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Subject: Aerospace engineering.

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State University of New York at Buffalo. Mechanical and Aerospace Engineering. degree granting institution.

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University of Kansas. Aerospace Engineering. degree granting institution.

(2)

California State University, Long Beach. Mechanical and Aerospace Engineering. degree granting institution.

(1)

Callender, William Bryan, author.

(1)

Castellini, Paolo. editor.

(1)

Chap, Andrew Mark, author. (orcid)0000-0002-8513-3632

(1)

Chhunchha, Aakash C., author.

(1)

Di Maio, Dario. editor.

(1)

DiGregorio, Nicholas J., author. (orcid)0000-0002-3264-9125

(1)

Dirkx, Dominic. author.

(1)

Hammerton, Jared Robert, author.

(1)

Hong Kong University of Science and Technology (Hong Kong). Mechanical and Aerospace Engineering. degree granting institution.

(1)

Hoskin, Adam, author.

(1)

Iowa State University. Aerospace Engineering. degree granting institution.

(1)

Mao, Yinbo, author.

(1)

Moghadassian, Behnam, author.

(1)

Mooij, Erwin. author.

(1)

North Dakota State University. Mechanical Engineering. degree granting institution.

(1)

Old Dominion University. Mechanical & Aerospace Engineering. degree granting institution.

(1)

Patterson, M. Elijah, author.

(1)

Philippe, Sébastien, author.

(1)

Princeton University. Mechanical and Aerospace Engineering. degree granting institution.

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Rostad, Braden Lee, author.

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Rothstein-Dowden, A., author.

(1)

Sadowski, Nicholas Barrett, author.

(1)

Sheng, Andrew, author.

(1)

Strilchuk, Pedro Martin Mendoza, author.

(1)

Syracuse University. Mechanical and Aerospace Engineering. degree granting institution.

(1)

The University of Alabama. Aerospace Engineering. degree granting institution.

(1)

The University of Alabama. Mechanical Engineering. degree granting institution.

(1)

University of California, Los Angeles. Mechanical Engineering 0330. degree granting institution.

(1)

University of Cincinnati. Engineering : Aerospace Engineering. degree granting institution.

(1)

University of Colorado at Boulder. Aerospace Engineering. degree granting institution.

(1)

University of Maryland, College Park. Aerospace Engineering. degree granting institution.

(1)

University of Surrey (United Kingdom). degree granting institution.

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Vardaman, Nathan James, author.

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Xu, Ke, author.

(1)

Zeng, Chen, author.

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Mechanical engineering.

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Fluid mechanics.

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Aerospace Technology and Astronautics.

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Control engineering.

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Cover image for Computational and experimental study of geometry modifications inside a flow-blurring injector

Computational and experimental study of geometry modifications inside a flow-blurring injector

1.

Computational and experimental study of geometry modifications inside a flow-blurring injector

by

Vardaman, Nathan James, author.

http://gateway.proquest.com/openurl?url_ver=Z39.88-2004&rft_val_fmt=info:ofi/fmt:kev:mtx:dissertation&res_dat=xri:pqm&rft_dat=xri:pqdiss:10752473

Format:

Excerpt:

Computational and experimental study of geometry modifications inside a flow-blurring injector /

Cover image for Studies of Multipoint Optimization of Transonic Stators

Studies of Multipoint Optimization of Transonic Stators

2.

Studies of Multipoint Optimization of Transonic Stators

by

Patterson, M. Elijah, author.

http://gateway.proquest.com/openurl?url_ver=Z39.88-2004&rft_val_fmt=info:ofi/fmt:kev:mtx:dissertation&res_dat=xri:pqm&rft_dat=xri:pqdiss:10827895

Format:

Excerpt:

blade geometry and compared to a design case where the stator blade angle was a part of the design

Cover image for Unsteady Aerodynamics &Turbulent Near-wake Characterization of Static & Rotating Cylinder Systems

Unsteady Aerodynamics &Turbulent Near-wake Characterization of Static & Rotating Cylinder Systems

3.

Unsteady Aerodynamics &Turbulent Near-wake Characterization of Static & Rotating Cylinder Systems

by

Rostad, Braden Lee, author.

http://gateway.proquest.com/openurl?url_ver=Z39.88-2004&rft_val_fmt=info:ofi/fmt:kev:mtx:dissertation&res_dat=xri:pqm&rft_dat=xri:pqdiss:10790738

Format:

Excerpt:

been the topic of a significant portion of this research due to its simple geometry and its ability to

Cover image for Body Force Modeling for Engine Inlet Fan System

Body Force Modeling for Engine Inlet Fan System

4.

Body Force Modeling for Engine Inlet Fan System

by

Mao, Yinbo, author.

http://gateway.proquest.com/openurl?url_ver=Z39.88-2004&rft_val_fmt=info:ofi/fmt:kev:mtx:dissertation&res_dat=xri:pqm&rft_dat=xri:pqdiss:10793030

Format:

Excerpt:

geometry. Instead, fan performance data is fed into the body force model, and the resulting body force

Cover image for Aerodynamic Heating Analysis of Re-entry Space Capsule Using Computational Fluid Dynamics

Aerodynamic Heating Analysis of Re-entry Space Capsule Using Computational Fluid Dynamics

5.

Aerodynamic Heating Analysis of Re-entry Space Capsule Using Computational Fluid Dynamics

by

Chhunchha, Aakash C., author.

http://gateway.proquest.com/openurl?url_ver=Z39.88-2004&rft_val_fmt=info:ofi/fmt:kev:mtx:dissertation&res_dat=xri:pqm&rft_dat=xri:pqdiss:10752510

Format:

Excerpt:

50 km. Taking advantage of the symmetry, only a quarter portion of the geometry is considered to

Cover image for Conceptual Shape Optimization of Entry Vehicles Applied to Capsules and Winged Fuselage Vehicles

Conceptual Shape Optimization of Entry Vehicles Applied to Capsules and Winged Fuselage Vehicles

6.

Conceptual Shape Optimization of Entry Vehicles Applied to Capsules and Winged Fuselage Vehicles

by

Dirkx, Dominic. author.

http://dx.doi.org/10.1007/978-3-319-46055-0

Format:

Excerpt:

Interpolation -- Vehicle Geometry -- Optimization -- Simulator Development -- Results - Capsule -- Results

Cover image for Modeling Brittle Fracture under Thermo-mechanical Loading with Discrete Volterra Dislocation Arrays

Modeling Brittle Fracture under Thermo-mechanical Loading with Discrete Volterra Dislocation Arrays

7.

Modeling Brittle Fracture under Thermo-mechanical Loading with Discrete Volterra Dislocation Arrays

by

Sheng, Andrew, author.

http://gateway.proquest.com/openurl?url_ver=Z39.88-2004&rft_val_fmt=info:ofi/fmt:kev:mtx:dissertation&res_dat=xri:pqm&rft_dat=xri:pqdiss:10830460

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Excerpt:

superposition procedure. The elastic field of a crack in a finite geometry is separated into two parts: the

Cover image for Isogeometric Analysis of Subsonic Aerodynamic Flows with Application to Shape Optimization

Isogeometric Analysis of Subsonic Aerodynamic Flows with Application to Shape Optimization

8.

Isogeometric Analysis of Subsonic Aerodynamic Flows with Application to Shape Optimization

by

Rothstein-Dowden, A., author.

http://gateway.proquest.com/openurl?url_ver=Z39.88-2004&rft_val_fmt=info:ofi/fmt:kev:mtx:dissertation&res_dat=xri:pqm&rft_dat=xri:pqdiss:10809473

Format:

Excerpt:

-sonic flow as a tool for early stage aircraft design. The geometry of the airfoil is left arbitrary and the

Cover image for Blossoming of Coiled Deployable Booms

Blossoming of Coiled Deployable Booms

9.

Blossoming of Coiled Deployable Booms

by

Hoskin, Adam, author.

http://gateway.proquest.com/openurl?url_ver=Z39.88-2004&rft_val_fmt=info:ofi/fmt:kev:mtx:dissertation&res_dat=xri:pqm&rft_dat=xri:pqdiss:10856987

Format:

Excerpt:

spindle torque during blossoming. The effects that the coil geometry and the friction between the layers

Cover image for Rotating Machinery, Hybrid Test Methods, Vibro-Acoustics & Laser Vibrometry, Volume 8 Proceedings of the 35th IMAC, A Conference and Exposition on Structural Dynamics 2017

Rotating Machinery, Hybrid Test Methods, Vibro-Acoustics & Laser Vibrometry, Volume 8 Proceedings of the 35th IMAC, A Conference and Exposition on Structural Dynamics 2017

10.

Rotating Machinery, Hybrid Test Methods, Vibro-Acoustics & Laser Vibrometry, Volume 8 Proceedings of the 35th IMAC, A Conference and Exposition on Structural Dynamics 2017

by

Di Maio, Dario. editor.

http://dx.doi.org/10.1007/978-3-319-54648-3

Format:

Excerpt:

Validation Using 3D SLDV, Geometry Scanning and FEM of a Multi-Purpose Drone Propeller Blade -- Chapter 3

Cover image for A Cost Effective Design for a Propeller Thrust/Torque Balance

A Cost Effective Design for a Propeller Thrust/Torque Balance

11.

A Cost Effective Design for a Propeller Thrust/Torque Balance

by

Sadowski, Nicholas Barrett, author.

http://gateway.proquest.com/openurl?url_ver=Z39.88-2004&rft_val_fmt=info:ofi/fmt:kev:mtx:dissertation&res_dat=xri:pqm&rft_dat=xri:pqdiss:10791852

Format:

Excerpt:

Design considerations include constraints on geometry shape/size, thermal compensation, vibration

Cover image for Optimum Wing Shaping and Gust Load Alleviation of Highly Flexible Aircraft with Finite Actuations

Optimum Wing Shaping and Gust Load Alleviation of Highly Flexible Aircraft with Finite Actuations

12.

Optimum Wing Shaping and Gust Load Alleviation of Highly Flexible Aircraft with Finite Actuations

by

Hammerton, Jared Robert, author.

http://gateway.proquest.com/openurl?url_ver=Z39.88-2004&rft_val_fmt=info:ofi/fmt:kev:mtx:dissertation&res_dat=xri:pqm&rft_dat=xri:pqdiss:10747706

Format:

Excerpt:

determining this is to utilize an aeroelastic optimization process to define the wing geometry.

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