853/11568


Georgia Tech

20. 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 August 08, 2020. 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. 08 Aug 2020.

Vancouver:

Young DA. An Innovative Methodology for Allocating Reliability and Cost in a Lunar Exploration Architecture. [Internet] [Doctoral dissertation]. Georgia Tech; 2007. [cited 2020 Aug 08]. 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


Georgia Tech

21. Villeneuve, Frédéric. A Method for Concept and Technology Exploration of Aerospace Architectures.

Degree: PhD, Aerospace Engineering, 2007, Georgia Tech

 This dissertation presents the development of a new concept and technology exploration methodology for aerospace architectures. The methodology is based on modeling the design space… (more)

Subjects/Keywords: Design; Graph; Ant colony; Technology; Concept; Mathematical optimization; Swarm intelligence; Ant algorithms; Launch vehicles (Astronautics) Design and construction

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APA (6th Edition):

Villeneuve, F. (2007). A Method for Concept and Technology Exploration of Aerospace Architectures. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/16212

Chicago Manual of Style (16th Edition):

Villeneuve, Frédéric. “A Method for Concept and Technology Exploration of Aerospace Architectures.” 2007. Doctoral Dissertation, Georgia Tech. Accessed August 08, 2020. http://hdl.handle.net/1853/16212.

MLA Handbook (7th Edition):

Villeneuve, Frédéric. “A Method for Concept and Technology Exploration of Aerospace Architectures.” 2007. Web. 08 Aug 2020.

Vancouver:

Villeneuve F. A Method for Concept and Technology Exploration of Aerospace Architectures. [Internet] [Doctoral dissertation]. Georgia Tech; 2007. [cited 2020 Aug 08]. Available from: http://hdl.handle.net/1853/16212.

Council of Science Editors:

Villeneuve F. A Method for Concept and Technology Exploration of Aerospace Architectures. [Doctoral Dissertation]. Georgia Tech; 2007. Available from: http://hdl.handle.net/1853/16212


Georgia Tech

22. Lewe, Jung-Ho. An Integrated Decision-Making Framework for Transportation Architectures: Application to Aviation Systems Design.

Degree: PhD, Aerospace Engineering, 2005, Georgia Tech

 The National Transportation System (NTS) is undoubtedly a complex system-of-systems – a collection of diverse 'things' that evolve over time, organized at multiple levels, to achieve… (more)

Subjects/Keywords: Aircraft concept evaluation; Personal air vehicles; Agent-based simulation; Demand prediction; Tournament Logit; Induced travel; Multimodal transport model; Forecasting; Transportation Planning; Aeronautics, Commercial United States Planning

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

APA (6th Edition):

Lewe, J. (2005). An Integrated Decision-Making Framework for Transportation Architectures: Application to Aviation Systems Design. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/6918

Chicago Manual of Style (16th Edition):

Lewe, Jung-Ho. “An Integrated Decision-Making Framework for Transportation Architectures: Application to Aviation Systems Design.” 2005. Doctoral Dissertation, Georgia Tech. Accessed August 08, 2020. http://hdl.handle.net/1853/6918.

MLA Handbook (7th Edition):

Lewe, Jung-Ho. “An Integrated Decision-Making Framework for Transportation Architectures: Application to Aviation Systems Design.” 2005. Web. 08 Aug 2020.

Vancouver:

Lewe J. An Integrated Decision-Making Framework for Transportation Architectures: Application to Aviation Systems Design. [Internet] [Doctoral dissertation]. Georgia Tech; 2005. [cited 2020 Aug 08]. Available from: http://hdl.handle.net/1853/6918.

Council of Science Editors:

Lewe J. An Integrated Decision-Making Framework for Transportation Architectures: Application to Aviation Systems Design. [Doctoral Dissertation]. Georgia Tech; 2005. Available from: http://hdl.handle.net/1853/6918

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