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You searched for subject:(Aerodynamic decelerator). Showing records 1 – 5 of 5 total matches.

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Georgia Tech

1. Clark, Ian Gauld. Aerodynamic design, analysis, and validation of a supersonic inflatable decelerator.

Degree: PhD, Aerospace Engineering, 2009, Georgia Tech

 Since the 1970's, NASA has relied on the use of rigid aeroshells and supersonic parachutes to enable robotic mission to Mars. These technologies are constrained… (more)

Subjects/Keywords: Supersonic decelerator; Inflatable aerodynamic decelerator; Tension cone; Ballute; Aerodynamic decelerator; Atmospheric entry; Computational fluid dynamics; Acceleration (Mechanics); Ablation (Aerothermodynamics)

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APA (6th Edition):

Clark, I. G. (2009). Aerodynamic design, analysis, and validation of a supersonic inflatable decelerator. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/34708

Chicago Manual of Style (16th Edition):

Clark, Ian Gauld. “Aerodynamic design, analysis, and validation of a supersonic inflatable decelerator.” 2009. Doctoral Dissertation, Georgia Tech. Accessed October 19, 2019. http://hdl.handle.net/1853/34708.

MLA Handbook (7th Edition):

Clark, Ian Gauld. “Aerodynamic design, analysis, and validation of a supersonic inflatable decelerator.” 2009. Web. 19 Oct 2019.

Vancouver:

Clark IG. Aerodynamic design, analysis, and validation of a supersonic inflatable decelerator. [Internet] [Doctoral dissertation]. Georgia Tech; 2009. [cited 2019 Oct 19]. Available from: http://hdl.handle.net/1853/34708.

Council of Science Editors:

Clark IG. Aerodynamic design, analysis, and validation of a supersonic inflatable decelerator. [Doctoral Dissertation]. Georgia Tech; 2009. Available from: http://hdl.handle.net/1853/34708


Georgia Tech

2. Bopp, Matthew Scott. A time accurate fluid-structure interaction framework using a Cartesian grid CFD solver.

Degree: PhD, Aerospace Engineering, 2017, Georgia Tech

 The landing of the Mars Science Laboratory (MSL) in 2012 demonstrated the limits of supersonic planetary entry technology through the use of a disk-gap-band parachute… (more)

Subjects/Keywords: CFD; FSI; Cartesian; EDL; Aerodynamic decelerator; Fluid dynamics; Structural dynamics; Coupling; C++; Immersed boundary method

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APA (6th Edition):

Bopp, M. S. (2017). A time accurate fluid-structure interaction framework using a Cartesian grid CFD solver. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/59257

Chicago Manual of Style (16th Edition):

Bopp, Matthew Scott. “A time accurate fluid-structure interaction framework using a Cartesian grid CFD solver.” 2017. Doctoral Dissertation, Georgia Tech. Accessed October 19, 2019. http://hdl.handle.net/1853/59257.

MLA Handbook (7th Edition):

Bopp, Matthew Scott. “A time accurate fluid-structure interaction framework using a Cartesian grid CFD solver.” 2017. Web. 19 Oct 2019.

Vancouver:

Bopp MS. A time accurate fluid-structure interaction framework using a Cartesian grid CFD solver. [Internet] [Doctoral dissertation]. Georgia Tech; 2017. [cited 2019 Oct 19]. Available from: http://hdl.handle.net/1853/59257.

Council of Science Editors:

Bopp MS. A time accurate fluid-structure interaction framework using a Cartesian grid CFD solver. [Doctoral Dissertation]. Georgia Tech; 2017. Available from: http://hdl.handle.net/1853/59257


University of Colorado

3. Skeen, Michael Anthony. Conceptual Modeling and Analysis of Drag-Augmented Supersonic Retropropulsion for Application in Mars Entry, Descent, and Landing Vehicles.

Degree: MS, Aerospace Engineering Sciences, 2013, University of Colorado

  The development of new decelerator technologies will be required as the desired payload mass for future Mars landing missions increases beyond the current state-of-the-art… (more)

Subjects/Keywords: Aerodynamic-propulsive interaction; Descent trajectory; Mars landing vehicle; Shock cascade; Supersonic decelerator; Supersonic retropropulsion; Aeronautical Vehicles; Aerospace Engineering; Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Skeen, M. A. (2013). Conceptual Modeling and Analysis of Drag-Augmented Supersonic Retropropulsion for Application in Mars Entry, Descent, and Landing Vehicles. (Masters Thesis). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/65

Chicago Manual of Style (16th Edition):

Skeen, Michael Anthony. “Conceptual Modeling and Analysis of Drag-Augmented Supersonic Retropropulsion for Application in Mars Entry, Descent, and Landing Vehicles.” 2013. Masters Thesis, University of Colorado. Accessed October 19, 2019. http://scholar.colorado.edu/asen_gradetds/65.

MLA Handbook (7th Edition):

Skeen, Michael Anthony. “Conceptual Modeling and Analysis of Drag-Augmented Supersonic Retropropulsion for Application in Mars Entry, Descent, and Landing Vehicles.” 2013. Web. 19 Oct 2019.

Vancouver:

Skeen MA. Conceptual Modeling and Analysis of Drag-Augmented Supersonic Retropropulsion for Application in Mars Entry, Descent, and Landing Vehicles. [Internet] [Masters thesis]. University of Colorado; 2013. [cited 2019 Oct 19]. Available from: http://scholar.colorado.edu/asen_gradetds/65.

Council of Science Editors:

Skeen MA. Conceptual Modeling and Analysis of Drag-Augmented Supersonic Retropropulsion for Application in Mars Entry, Descent, and Landing Vehicles. [Masters Thesis]. University of Colorado; 2013. Available from: http://scholar.colorado.edu/asen_gradetds/65


University of Maine

4. Clapp, Joshua. Structural Behavior of Inflatable, Reinforced, Braided, Tubular Members.

Degree: PhD, Civil Engineering, 2017, University of Maine

  The Hypersonic Inflatable Aerodynamic Decelerator (HIAD) system being developed by the National Aeronautics and Space Administration (NASA) is an inflatable structure composed of multiple,… (more)

Subjects/Keywords: inflatable structures; braided tube; netting theory; structural response; Hypersonic Inflatable Aerodynamic Decelerator; digital image correlation; Space Vehicles; Structural Engineering; Structures and Materials

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

APA (6th Edition):

Clapp, J. (2017). Structural Behavior of Inflatable, Reinforced, Braided, Tubular Members. (Doctoral Dissertation). University of Maine. Retrieved from https://digitalcommons.library.umaine.edu/etd/2741

Chicago Manual of Style (16th Edition):

Clapp, Joshua. “Structural Behavior of Inflatable, Reinforced, Braided, Tubular Members.” 2017. Doctoral Dissertation, University of Maine. Accessed October 19, 2019. https://digitalcommons.library.umaine.edu/etd/2741.

MLA Handbook (7th Edition):

Clapp, Joshua. “Structural Behavior of Inflatable, Reinforced, Braided, Tubular Members.” 2017. Web. 19 Oct 2019.

Vancouver:

Clapp J. Structural Behavior of Inflatable, Reinforced, Braided, Tubular Members. [Internet] [Doctoral dissertation]. University of Maine; 2017. [cited 2019 Oct 19]. Available from: https://digitalcommons.library.umaine.edu/etd/2741.

Council of Science Editors:

Clapp J. Structural Behavior of Inflatable, Reinforced, Braided, Tubular Members. [Doctoral Dissertation]. University of Maine; 2017. Available from: https://digitalcommons.library.umaine.edu/etd/2741

5. Hill, Jeremy Lee. Mechanical property determination for flexible material systems.

Degree: PhD, Aerospace Engineering, 2016, Georgia Tech

 Inflatable Aerodynamic Decelerators (IADs) are a candidate technology NASA began investigating in the late 1960’s. Compared to supersonic parachutes, IADs represent a decelerator option capable… (more)

Subjects/Keywords: Inflatable aerodynamic decelerator; Flexible material systems; Finite element analysis; Multi-scale modeling; Parameter identification

…HIAD Hypersonic Inflatable Aerodynamic Decelerator IAD Inflatable Aerodynamic Decelerator… …SIAD Supersonic Inflatable Aerodynamic Decelerator SRSM Sequential Response Surface… …The Hypersonic Inflatable Aerodynamic Decelerator (HIAD) and Low Density… …Supersonic Decelerator LSR Least Squares Residual ME Margin of Error xiv MSE Mean Square… …Aerodynamic Decelerators (IADs) are a candidate technology NASA began investigating in the… 

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

APA (6th Edition):

Hill, J. L. (2016). Mechanical property determination for flexible material systems. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/54993

Chicago Manual of Style (16th Edition):

Hill, Jeremy Lee. “Mechanical property determination for flexible material systems.” 2016. Doctoral Dissertation, Georgia Tech. Accessed October 19, 2019. http://hdl.handle.net/1853/54993.

MLA Handbook (7th Edition):

Hill, Jeremy Lee. “Mechanical property determination for flexible material systems.” 2016. Web. 19 Oct 2019.

Vancouver:

Hill JL. Mechanical property determination for flexible material systems. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2019 Oct 19]. Available from: http://hdl.handle.net/1853/54993.

Council of Science Editors:

Hill JL. Mechanical property determination for flexible material systems. [Doctoral Dissertation]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/54993

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