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You searched for subject:(Hypersonic Vehicle). Showing records 1 – 19 of 19 total matches.

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Texas A&M University

1. Famularo, Douglas I. Observer-Based Nonlinear Dynamic Inversion Adaptive Control with State Constraints.

Degree: PhD, Aerospace Engineering, 2017, Texas A&M University

Hypersonic vehicle research and development has grown recently in the aerospace industry due to the powerful potential of operating a vehicle that flies at substantially… (more)

Subjects/Keywords: Adaptive Control; Nonlinear Dynamic Inversion; Nonlinear Hypersonic Vehicle Control; State Constraints

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APA (6th Edition):

Famularo, D. I. (2017). Observer-Based Nonlinear Dynamic Inversion Adaptive Control with State Constraints. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/169595

Chicago Manual of Style (16th Edition):

Famularo, Douglas I. “Observer-Based Nonlinear Dynamic Inversion Adaptive Control with State Constraints.” 2017. Doctoral Dissertation, Texas A&M University. Accessed December 14, 2019. http://hdl.handle.net/1969.1/169595.

MLA Handbook (7th Edition):

Famularo, Douglas I. “Observer-Based Nonlinear Dynamic Inversion Adaptive Control with State Constraints.” 2017. Web. 14 Dec 2019.

Vancouver:

Famularo DI. Observer-Based Nonlinear Dynamic Inversion Adaptive Control with State Constraints. [Internet] [Doctoral dissertation]. Texas A&M University; 2017. [cited 2019 Dec 14]. Available from: http://hdl.handle.net/1969.1/169595.

Council of Science Editors:

Famularo DI. Observer-Based Nonlinear Dynamic Inversion Adaptive Control with State Constraints. [Doctoral Dissertation]. Texas A&M University; 2017. Available from: http://hdl.handle.net/1969.1/169595


University of Dayton

2. Alsuwian, Turki Mohammed. Comparative Analysis of Flight Control Designs for Hypersonic Vehicles at Subsonic Speeds.

Degree: PhD, Electrical Engineering, 2018, University of Dayton

Hypersonic vehicles are complex nonlinear systems with uncertain dynamics. Multiple designs of control systems for hypersonic vehicles based on nonlinear dynamic models have been applied… (more)

Subjects/Keywords: Aerospace Engineering; Electrical Engineering; Hypersonic Vehicle; Adaptive Control; Flight Control; Subsonic Speed; Control Design

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APA (6th Edition):

Alsuwian, T. M. (2018). Comparative Analysis of Flight Control Designs for Hypersonic Vehicles at Subsonic Speeds. (Doctoral Dissertation). University of Dayton. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=dayton1543828056218447

Chicago Manual of Style (16th Edition):

Alsuwian, Turki Mohammed. “Comparative Analysis of Flight Control Designs for Hypersonic Vehicles at Subsonic Speeds.” 2018. Doctoral Dissertation, University of Dayton. Accessed December 14, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=dayton1543828056218447.

MLA Handbook (7th Edition):

Alsuwian, Turki Mohammed. “Comparative Analysis of Flight Control Designs for Hypersonic Vehicles at Subsonic Speeds.” 2018. Web. 14 Dec 2019.

Vancouver:

Alsuwian TM. Comparative Analysis of Flight Control Designs for Hypersonic Vehicles at Subsonic Speeds. [Internet] [Doctoral dissertation]. University of Dayton; 2018. [cited 2019 Dec 14]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=dayton1543828056218447.

Council of Science Editors:

Alsuwian TM. Comparative Analysis of Flight Control Designs for Hypersonic Vehicles at Subsonic Speeds. [Doctoral Dissertation]. University of Dayton; 2018. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=dayton1543828056218447


Arizona State University

3. Khatri, Jaidev. Modeling, Analysis, and Control of a Hypersonic Vehicle with Significant Aero-Thermo-Elastic-Propulsion Interactions: Elastic, Thermal and Mass Uncertainty.

Degree: MS, Electrical Engineering, 2011, Arizona State University

 This thesis examines themodeling, analysis, and control system design issues for scramjet powered hypersonic vehicles. A nonlinear three degrees of freedom longitudinal model which includes… (more)

Subjects/Keywords: Electrical Engineering; Aerospace Engineering; Mechanical Engineering; Aero-Thermo-Elastic; Control design; Hypersonic Vehicle

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APA (6th Edition):

Khatri, J. (2011). Modeling, Analysis, and Control of a Hypersonic Vehicle with Significant Aero-Thermo-Elastic-Propulsion Interactions: Elastic, Thermal and Mass Uncertainty. (Masters Thesis). Arizona State University. Retrieved from http://repository.asu.edu/items/8873

Chicago Manual of Style (16th Edition):

Khatri, Jaidev. “Modeling, Analysis, and Control of a Hypersonic Vehicle with Significant Aero-Thermo-Elastic-Propulsion Interactions: Elastic, Thermal and Mass Uncertainty.” 2011. Masters Thesis, Arizona State University. Accessed December 14, 2019. http://repository.asu.edu/items/8873.

MLA Handbook (7th Edition):

Khatri, Jaidev. “Modeling, Analysis, and Control of a Hypersonic Vehicle with Significant Aero-Thermo-Elastic-Propulsion Interactions: Elastic, Thermal and Mass Uncertainty.” 2011. Web. 14 Dec 2019.

Vancouver:

Khatri J. Modeling, Analysis, and Control of a Hypersonic Vehicle with Significant Aero-Thermo-Elastic-Propulsion Interactions: Elastic, Thermal and Mass Uncertainty. [Internet] [Masters thesis]. Arizona State University; 2011. [cited 2019 Dec 14]. Available from: http://repository.asu.edu/items/8873.

Council of Science Editors:

Khatri J. Modeling, Analysis, and Control of a Hypersonic Vehicle with Significant Aero-Thermo-Elastic-Propulsion Interactions: Elastic, Thermal and Mass Uncertainty. [Masters Thesis]. Arizona State University; 2011. Available from: http://repository.asu.edu/items/8873


Georgia Tech

4. Dykes, John William. TEMPUS: A methodology for model-based robust-optimal design of time-dynamic system identification experiments using variational asymptotic expansions.

Degree: PhD, Aerospace Engineering, 2016, Georgia Tech

 The development of appropriate flight tests has proven to be a critical element in the development process of many revolutionary next-generation aerospace vehicles. For example,… (more)

Subjects/Keywords: Variational asymptotic expansions; System identification; Information experiments; Robust-optimal dynamic experiment design; Model-based; Hypersonic flight testing; SCRAMjet; Generic hypersonic vehicle model

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APA (6th Edition):

Dykes, J. W. (2016). TEMPUS: A methodology for model-based robust-optimal design of time-dynamic system identification experiments using variational asymptotic expansions. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/59120

Chicago Manual of Style (16th Edition):

Dykes, John William. “TEMPUS: A methodology for model-based robust-optimal design of time-dynamic system identification experiments using variational asymptotic expansions.” 2016. Doctoral Dissertation, Georgia Tech. Accessed December 14, 2019. http://hdl.handle.net/1853/59120.

MLA Handbook (7th Edition):

Dykes, John William. “TEMPUS: A methodology for model-based robust-optimal design of time-dynamic system identification experiments using variational asymptotic expansions.” 2016. Web. 14 Dec 2019.

Vancouver:

Dykes JW. TEMPUS: A methodology for model-based robust-optimal design of time-dynamic system identification experiments using variational asymptotic expansions. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2019 Dec 14]. Available from: http://hdl.handle.net/1853/59120.

Council of Science Editors:

Dykes JW. TEMPUS: A methodology for model-based robust-optimal design of time-dynamic system identification experiments using variational asymptotic expansions. [Doctoral Dissertation]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/59120


University of Florida

5. Wilcox, Zachary. Nonlinear Control of Linear Parameter Varying Systems with Applications to Hypersonic Vehicles.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2010, University of Florida

 The focus of this dissertation is to design a controller for linear parameter varying (LPV) systems, apply it specifically to air-breathing hypersonic vehicles, and examine… (more)

Subjects/Keywords: Cost functions; Design analysis; Dynamic modeling; Hypersonic aircraft; Matrices; Modeling; Parametric models; Simulations; Temperature profiles; Velocity; aerospace, aircraft, controls, hypersonic, linear, lpv, nonlinear, parameter, robust, varying, vehicle

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APA (6th Edition):

Wilcox, Z. (2010). Nonlinear Control of Linear Parameter Varying Systems with Applications to Hypersonic Vehicles. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0041960

Chicago Manual of Style (16th Edition):

Wilcox, Zachary. “Nonlinear Control of Linear Parameter Varying Systems with Applications to Hypersonic Vehicles.” 2010. Doctoral Dissertation, University of Florida. Accessed December 14, 2019. http://ufdc.ufl.edu/UFE0041960.

MLA Handbook (7th Edition):

Wilcox, Zachary. “Nonlinear Control of Linear Parameter Varying Systems with Applications to Hypersonic Vehicles.” 2010. Web. 14 Dec 2019.

Vancouver:

Wilcox Z. Nonlinear Control of Linear Parameter Varying Systems with Applications to Hypersonic Vehicles. [Internet] [Doctoral dissertation]. University of Florida; 2010. [cited 2019 Dec 14]. Available from: http://ufdc.ufl.edu/UFE0041960.

Council of Science Editors:

Wilcox Z. Nonlinear Control of Linear Parameter Varying Systems with Applications to Hypersonic Vehicles. [Doctoral Dissertation]. University of Florida; 2010. Available from: http://ufdc.ufl.edu/UFE0041960


University of Cincinnati

6. Vick, Tyler J. Geometry Modeling and Adaptive Control of Air-Breathing Hypersonic Vehicles.

Degree: MS, Engineering and Applied Science: Aerospace Engineering, 2014, University of Cincinnati

 Air-breathing hypersonic vehicles have the potential to provide global reach and affordable access to space. Recent technological advancements have made scramjet-powered flight achievable, as evidenced… (more)

Subjects/Keywords: Aerospace Materials; Hypersonic Vehicle; Adaptive Control; Geometry Modeling; Modeling and Simulation; Model Reference; Linear Quadratic Regulator

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APA (6th Edition):

Vick, T. J. (2014). Geometry Modeling and Adaptive Control of Air-Breathing Hypersonic Vehicles. (Masters Thesis). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin1397468045

Chicago Manual of Style (16th Edition):

Vick, Tyler J. “Geometry Modeling and Adaptive Control of Air-Breathing Hypersonic Vehicles.” 2014. Masters Thesis, University of Cincinnati. Accessed December 14, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1397468045.

MLA Handbook (7th Edition):

Vick, Tyler J. “Geometry Modeling and Adaptive Control of Air-Breathing Hypersonic Vehicles.” 2014. Web. 14 Dec 2019.

Vancouver:

Vick TJ. Geometry Modeling and Adaptive Control of Air-Breathing Hypersonic Vehicles. [Internet] [Masters thesis]. University of Cincinnati; 2014. [cited 2019 Dec 14]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1397468045.

Council of Science Editors:

Vick TJ. Geometry Modeling and Adaptive Control of Air-Breathing Hypersonic Vehicles. [Masters Thesis]. University of Cincinnati; 2014. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin1397468045

7. 山下, 礼. 全空間シミュレーションによる極超音速飛行体のソニックブーム解析(要旨).

Degree: 修士(科学), 2017, The University of Tokyo / 東京大学

Subjects/Keywords: Sonic Boom; Hypersonic Vehicle; CFD; Shock Wave

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APA (6th Edition):

山下, . (2017). 全空間シミュレーションによる極超音速飛行体のソニックブーム解析(要旨). (Thesis). The University of Tokyo / 東京大学. Retrieved from http://hdl.handle.net/2261/48849

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):

山下, 礼. “全空間シミュレーションによる極超音速飛行体のソニックブーム解析(要旨).” 2017. Thesis, The University of Tokyo / 東京大学. Accessed December 14, 2019. http://hdl.handle.net/2261/48849.

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

MLA Handbook (7th Edition):

山下, 礼. “全空間シミュレーションによる極超音速飛行体のソニックブーム解析(要旨).” 2017. Web. 14 Dec 2019.

Vancouver:

山下 . 全空間シミュレーションによる極超音速飛行体のソニックブーム解析(要旨). [Internet] [Thesis]. The University of Tokyo / 東京大学; 2017. [cited 2019 Dec 14]. Available from: http://hdl.handle.net/2261/48849.

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

Council of Science Editors:

山下 . 全空間シミュレーションによる極超音速飛行体のソニックブーム解析(要旨). [Thesis]. The University of Tokyo / 東京大学; 2017. Available from: http://hdl.handle.net/2261/48849

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

8. Terhes, C. Preliminary Structural Design for a Hypersonic UAV:.

Degree: 2014, Delft University of Technology

 The design and development of a small unmanned aerial vehicle is proposed in order to provide more accurate hypersonic flight data. The outcomes could improve… (more)

Subjects/Keywords: structural design; hypersonic vehicle; FEM; FEA

…will take place and the vehicle will reach the desired hypersonic speed of 2 km/s… …x5D; A. Eggers C.Terhes 1.3. THE GRADUATION PROJECT Cleary a hypersonic vehicle has… …Hypersonic vehicle performance depends on several factors such as structural concepts, material… …x5B;4]. Focusing of structural challenge of the hypersonic vehicle, the mechanics of… …PROPOSED ATTACHMENT AFT OF THE VEHICLE 54 FIGURE 29: AXIAL EXPANSION JOINT WELDING IN ©SPIROFLEX… 

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APA (6th Edition):

Terhes, C. (2014). Preliminary Structural Design for a Hypersonic UAV:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:802993a5-b218-4b7f-a7b4-9cf5375f7b38

Chicago Manual of Style (16th Edition):

Terhes, C. “Preliminary Structural Design for a Hypersonic UAV:.” 2014. Masters Thesis, Delft University of Technology. Accessed December 14, 2019. http://resolver.tudelft.nl/uuid:802993a5-b218-4b7f-a7b4-9cf5375f7b38.

MLA Handbook (7th Edition):

Terhes, C. “Preliminary Structural Design for a Hypersonic UAV:.” 2014. Web. 14 Dec 2019.

Vancouver:

Terhes C. Preliminary Structural Design for a Hypersonic UAV:. [Internet] [Masters thesis]. Delft University of Technology; 2014. [cited 2019 Dec 14]. Available from: http://resolver.tudelft.nl/uuid:802993a5-b218-4b7f-a7b4-9cf5375f7b38.

Council of Science Editors:

Terhes C. Preliminary Structural Design for a Hypersonic UAV:. [Masters Thesis]. Delft University of Technology; 2014. Available from: http://resolver.tudelft.nl/uuid:802993a5-b218-4b7f-a7b4-9cf5375f7b38


University of Michigan

9. Marley, Christopher. Thermal Management in a Scramjet-Powered Hypersonic Cruise Vehicle.

Degree: PhD, Aerospace Engineering, 2018, University of Michigan

 Due to the large aerodynamic heating at high Mach numbers, Thermal Protection System (TPS) design considerations are critical for hypersonic vehicles, and engineers seek to… (more)

Subjects/Keywords: Hypersonic Cruise Vehicle; Active Thermal Protection System (TPS); Passive Thermal Protection System (TPS); Scramjet; Aerospace Engineering; Engineering

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APA (6th Edition):

Marley, C. (2018). Thermal Management in a Scramjet-Powered Hypersonic Cruise Vehicle. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/144038

Chicago Manual of Style (16th Edition):

Marley, Christopher. “Thermal Management in a Scramjet-Powered Hypersonic Cruise Vehicle.” 2018. Doctoral Dissertation, University of Michigan. Accessed December 14, 2019. http://hdl.handle.net/2027.42/144038.

MLA Handbook (7th Edition):

Marley, Christopher. “Thermal Management in a Scramjet-Powered Hypersonic Cruise Vehicle.” 2018. Web. 14 Dec 2019.

Vancouver:

Marley C. Thermal Management in a Scramjet-Powered Hypersonic Cruise Vehicle. [Internet] [Doctoral dissertation]. University of Michigan; 2018. [cited 2019 Dec 14]. Available from: http://hdl.handle.net/2027.42/144038.

Council of Science Editors:

Marley C. Thermal Management in a Scramjet-Powered Hypersonic Cruise Vehicle. [Doctoral Dissertation]. University of Michigan; 2018. Available from: http://hdl.handle.net/2027.42/144038


Indian Institute of Science

10. Trikha, Manish. Dynamics And Stability Of A Launch Vehicle.

Degree: 2010, Indian Institute of Science

 Stability is an important criterion in the design and performance of launch vehicles. Present day launch vehicles have become more and more flexible due to… (more)

Subjects/Keywords: Launch Vehicles (Astronautics); Launch Vehicles - Mathematical Models; Launch Vehicle Stability; Launch Vehicle Dynamics; Aerodynamics; Launch Vehicle Design; Launch Vehicle Loads; Launch Vehicles - Propulsion; Propulsive Thrust; Aerodynamic Forces; Slender Aerospace Vehicles; Slender Hypersonic Vehicles; Space Launch Vehicles; Astronautics

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APA (6th Edition):

Trikha, M. (2010). Dynamics And Stability Of A Launch Vehicle. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/1269

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):

Trikha, Manish. “Dynamics And Stability Of A Launch Vehicle.” 2010. Thesis, Indian Institute of Science. Accessed December 14, 2019. http://hdl.handle.net/2005/1269.

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

MLA Handbook (7th Edition):

Trikha, Manish. “Dynamics And Stability Of A Launch Vehicle.” 2010. Web. 14 Dec 2019.

Vancouver:

Trikha M. Dynamics And Stability Of A Launch Vehicle. [Internet] [Thesis]. Indian Institute of Science; 2010. [cited 2019 Dec 14]. Available from: http://hdl.handle.net/2005/1269.

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

Council of Science Editors:

Trikha M. Dynamics And Stability Of A Launch Vehicle. [Thesis]. Indian Institute of Science; 2010. Available from: http://hdl.handle.net/2005/1269

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


Indian Institute of Science

11. Trikha, Manish. Dynamics And Stability Of A Launch Vehicle.

Degree: 2010, Indian Institute of Science

 Stability is an important criterion in the design and performance of launch vehicles. Present day launch vehicles have become more and more flexible due to… (more)

Subjects/Keywords: Launch Vehicles (Astronautics); Launch Vehicles - Mathematical Models; Launch Vehicle Stability; Launch Vehicle Dynamics; Aerodynamics; Launch Vehicle Design; Launch Vehicle Loads; Launch Vehicles - Propulsion; Propulsive Thrust; Aerodynamic Forces; Slender Aerospace Vehicles; Slender Hypersonic Vehicles; Space Launch Vehicles; Astronautics

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APA (6th Edition):

Trikha, M. (2010). Dynamics And Stability Of A Launch Vehicle. (Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ernet.in/handle/2005/1269 ; http://etd.ncsi.iisc.ernet.in/abstracts/1650/G23817-Abs.pdf

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):

Trikha, Manish. “Dynamics And Stability Of A Launch Vehicle.” 2010. Thesis, Indian Institute of Science. Accessed December 14, 2019. http://etd.iisc.ernet.in/handle/2005/1269 ; http://etd.ncsi.iisc.ernet.in/abstracts/1650/G23817-Abs.pdf.

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

MLA Handbook (7th Edition):

Trikha, Manish. “Dynamics And Stability Of A Launch Vehicle.” 2010. Web. 14 Dec 2019.

Vancouver:

Trikha M. Dynamics And Stability Of A Launch Vehicle. [Internet] [Thesis]. Indian Institute of Science; 2010. [cited 2019 Dec 14]. Available from: http://etd.iisc.ernet.in/handle/2005/1269 ; http://etd.ncsi.iisc.ernet.in/abstracts/1650/G23817-Abs.pdf.

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

Council of Science Editors:

Trikha M. Dynamics And Stability Of A Launch Vehicle. [Thesis]. Indian Institute of Science; 2010. Available from: http://etd.iisc.ernet.in/handle/2005/1269 ; http://etd.ncsi.iisc.ernet.in/abstracts/1650/G23817-Abs.pdf

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

12. Paulo Henrique Mineiro Leite. Simulação direta molecular da influência de degraus na superfície de veículos na reentrada.

Degree: 2009, Instituto Nacional de Pesquisas Espaciais

In the design of a hypersonic vehicle, the knowledge of the factors that affect the thermal and aerodynamic loads acting on the vehicle surface becomes… (more)

Subjects/Keywords: Simulação direta de Monte Carlo; escoamento hipersônico; escoamento rarefeito; influência de degraus; veículo de reentrada; direct simulation Monte Carlo; hypersonic flow; rarefied flow; steps influence; reentry vehicle

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APA (6th Edition):

Leite, P. H. M. (2009). Simulação direta molecular da influência de degraus na superfície de veículos na reentrada. (Thesis). Instituto Nacional de Pesquisas Espaciais. Retrieved from http://urlib.net/sid.inpe.br/[email protected]/2009/08.27.17.55

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):

Leite, Paulo Henrique Mineiro. “Simulação direta molecular da influência de degraus na superfície de veículos na reentrada.” 2009. Thesis, Instituto Nacional de Pesquisas Espaciais. Accessed December 14, 2019. http://urlib.net/sid.inpe.br/[email protected]/2009/08.27.17.55.

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

MLA Handbook (7th Edition):

Leite, Paulo Henrique Mineiro. “Simulação direta molecular da influência de degraus na superfície de veículos na reentrada.” 2009. Web. 14 Dec 2019.

Vancouver:

Leite PHM. Simulação direta molecular da influência de degraus na superfície de veículos na reentrada. [Internet] [Thesis]. Instituto Nacional de Pesquisas Espaciais; 2009. [cited 2019 Dec 14]. Available from: http://urlib.net/sid.inpe.br/[email protected]/2009/08.27.17.55.

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

Council of Science Editors:

Leite PHM. Simulação direta molecular da influência de degraus na superfície de veículos na reentrada. [Thesis]. Instituto Nacional de Pesquisas Espaciais; 2009. Available from: http://urlib.net/sid.inpe.br/[email protected]/2009/08.27.17.55

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

13. Luis Thiago Lucci Correa Paolicchi. Computational analysis of gap effects on the surface of reentry space vehicle.

Degree: 2010, Instituto Nacional de Pesquisas Espaciais

Uma investigação computacional foi realizada com o objetivo de examinar o impacto de descontinuidades na estrutura do escoamento e propriedades aerodinâmicas na superfície de veículos… (more)

Subjects/Keywords: simulação direta Monte Carlo; escoamento hipersônico; escoamento rarefeito; escoamento em filetes; veículos reentrantes; direct simulation Monte Carlo; hypersonic flow; rarefied flow; gap flow; reentry vehicle

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APA (6th Edition):

Paolicchi, L. T. L. C. (2010). Computational analysis of gap effects on the surface of reentry space vehicle. (Thesis). Instituto Nacional de Pesquisas Espaciais. Retrieved from http://urlib.net/sid.inpe.br/mtc-m19/2011/01.31.17.46

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):

Paolicchi, Luis Thiago Lucci Correa. “Computational analysis of gap effects on the surface of reentry space vehicle.” 2010. Thesis, Instituto Nacional de Pesquisas Espaciais. Accessed December 14, 2019. http://urlib.net/sid.inpe.br/mtc-m19/2011/01.31.17.46.

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

MLA Handbook (7th Edition):

Paolicchi, Luis Thiago Lucci Correa. “Computational analysis of gap effects on the surface of reentry space vehicle.” 2010. Web. 14 Dec 2019.

Vancouver:

Paolicchi LTLC. Computational analysis of gap effects on the surface of reentry space vehicle. [Internet] [Thesis]. Instituto Nacional de Pesquisas Espaciais; 2010. [cited 2019 Dec 14]. Available from: http://urlib.net/sid.inpe.br/mtc-m19/2011/01.31.17.46.

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

Council of Science Editors:

Paolicchi LTLC. Computational analysis of gap effects on the surface of reentry space vehicle. [Thesis]. Instituto Nacional de Pesquisas Espaciais; 2010. Available from: http://urlib.net/sid.inpe.br/mtc-m19/2011/01.31.17.46

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


Indian Institute of Science

14. Maity, Arnab. Optimal Guidance Of Aerospace Vehicles Using Generalized MPSP With Advanced Control Of Supersonic Air-Breathing Engines.

Degree: 2012, Indian Institute of Science

 A new suboptimal guidance law design approach for aerospace vehicles is proposed in this thesis, followed by an advanced control design for supersonic air-breathing engines.… (more)

Subjects/Keywords: Aerospace Vehicles; Aerospace Vehicles - Guidance and Control; Air-Breathing Engines - Control; Generalized Model Predictive Static Programming (G-MPSP); Supersonic Air-Breathing Engines; Launch Vehicles (Astronautics); Solid Motor Propelled Carrier Launch Vehicle; Air-Breathing Vehicles - Guidance; Kalman Filtering; Flight Trajectory; Supersonic Air-Breathing Vehicles - Guidance; Supersonic Air-Breathing Vehicle; Hypersonic Mission; Extended Kalman Filter (EKF); Optimal Control Theory; Astronautics

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

APA (6th Edition):

Maity, A. (2012). Optimal Guidance Of Aerospace Vehicles Using Generalized MPSP With Advanced Control Of Supersonic Air-Breathing Engines. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/2550

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):

Maity, Arnab. “Optimal Guidance Of Aerospace Vehicles Using Generalized MPSP With Advanced Control Of Supersonic Air-Breathing Engines.” 2012. Thesis, Indian Institute of Science. Accessed December 14, 2019. http://hdl.handle.net/2005/2550.

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

MLA Handbook (7th Edition):

Maity, Arnab. “Optimal Guidance Of Aerospace Vehicles Using Generalized MPSP With Advanced Control Of Supersonic Air-Breathing Engines.” 2012. Web. 14 Dec 2019.

Vancouver:

Maity A. Optimal Guidance Of Aerospace Vehicles Using Generalized MPSP With Advanced Control Of Supersonic Air-Breathing Engines. [Internet] [Thesis]. Indian Institute of Science; 2012. [cited 2019 Dec 14]. Available from: http://hdl.handle.net/2005/2550.

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

Council of Science Editors:

Maity A. Optimal Guidance Of Aerospace Vehicles Using Generalized MPSP With Advanced Control Of Supersonic Air-Breathing Engines. [Thesis]. Indian Institute of Science; 2012. Available from: http://hdl.handle.net/2005/2550

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


Indian Institute of Science

15. Maity, Arnab. Optimal Guidance Of Aerospace Vehicles Using Generalized MPSP With Advanced Control Of Supersonic Air-Breathing Engines.

Degree: 2012, Indian Institute of Science

 A new suboptimal guidance law design approach for aerospace vehicles is proposed in this thesis, followed by an advanced control design for supersonic air-breathing engines.… (more)

Subjects/Keywords: Aerospace Vehicles; Aerospace Vehicles - Guidance and Control; Air-Breathing Engines - Control; Generalized Model Predictive Static Programming (G-MPSP); Supersonic Air-Breathing Engines; Launch Vehicles (Astronautics); Solid Motor Propelled Carrier Launch Vehicle; Air-Breathing Vehicles - Guidance; Kalman Filtering; Flight Trajectory; Supersonic Air-Breathing Vehicles - Guidance; Supersonic Air-Breathing Vehicle; Hypersonic Mission; Extended Kalman Filter (EKF); Optimal Control Theory; Astronautics

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

APA (6th Edition):

Maity, A. (2012). Optimal Guidance Of Aerospace Vehicles Using Generalized MPSP With Advanced Control Of Supersonic Air-Breathing Engines. (Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ernet.in/handle/2005/2550 ; http://etd.ncsi.iisc.ernet.in/abstracts/3308/G25667-Abs.pdf

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):

Maity, Arnab. “Optimal Guidance Of Aerospace Vehicles Using Generalized MPSP With Advanced Control Of Supersonic Air-Breathing Engines.” 2012. Thesis, Indian Institute of Science. Accessed December 14, 2019. http://etd.iisc.ernet.in/handle/2005/2550 ; http://etd.ncsi.iisc.ernet.in/abstracts/3308/G25667-Abs.pdf.

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

MLA Handbook (7th Edition):

Maity, Arnab. “Optimal Guidance Of Aerospace Vehicles Using Generalized MPSP With Advanced Control Of Supersonic Air-Breathing Engines.” 2012. Web. 14 Dec 2019.

Vancouver:

Maity A. Optimal Guidance Of Aerospace Vehicles Using Generalized MPSP With Advanced Control Of Supersonic Air-Breathing Engines. [Internet] [Thesis]. Indian Institute of Science; 2012. [cited 2019 Dec 14]. Available from: http://etd.iisc.ernet.in/handle/2005/2550 ; http://etd.ncsi.iisc.ernet.in/abstracts/3308/G25667-Abs.pdf.

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

Council of Science Editors:

Maity A. Optimal Guidance Of Aerospace Vehicles Using Generalized MPSP With Advanced Control Of Supersonic Air-Breathing Engines. [Thesis]. Indian Institute of Science; 2012. Available from: http://etd.iisc.ernet.in/handle/2005/2550 ; http://etd.ncsi.iisc.ernet.in/abstracts/3308/G25667-Abs.pdf

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


University of Dayton

16. Tancred, James Anderson. Aerodynamic Database Generation for a Complex Hypersonic Vehicle Configuration Utilizing Variable-Fidelity Kriging.

Degree: MS(M.S.), Aerospace Engineering, 2018, University of Dayton

 This work seeks to provide a proof-of-concept for the use of variable-fidelity (VF) kriging to approximate the lift and drag values for a complex hypersonic(more)

Subjects/Keywords: Aerospace Engineering; Applied Mathematics; aerodynamic database generation; hypersonic; aircraft vehicle design; variable-fidelity kriging; kriging; multi-fidelity kriging; Cart3D; reduced-order modeling; surrogate modeling; function approximation theory; computational fluid dynamics; CFD

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

APA (6th Edition):

Tancred, J. A. (2018). Aerodynamic Database Generation for a Complex Hypersonic Vehicle Configuration Utilizing Variable-Fidelity Kriging. (Masters Thesis). University of Dayton. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=dayton1543801033672049

Chicago Manual of Style (16th Edition):

Tancred, James Anderson. “Aerodynamic Database Generation for a Complex Hypersonic Vehicle Configuration Utilizing Variable-Fidelity Kriging.” 2018. Masters Thesis, University of Dayton. Accessed December 14, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=dayton1543801033672049.

MLA Handbook (7th Edition):

Tancred, James Anderson. “Aerodynamic Database Generation for a Complex Hypersonic Vehicle Configuration Utilizing Variable-Fidelity Kriging.” 2018. Web. 14 Dec 2019.

Vancouver:

Tancred JA. Aerodynamic Database Generation for a Complex Hypersonic Vehicle Configuration Utilizing Variable-Fidelity Kriging. [Internet] [Masters thesis]. University of Dayton; 2018. [cited 2019 Dec 14]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=dayton1543801033672049.

Council of Science Editors:

Tancred JA. Aerodynamic Database Generation for a Complex Hypersonic Vehicle Configuration Utilizing Variable-Fidelity Kriging. [Masters Thesis]. University of Dayton; 2018. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=dayton1543801033672049


University of Queensland

17. Preller, Dawid. Multidisciplinary design and optimisation of a pitch trimmed hypersonic airbreathing accelerating vehicle.

Degree: School of Mechanical and Mining Engineering, 2018, University of Queensland

Subjects/Keywords: Hypersonic; Scramjet; Airbreather; Multidisciplinary optimisation; Space access; Reusable; Small satellite; SPARTAN; Launch vehicle; 0901 Aerospace Engineering

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

APA (6th Edition):

Preller, D. (2018). Multidisciplinary design and optimisation of a pitch trimmed hypersonic airbreathing accelerating vehicle. (Thesis). University of Queensland. Retrieved from http://espace.library.uq.edu.au/view/UQ:725685

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):

Preller, Dawid. “Multidisciplinary design and optimisation of a pitch trimmed hypersonic airbreathing accelerating vehicle.” 2018. Thesis, University of Queensland. Accessed December 14, 2019. http://espace.library.uq.edu.au/view/UQ:725685.

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

MLA Handbook (7th Edition):

Preller, Dawid. “Multidisciplinary design and optimisation of a pitch trimmed hypersonic airbreathing accelerating vehicle.” 2018. Web. 14 Dec 2019.

Vancouver:

Preller D. Multidisciplinary design and optimisation of a pitch trimmed hypersonic airbreathing accelerating vehicle. [Internet] [Thesis]. University of Queensland; 2018. [cited 2019 Dec 14]. Available from: http://espace.library.uq.edu.au/view/UQ:725685.

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

Council of Science Editors:

Preller D. Multidisciplinary design and optimisation of a pitch trimmed hypersonic airbreathing accelerating vehicle. [Thesis]. University of Queensland; 2018. Available from: http://espace.library.uq.edu.au/view/UQ:725685

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


University of Florida

18. Nozaki, Yoshifumi. Reducing Skin Friction and Heat Transfer over a Hypersonic Cruising Vehicle by Mass Injection.

Degree: MS, Aerospace Engineering - Mechanical and Aerospace Engineering, 2007, University of Florida

 Demonstrating technologies for hypersonic aircraft that cruise at speeds greater than Mach 5 is one of the long-term visions of many agencies, like NASA. Reducing… (more)

Subjects/Keywords: Altitude; Boundary layers; Enthalpy; Flight time; Gas temperature; Heat; Heat transfer; Pressure; Skin friction; Stagnation point; aerodynamics, aircraft, cruise, flight, friction, heat, hypersonic, reduction, skin, space, transfer, vehicle

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

APA (6th Edition):

Nozaki, Y. (2007). Reducing Skin Friction and Heat Transfer over a Hypersonic Cruising Vehicle by Mass Injection. (Masters Thesis). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0020862

Chicago Manual of Style (16th Edition):

Nozaki, Yoshifumi. “Reducing Skin Friction and Heat Transfer over a Hypersonic Cruising Vehicle by Mass Injection.” 2007. Masters Thesis, University of Florida. Accessed December 14, 2019. http://ufdc.ufl.edu/UFE0020862.

MLA Handbook (7th Edition):

Nozaki, Yoshifumi. “Reducing Skin Friction and Heat Transfer over a Hypersonic Cruising Vehicle by Mass Injection.” 2007. Web. 14 Dec 2019.

Vancouver:

Nozaki Y. Reducing Skin Friction and Heat Transfer over a Hypersonic Cruising Vehicle by Mass Injection. [Internet] [Masters thesis]. University of Florida; 2007. [cited 2019 Dec 14]. Available from: http://ufdc.ufl.edu/UFE0020862.

Council of Science Editors:

Nozaki Y. Reducing Skin Friction and Heat Transfer over a Hypersonic Cruising Vehicle by Mass Injection. [Masters Thesis]. University of Florida; 2007. Available from: http://ufdc.ufl.edu/UFE0020862

19. Gillman, Eric D. Cathode Spot Injection of Dielectric Particles with Applications for Communications Blackout Plasma Depletion.

Degree: PhD, Nuclear Engineering & Radiological Sciences, 2012, University of Michigan

 Vehicles traveling at hypersonic velocities in the atmosphere are readily enveloped by a dense plasma layer that blocks, reflects, and significantly attenuates radio signals typically… (more)

Subjects/Keywords: Radio Blackout Mitigation; Hypersonic Vehicle Communications; Plasma Discharge; Dusty Plasma; Cathode Spot Arc; Aerospace Engineering; Nuclear Engineering and Radiological Sciences; Physics; Engineering; Science

…plasma. While the application of this research is intended for mitigating hypersonic vehicle… …hypersonic vehicle. This heating leads to ionization of the surrounding air. The plasma layer, with… …the frequency bands common for hypersonic vehicle communications. This phenomenon is a… …technical community as the most critical frequency band for hypersonic vehicle communication.[… …layer long enough for the hypersonic vehicle to transmit essential telemetry and receive… 

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

APA (6th Edition):

Gillman, E. D. (2012). Cathode Spot Injection of Dielectric Particles with Applications for Communications Blackout Plasma Depletion. (Doctoral Dissertation). University of Michigan. Retrieved from http://hdl.handle.net/2027.42/95986

Chicago Manual of Style (16th Edition):

Gillman, Eric D. “Cathode Spot Injection of Dielectric Particles with Applications for Communications Blackout Plasma Depletion.” 2012. Doctoral Dissertation, University of Michigan. Accessed December 14, 2019. http://hdl.handle.net/2027.42/95986.

MLA Handbook (7th Edition):

Gillman, Eric D. “Cathode Spot Injection of Dielectric Particles with Applications for Communications Blackout Plasma Depletion.” 2012. Web. 14 Dec 2019.

Vancouver:

Gillman ED. Cathode Spot Injection of Dielectric Particles with Applications for Communications Blackout Plasma Depletion. [Internet] [Doctoral dissertation]. University of Michigan; 2012. [cited 2019 Dec 14]. Available from: http://hdl.handle.net/2027.42/95986.

Council of Science Editors:

Gillman ED. Cathode Spot Injection of Dielectric Particles with Applications for Communications Blackout Plasma Depletion. [Doctoral Dissertation]. University of Michigan; 2012. Available from: http://hdl.handle.net/2027.42/95986

.