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You searched for +publisher:"University of Colorado" +contributor:("Kenneth Jansen"). Showing records 1 – 10 of 10 total matches.

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University of Colorado

1. Jung, Timothy Paul. Modified Linear Theory Aircraft Design Tools and Sonic Boom Minimization Strategy Applied to Signature Freezing via F-function Lobe Balancing.

Degree: PhD, Aerospace Engineering Sciences, 2012, University of Colorado

  Commercial supersonic travel has strong business potential; however, in order for the Federal Aviation Administration to lift its ban on supersonic flight overland, designers… (more)

Subjects/Keywords: F-function; Lobe Balancing; Modified Linear Theory; Sonic Boom; Supersonic; Acoustics, Dynamics, and Controls; Aerospace Engineering

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APA (6th Edition):

Jung, T. P. (2012). Modified Linear Theory Aircraft Design Tools and Sonic Boom Minimization Strategy Applied to Signature Freezing via F-function Lobe Balancing. (Doctoral Dissertation). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/49

Chicago Manual of Style (16th Edition):

Jung, Timothy Paul. “Modified Linear Theory Aircraft Design Tools and Sonic Boom Minimization Strategy Applied to Signature Freezing via F-function Lobe Balancing.” 2012. Doctoral Dissertation, University of Colorado. Accessed November 15, 2019. http://scholar.colorado.edu/asen_gradetds/49.

MLA Handbook (7th Edition):

Jung, Timothy Paul. “Modified Linear Theory Aircraft Design Tools and Sonic Boom Minimization Strategy Applied to Signature Freezing via F-function Lobe Balancing.” 2012. Web. 15 Nov 2019.

Vancouver:

Jung TP. Modified Linear Theory Aircraft Design Tools and Sonic Boom Minimization Strategy Applied to Signature Freezing via F-function Lobe Balancing. [Internet] [Doctoral dissertation]. University of Colorado; 2012. [cited 2019 Nov 15]. Available from: http://scholar.colorado.edu/asen_gradetds/49.

Council of Science Editors:

Jung TP. Modified Linear Theory Aircraft Design Tools and Sonic Boom Minimization Strategy Applied to Signature Freezing via F-function Lobe Balancing. [Doctoral Dissertation]. University of Colorado; 2012. Available from: http://scholar.colorado.edu/asen_gradetds/49


University of Colorado

2. Bateman, Daniel Gretz. Design and Qualication of an Upstream Gust Generator in a Low-Speed Wind Tunnel.

Degree: MS, Aerospace Engineering Sciences, 2017, University of Colorado

  A longitudinal gust generator was designed, constructed, installed and tested in the low-speed research wind tunnel within the Experimental Aerodynamics Laboratory at University of… (more)

Subjects/Keywords: aerodynamics; gust; unsteady; wind tunnel; Experimental Aerodynamics Laboratory; dynamic shutter (louver) system; Aerospace Engineering

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APA (6th Edition):

Bateman, D. G. (2017). Design and Qualication of an Upstream Gust Generator in a Low-Speed Wind Tunnel. (Masters Thesis). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/196

Chicago Manual of Style (16th Edition):

Bateman, Daniel Gretz. “Design and Qualication of an Upstream Gust Generator in a Low-Speed Wind Tunnel.” 2017. Masters Thesis, University of Colorado. Accessed November 15, 2019. https://scholar.colorado.edu/asen_gradetds/196.

MLA Handbook (7th Edition):

Bateman, Daniel Gretz. “Design and Qualication of an Upstream Gust Generator in a Low-Speed Wind Tunnel.” 2017. Web. 15 Nov 2019.

Vancouver:

Bateman DG. Design and Qualication of an Upstream Gust Generator in a Low-Speed Wind Tunnel. [Internet] [Masters thesis]. University of Colorado; 2017. [cited 2019 Nov 15]. Available from: https://scholar.colorado.edu/asen_gradetds/196.

Council of Science Editors:

Bateman DG. Design and Qualication of an Upstream Gust Generator in a Low-Speed Wind Tunnel. [Masters Thesis]. University of Colorado; 2017. Available from: https://scholar.colorado.edu/asen_gradetds/196


University of Colorado

3. Basore, Kevin Daniel. Error Analysis on Multi-Fidelity Design Spaces through Surrogate Modeling with an Emphasis on Scramjet Combustion.

Degree: MS, Aerospace Engineering Sciences, 2012, University of Colorado

  Hypersonic vehicle design is a challenging problem. The main obstacle that makes this work challenging is the non-linear interdependency between each of the vehicle’s… (more)

Subjects/Keywords: Hypersonics; Surrogate Modeling; Vehicle Design; Aeronautical Vehicles; Aerospace Engineering

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APA (6th Edition):

Basore, K. D. (2012). Error Analysis on Multi-Fidelity Design Spaces through Surrogate Modeling with an Emphasis on Scramjet Combustion. (Masters Thesis). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/36

Chicago Manual of Style (16th Edition):

Basore, Kevin Daniel. “Error Analysis on Multi-Fidelity Design Spaces through Surrogate Modeling with an Emphasis on Scramjet Combustion.” 2012. Masters Thesis, University of Colorado. Accessed November 15, 2019. http://scholar.colorado.edu/asen_gradetds/36.

MLA Handbook (7th Edition):

Basore, Kevin Daniel. “Error Analysis on Multi-Fidelity Design Spaces through Surrogate Modeling with an Emphasis on Scramjet Combustion.” 2012. Web. 15 Nov 2019.

Vancouver:

Basore KD. Error Analysis on Multi-Fidelity Design Spaces through Surrogate Modeling with an Emphasis on Scramjet Combustion. [Internet] [Masters thesis]. University of Colorado; 2012. [cited 2019 Nov 15]. Available from: http://scholar.colorado.edu/asen_gradetds/36.

Council of Science Editors:

Basore KD. Error Analysis on Multi-Fidelity Design Spaces through Surrogate Modeling with an Emphasis on Scramjet Combustion. [Masters Thesis]. University of Colorado; 2012. Available from: http://scholar.colorado.edu/asen_gradetds/36


University of Colorado

4. Pope, David. Implementing a Loosely Coupled Fluid Structure Interaction Finite Element Model in PHASTA.

Degree: MS, Aerospace Engineering Sciences, 2015, University of Colorado

  Fluid Structure Interaction problems are an important multi-physics phenomenon in the design of aerospace vehicles and other engineering applications. A variety of computational fluid… (more)

Subjects/Keywords: ALE; Structural Equations; Aerodynamics and Fluid Mechanics

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APA (6th Edition):

Pope, D. (2015). Implementing a Loosely Coupled Fluid Structure Interaction Finite Element Model in PHASTA. (Masters Thesis). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/109

Chicago Manual of Style (16th Edition):

Pope, David. “Implementing a Loosely Coupled Fluid Structure Interaction Finite Element Model in PHASTA.” 2015. Masters Thesis, University of Colorado. Accessed November 15, 2019. http://scholar.colorado.edu/asen_gradetds/109.

MLA Handbook (7th Edition):

Pope, David. “Implementing a Loosely Coupled Fluid Structure Interaction Finite Element Model in PHASTA.” 2015. Web. 15 Nov 2019.

Vancouver:

Pope D. Implementing a Loosely Coupled Fluid Structure Interaction Finite Element Model in PHASTA. [Internet] [Masters thesis]. University of Colorado; 2015. [cited 2019 Nov 15]. Available from: http://scholar.colorado.edu/asen_gradetds/109.

Council of Science Editors:

Pope D. Implementing a Loosely Coupled Fluid Structure Interaction Finite Element Model in PHASTA. [Masters Thesis]. University of Colorado; 2015. Available from: http://scholar.colorado.edu/asen_gradetds/109


University of Colorado

5. Chitale, Kedar C. Anisotropic Mesh Adaptivity for Turbulent Flows with Boundary Layers.

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

  Turbulent flows are found everywhere in nature and are studied, analyzed and simulated using various experimental and numerical tools. For computational analysis, a variety… (more)

Subjects/Keywords: Adaptive mesh generation; Anisotropic adaptivity; Boundary layers; Computational fluid dynamics; Multi element wings; Turbulent flows; Aerospace Engineering

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APA (6th Edition):

Chitale, K. C. (2013). Anisotropic Mesh Adaptivity for Turbulent Flows with Boundary Layers. (Doctoral Dissertation). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/68

Chicago Manual of Style (16th Edition):

Chitale, Kedar C. “Anisotropic Mesh Adaptivity for Turbulent Flows with Boundary Layers.” 2013. Doctoral Dissertation, University of Colorado. Accessed November 15, 2019. http://scholar.colorado.edu/asen_gradetds/68.

MLA Handbook (7th Edition):

Chitale, Kedar C. “Anisotropic Mesh Adaptivity for Turbulent Flows with Boundary Layers.” 2013. Web. 15 Nov 2019.

Vancouver:

Chitale KC. Anisotropic Mesh Adaptivity for Turbulent Flows with Boundary Layers. [Internet] [Doctoral dissertation]. University of Colorado; 2013. [cited 2019 Nov 15]. Available from: http://scholar.colorado.edu/asen_gradetds/68.

Council of Science Editors:

Chitale KC. Anisotropic Mesh Adaptivity for Turbulent Flows with Boundary Layers. [Doctoral Dissertation]. University of Colorado; 2013. Available from: http://scholar.colorado.edu/asen_gradetds/68


University of Colorado

6. Woods, Charles Nathan. Enabling Design-Oriented Fluid Simulations: Verification with Discontinuous Manufactured Solutions and Automatic Grid Generation with Moving Coordinates.

Degree: PhD, Aerospace Engineering Sciences, 2015, University of Colorado

  Computer simulations of complex mathematical models are a powerful tool for design, but they introduce uncertainties which can lead to poor design choices when… (more)

Subjects/Keywords: Discontinuous Integration; Discontinuous Manufactured Solutions; Manufactured Solutions; Quadrature; Unified Coordinate System; Verification; Applied Mathematics; Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Woods, C. N. (2015). Enabling Design-Oriented Fluid Simulations: Verification with Discontinuous Manufactured Solutions and Automatic Grid Generation with Moving Coordinates. (Doctoral Dissertation). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/98

Chicago Manual of Style (16th Edition):

Woods, Charles Nathan. “Enabling Design-Oriented Fluid Simulations: Verification with Discontinuous Manufactured Solutions and Automatic Grid Generation with Moving Coordinates.” 2015. Doctoral Dissertation, University of Colorado. Accessed November 15, 2019. http://scholar.colorado.edu/asen_gradetds/98.

MLA Handbook (7th Edition):

Woods, Charles Nathan. “Enabling Design-Oriented Fluid Simulations: Verification with Discontinuous Manufactured Solutions and Automatic Grid Generation with Moving Coordinates.” 2015. Web. 15 Nov 2019.

Vancouver:

Woods CN. Enabling Design-Oriented Fluid Simulations: Verification with Discontinuous Manufactured Solutions and Automatic Grid Generation with Moving Coordinates. [Internet] [Doctoral dissertation]. University of Colorado; 2015. [cited 2019 Nov 15]. Available from: http://scholar.colorado.edu/asen_gradetds/98.

Council of Science Editors:

Woods CN. Enabling Design-Oriented Fluid Simulations: Verification with Discontinuous Manufactured Solutions and Automatic Grid Generation with Moving Coordinates. [Doctoral Dissertation]. University of Colorado; 2015. Available from: http://scholar.colorado.edu/asen_gradetds/98


University of Colorado

7. Woolwine, Kyle Joseph. A Reduced Order Model of an External Compression Supersonic Inlet.

Degree: PhD, Aerospace Engineering Sciences, 2016, University of Colorado

 The research contained in this thesis was performed in order to model the external compression axisymmetric inlet portion of a supersonic jet engine in a… (more)

Subjects/Keywords: CFD; Inlet; Reduced Order Modeiling; Supersonic; Aerospace Engineering

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APA (6th Edition):

Woolwine, K. J. (2016). A Reduced Order Model of an External Compression Supersonic Inlet. (Doctoral Dissertation). University of Colorado. Retrieved from http://scholar.colorado.edu/asen_gradetds/145

Chicago Manual of Style (16th Edition):

Woolwine, Kyle Joseph. “A Reduced Order Model of an External Compression Supersonic Inlet.” 2016. Doctoral Dissertation, University of Colorado. Accessed November 15, 2019. http://scholar.colorado.edu/asen_gradetds/145.

MLA Handbook (7th Edition):

Woolwine, Kyle Joseph. “A Reduced Order Model of an External Compression Supersonic Inlet.” 2016. Web. 15 Nov 2019.

Vancouver:

Woolwine KJ. A Reduced Order Model of an External Compression Supersonic Inlet. [Internet] [Doctoral dissertation]. University of Colorado; 2016. [cited 2019 Nov 15]. Available from: http://scholar.colorado.edu/asen_gradetds/145.

Council of Science Editors:

Woolwine KJ. A Reduced Order Model of an External Compression Supersonic Inlet. [Doctoral Dissertation]. University of Colorado; 2016. Available from: http://scholar.colorado.edu/asen_gradetds/145


University of Colorado

8. Coley, Christopher Joel. Residual-Based Large Eddy Simulation of Turbulent Flows Using Divergence-Conforming Discretizations.

Degree: PhD, 2017, University of Colorado

  In this dissertation, a class of methods which combines divergence-conforming discretizations with residual-based subgrid modeling for large eddy simulation of turbulent flows is introduced.… (more)

Subjects/Keywords: Divergence-conforming; Large eddy simulation; Residual-based large eddy simulation; Structure-preserving; Turbulence modeling; Variational multiscale method; Aerospace Engineering

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APA (6th Edition):

Coley, C. J. (2017). Residual-Based Large Eddy Simulation of Turbulent Flows Using Divergence-Conforming Discretizations. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/172

Chicago Manual of Style (16th Edition):

Coley, Christopher Joel. “Residual-Based Large Eddy Simulation of Turbulent Flows Using Divergence-Conforming Discretizations.” 2017. Doctoral Dissertation, University of Colorado. Accessed November 15, 2019. https://scholar.colorado.edu/asen_gradetds/172.

MLA Handbook (7th Edition):

Coley, Christopher Joel. “Residual-Based Large Eddy Simulation of Turbulent Flows Using Divergence-Conforming Discretizations.” 2017. Web. 15 Nov 2019.

Vancouver:

Coley CJ. Residual-Based Large Eddy Simulation of Turbulent Flows Using Divergence-Conforming Discretizations. [Internet] [Doctoral dissertation]. University of Colorado; 2017. [cited 2019 Nov 15]. Available from: https://scholar.colorado.edu/asen_gradetds/172.

Council of Science Editors:

Coley CJ. Residual-Based Large Eddy Simulation of Turbulent Flows Using Divergence-Conforming Discretizations. [Doctoral Dissertation]. University of Colorado; 2017. Available from: https://scholar.colorado.edu/asen_gradetds/172


University of Colorado

9. Engvall, Luke H. Geometrically Exact and Analysis Suitable Mesh Generation Using Rational Bernstein–Bezier Elements.

Degree: PhD, 2018, University of Colorado

  This dissertation presents two novel contributions to the fields of isogeometric analysis and <i>p</i>-version finite elements. First, we present a framework for geometrically exact… (more)

Subjects/Keywords: curvilinear mesh generation; higher-order finite elements; isogeometric analysis; mesh generation; discretization; Engineering; Mechanical Engineering

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APA (6th Edition):

Engvall, L. H. (2018). Geometrically Exact and Analysis Suitable Mesh Generation Using Rational Bernstein–Bezier Elements. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/mcen_gradetds/170

Chicago Manual of Style (16th Edition):

Engvall, Luke H. “Geometrically Exact and Analysis Suitable Mesh Generation Using Rational Bernstein–Bezier Elements.” 2018. Doctoral Dissertation, University of Colorado. Accessed November 15, 2019. https://scholar.colorado.edu/mcen_gradetds/170.

MLA Handbook (7th Edition):

Engvall, Luke H. “Geometrically Exact and Analysis Suitable Mesh Generation Using Rational Bernstein–Bezier Elements.” 2018. Web. 15 Nov 2019.

Vancouver:

Engvall LH. Geometrically Exact and Analysis Suitable Mesh Generation Using Rational Bernstein–Bezier Elements. [Internet] [Doctoral dissertation]. University of Colorado; 2018. [cited 2019 Nov 15]. Available from: https://scholar.colorado.edu/mcen_gradetds/170.

Council of Science Editors:

Engvall LH. Geometrically Exact and Analysis Suitable Mesh Generation Using Rational Bernstein–Bezier Elements. [Doctoral Dissertation]. University of Colorado; 2018. Available from: https://scholar.colorado.edu/mcen_gradetds/170


University of Colorado

10. Coley, Christopher Joel. Residual-Based Large Eddy Simulation of Turbulent Flows Using Divergence-Conforming Discretizations.

Degree: PhD, 2017, University of Colorado

  In this dissertation, a class of methods which combines divergence-conforming discretizations with residual-based subgrid modeling for large eddy simulation of turbulent flows is introduced.… (more)

Subjects/Keywords: divergence-conforming; large eddy simulation; residual-based large eddy simulation; structure-preserving; turbulence modeling; variational multiscale method; Aerospace Engineering; Applied Mathematics

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

APA (6th Edition):

Coley, C. J. (2017). Residual-Based Large Eddy Simulation of Turbulent Flows Using Divergence-Conforming Discretizations. (Doctoral Dissertation). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/220

Chicago Manual of Style (16th Edition):

Coley, Christopher Joel. “Residual-Based Large Eddy Simulation of Turbulent Flows Using Divergence-Conforming Discretizations.” 2017. Doctoral Dissertation, University of Colorado. Accessed November 15, 2019. https://scholar.colorado.edu/asen_gradetds/220.

MLA Handbook (7th Edition):

Coley, Christopher Joel. “Residual-Based Large Eddy Simulation of Turbulent Flows Using Divergence-Conforming Discretizations.” 2017. Web. 15 Nov 2019.

Vancouver:

Coley CJ. Residual-Based Large Eddy Simulation of Turbulent Flows Using Divergence-Conforming Discretizations. [Internet] [Doctoral dissertation]. University of Colorado; 2017. [cited 2019 Nov 15]. Available from: https://scholar.colorado.edu/asen_gradetds/220.

Council of Science Editors:

Coley CJ. Residual-Based Large Eddy Simulation of Turbulent Flows Using Divergence-Conforming Discretizations. [Doctoral Dissertation]. University of Colorado; 2017. Available from: https://scholar.colorado.edu/asen_gradetds/220

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