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You searched for subject:(Transonic). Showing records 1 – 30 of 190 total matches.

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1. Gray, Cody D. Design and development of a continuous, open-return transonic wind tunnel facility.

Degree: MS, Aerospace Engineering, 2017, University of Illinois – Urbana-Champaign

 A new transonic wind tunnel facility was designed and built on the University of Illinois at Urbana-Champaign campus to enhance testing capabilities of the transonic(more)

Subjects/Keywords: Transonic

…103 ix List of Tables Table 1.1 Comparison of new transonic wind tunnel and existing… …21 Table 3.1 Transonic wind tunnel performance characteristics… …frequency drive xiii Chapter 1 Introduction Transonic wind tunnel testing encompasses the… …in the flow have made it impossible to establish simple transonic theories that can be used… …to reliably predict the aerodynamic flow about a transonic aircraft. The difficulties in… 

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

APA (6th Edition):

Gray, C. D. (2017). Design and development of a continuous, open-return transonic wind tunnel facility. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/97433

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):

Gray, Cody D. “Design and development of a continuous, open-return transonic wind tunnel facility.” 2017. Thesis, University of Illinois – Urbana-Champaign. Accessed January 22, 2021. http://hdl.handle.net/2142/97433.

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

MLA Handbook (7th Edition):

Gray, Cody D. “Design and development of a continuous, open-return transonic wind tunnel facility.” 2017. Web. 22 Jan 2021.

Vancouver:

Gray CD. Design and development of a continuous, open-return transonic wind tunnel facility. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2017. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/2142/97433.

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

Council of Science Editors:

Gray CD. Design and development of a continuous, open-return transonic wind tunnel facility. [Thesis]. University of Illinois – Urbana-Champaign; 2017. Available from: http://hdl.handle.net/2142/97433

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


Virginia Tech

2. Knight, Kyle Cohn Davis. Assessment of RANS Turbulence Models for Strut-Wing Junctions.

Degree: MS, Aerospace Engineering, 2011, Virginia Tech

 Multidisciplinary Design Optimization (MDO) studies show the Strut/Truss Braced Wing (SBW/TBW) concept has the potential to save a significant amount of fuel over conventional designs.… (more)

Subjects/Keywords: Turbulence; Interference; Transonic

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APA (6th Edition):

Knight, K. C. D. (2011). Assessment of RANS Turbulence Models for Strut-Wing Junctions. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/31760

Chicago Manual of Style (16th Edition):

Knight, Kyle Cohn Davis. “Assessment of RANS Turbulence Models for Strut-Wing Junctions.” 2011. Masters Thesis, Virginia Tech. Accessed January 22, 2021. http://hdl.handle.net/10919/31760.

MLA Handbook (7th Edition):

Knight, Kyle Cohn Davis. “Assessment of RANS Turbulence Models for Strut-Wing Junctions.” 2011. Web. 22 Jan 2021.

Vancouver:

Knight KCD. Assessment of RANS Turbulence Models for Strut-Wing Junctions. [Internet] [Masters thesis]. Virginia Tech; 2011. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/10919/31760.

Council of Science Editors:

Knight KCD. Assessment of RANS Turbulence Models for Strut-Wing Junctions. [Masters Thesis]. Virginia Tech; 2011. Available from: http://hdl.handle.net/10919/31760


UCLA

3. Mellquist, Erik Charles. Computational Transonic Flutter Solutions for Cranked Wings by the Direct Eulerian-Lagrangian Method.

Degree: Aerospace Engineering, 2014, UCLA

 In this dissertation, a three-dimensional computational aeroelastic simulation for cranked, highly-swept wings is developed, and solutions are presented for several wing models. The computational model… (more)

Subjects/Keywords: Aerospace engineering; aeroelasticity; flutter; transonic

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APA (6th Edition):

Mellquist, E. C. (2014). Computational Transonic Flutter Solutions for Cranked Wings by the Direct Eulerian-Lagrangian Method. (Thesis). UCLA. Retrieved from http://www.escholarship.org/uc/item/9rk54186

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):

Mellquist, Erik Charles. “Computational Transonic Flutter Solutions for Cranked Wings by the Direct Eulerian-Lagrangian Method.” 2014. Thesis, UCLA. Accessed January 22, 2021. http://www.escholarship.org/uc/item/9rk54186.

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

MLA Handbook (7th Edition):

Mellquist, Erik Charles. “Computational Transonic Flutter Solutions for Cranked Wings by the Direct Eulerian-Lagrangian Method.” 2014. Web. 22 Jan 2021.

Vancouver:

Mellquist EC. Computational Transonic Flutter Solutions for Cranked Wings by the Direct Eulerian-Lagrangian Method. [Internet] [Thesis]. UCLA; 2014. [cited 2021 Jan 22]. Available from: http://www.escholarship.org/uc/item/9rk54186.

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

Council of Science Editors:

Mellquist EC. Computational Transonic Flutter Solutions for Cranked Wings by the Direct Eulerian-Lagrangian Method. [Thesis]. UCLA; 2014. Available from: http://www.escholarship.org/uc/item/9rk54186

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


University of Cambridge

4. Dent, Anthony. Flow in Multistage Transonic Compressors.

Degree: PhD, 2019, University of Cambridge

Transonic compressors are regularly used as part of the compression system in industrial gas turbines because their high operating speeds make them capable of producing… (more)

Subjects/Keywords: Multistage; Transonic; Compressors; CFD

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APA (6th Edition):

Dent, A. (2019). Flow in Multistage Transonic Compressors. (Doctoral Dissertation). University of Cambridge. Retrieved from https://www.repository.cam.ac.uk/handle/1810/292441

Chicago Manual of Style (16th Edition):

Dent, Anthony. “Flow in Multistage Transonic Compressors.” 2019. Doctoral Dissertation, University of Cambridge. Accessed January 22, 2021. https://www.repository.cam.ac.uk/handle/1810/292441.

MLA Handbook (7th Edition):

Dent, Anthony. “Flow in Multistage Transonic Compressors.” 2019. Web. 22 Jan 2021.

Vancouver:

Dent A. Flow in Multistage Transonic Compressors. [Internet] [Doctoral dissertation]. University of Cambridge; 2019. [cited 2021 Jan 22]. Available from: https://www.repository.cam.ac.uk/handle/1810/292441.

Council of Science Editors:

Dent A. Flow in Multistage Transonic Compressors. [Doctoral Dissertation]. University of Cambridge; 2019. Available from: https://www.repository.cam.ac.uk/handle/1810/292441


Washington University in St. Louis

5. Du, Pan. Numerical Drag Prediction of NASA Common Research Models Using Different Turbulence Models.

Degree: ME, Mechanical Engineering & Materials Science, 2017, Washington University in St. Louis

  The goal of this research is to perform 3D turbulence flow simulations to predict the drag of Wing-body-tail (WBT) and Wing-body-nacelle-Pylon (WBNP) aircraft configurations… (more)

Subjects/Keywords: Numerical; CFD; Drag; Transonic; Engineering

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APA (6th Edition):

Du, P. (2017). Numerical Drag Prediction of NASA Common Research Models Using Different Turbulence Models. (Thesis). Washington University in St. Louis. Retrieved from https://openscholarship.wustl.edu/eng_etds/262

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):

Du, Pan. “Numerical Drag Prediction of NASA Common Research Models Using Different Turbulence Models.” 2017. Thesis, Washington University in St. Louis. Accessed January 22, 2021. https://openscholarship.wustl.edu/eng_etds/262.

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

MLA Handbook (7th Edition):

Du, Pan. “Numerical Drag Prediction of NASA Common Research Models Using Different Turbulence Models.” 2017. Web. 22 Jan 2021.

Vancouver:

Du P. Numerical Drag Prediction of NASA Common Research Models Using Different Turbulence Models. [Internet] [Thesis]. Washington University in St. Louis; 2017. [cited 2021 Jan 22]. Available from: https://openscholarship.wustl.edu/eng_etds/262.

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

Council of Science Editors:

Du P. Numerical Drag Prediction of NASA Common Research Models Using Different Turbulence Models. [Thesis]. Washington University in St. Louis; 2017. Available from: https://openscholarship.wustl.edu/eng_etds/262

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

6. Dent, Anthony. Flow in multistage transonic compressors.

Degree: PhD, 2019, University of Cambridge

Transonic compressors are regularly used as part of the compression system in industrial gas turbines because their high operating speeds make them capable of producing… (more)

Subjects/Keywords: Multistage; Transonic; Compressors; CFD

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APA (6th Edition):

Dent, A. (2019). Flow in multistage transonic compressors. (Doctoral Dissertation). University of Cambridge. Retrieved from https://doi.org/10.17863/CAM.39598 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.774787

Chicago Manual of Style (16th Edition):

Dent, Anthony. “Flow in multistage transonic compressors.” 2019. Doctoral Dissertation, University of Cambridge. Accessed January 22, 2021. https://doi.org/10.17863/CAM.39598 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.774787.

MLA Handbook (7th Edition):

Dent, Anthony. “Flow in multistage transonic compressors.” 2019. Web. 22 Jan 2021.

Vancouver:

Dent A. Flow in multistage transonic compressors. [Internet] [Doctoral dissertation]. University of Cambridge; 2019. [cited 2021 Jan 22]. Available from: https://doi.org/10.17863/CAM.39598 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.774787.

Council of Science Editors:

Dent A. Flow in multistage transonic compressors. [Doctoral Dissertation]. University of Cambridge; 2019. Available from: https://doi.org/10.17863/CAM.39598 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.774787


Delft University of Technology

7. Orlita, M. (author). Cruise Performance Optimization of the Airbus A320 through Flap Morphing.

Degree: 2016, Delft University of Technology

 In the era of increasing aviation traffic the conditions are right to promote design of ambitious concepts. At Fokker Aerostructures attention is drawn to smooth… (more)

Subjects/Keywords: morphing; camber; transonic; drag; optimization; cruise

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APA (6th Edition):

Orlita, M. (. (2016). Cruise Performance Optimization of the Airbus A320 through Flap Morphing. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:92868b2d-87c4-4e0b-9761-698dd54f02f9

Chicago Manual of Style (16th Edition):

Orlita, M (author). “Cruise Performance Optimization of the Airbus A320 through Flap Morphing.” 2016. Masters Thesis, Delft University of Technology. Accessed January 22, 2021. http://resolver.tudelft.nl/uuid:92868b2d-87c4-4e0b-9761-698dd54f02f9.

MLA Handbook (7th Edition):

Orlita, M (author). “Cruise Performance Optimization of the Airbus A320 through Flap Morphing.” 2016. Web. 22 Jan 2021.

Vancouver:

Orlita M(. Cruise Performance Optimization of the Airbus A320 through Flap Morphing. [Internet] [Masters thesis]. Delft University of Technology; 2016. [cited 2021 Jan 22]. Available from: http://resolver.tudelft.nl/uuid:92868b2d-87c4-4e0b-9761-698dd54f02f9.

Council of Science Editors:

Orlita M(. Cruise Performance Optimization of the Airbus A320 through Flap Morphing. [Masters Thesis]. Delft University of Technology; 2016. Available from: http://resolver.tudelft.nl/uuid:92868b2d-87c4-4e0b-9761-698dd54f02f9


Georgia Tech

8. Dansby, Ted. The investigation of two subsonic type airfoils in the transonic region by application of the hydraulic analogy.

Degree: MS, Aeronautical Engineering, 1954, Georgia Tech

Subjects/Keywords: Aerodynamics; Aerofoils; Transonic

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APA (6th Edition):

Dansby, T. (1954). The investigation of two subsonic type airfoils in the transonic region by application of the hydraulic analogy. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/13001

Chicago Manual of Style (16th Edition):

Dansby, Ted. “The investigation of two subsonic type airfoils in the transonic region by application of the hydraulic analogy.” 1954. Masters Thesis, Georgia Tech. Accessed January 22, 2021. http://hdl.handle.net/1853/13001.

MLA Handbook (7th Edition):

Dansby, Ted. “The investigation of two subsonic type airfoils in the transonic region by application of the hydraulic analogy.” 1954. Web. 22 Jan 2021.

Vancouver:

Dansby T. The investigation of two subsonic type airfoils in the transonic region by application of the hydraulic analogy. [Internet] [Masters thesis]. Georgia Tech; 1954. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1853/13001.

Council of Science Editors:

Dansby T. The investigation of two subsonic type airfoils in the transonic region by application of the hydraulic analogy. [Masters Thesis]. Georgia Tech; 1954. Available from: http://hdl.handle.net/1853/13001


Virginia Tech

9. Gillespie, John Lawrie. Aerodynamics of a Transonic Turbine Vane with a 3D Contoured Endwall, Upstream Purge Flow, and a Backward-Facing Step.

Degree: MS, Aerospace Engineering, 2017, Virginia Tech

 This experiment investigated the effects of a non-axisymmetric endwall contour and upstream purge flow on the secondary flow of an inlet guide vane. Three cases… (more)

Subjects/Keywords: Cascade; Transonic; Turbine; Secondary Flow; Contoured Endwall

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APA (6th Edition):

Gillespie, J. L. (2017). Aerodynamics of a Transonic Turbine Vane with a 3D Contoured Endwall, Upstream Purge Flow, and a Backward-Facing Step. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/78683

Chicago Manual of Style (16th Edition):

Gillespie, John Lawrie. “Aerodynamics of a Transonic Turbine Vane with a 3D Contoured Endwall, Upstream Purge Flow, and a Backward-Facing Step.” 2017. Masters Thesis, Virginia Tech. Accessed January 22, 2021. http://hdl.handle.net/10919/78683.

MLA Handbook (7th Edition):

Gillespie, John Lawrie. “Aerodynamics of a Transonic Turbine Vane with a 3D Contoured Endwall, Upstream Purge Flow, and a Backward-Facing Step.” 2017. Web. 22 Jan 2021.

Vancouver:

Gillespie JL. Aerodynamics of a Transonic Turbine Vane with a 3D Contoured Endwall, Upstream Purge Flow, and a Backward-Facing Step. [Internet] [Masters thesis]. Virginia Tech; 2017. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/10919/78683.

Council of Science Editors:

Gillespie JL. Aerodynamics of a Transonic Turbine Vane with a 3D Contoured Endwall, Upstream Purge Flow, and a Backward-Facing Step. [Masters Thesis]. Virginia Tech; 2017. Available from: http://hdl.handle.net/10919/78683


University of Tennessee – Knoxville

10. Schuman, William Calain. A Computational Evaluation of Transonic Wind Tunnel Wall Interference on High Aspect Ratio Models in the Arnold Engineering Development Complex 16 Foot Transonic Tunnel.

Degree: MS, Aerospace Engineering, 2016, University of Tennessee – Knoxville

  One of the inherent difficulties in utilizing a ventilated test section wind tunnel is the interaction of the model flow field and the test… (more)

Subjects/Keywords: Transonic Wind Tunnels; Wall Interference; Transonic Wall Interference; Computational Fluid Dynamics; Aerodynamics and Fluid Mechanics

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APA (6th Edition):

Schuman, W. C. (2016). A Computational Evaluation of Transonic Wind Tunnel Wall Interference on High Aspect Ratio Models in the Arnold Engineering Development Complex 16 Foot Transonic Tunnel. (Thesis). University of Tennessee – Knoxville. Retrieved from https://trace.tennessee.edu/utk_gradthes/3808

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):

Schuman, William Calain. “A Computational Evaluation of Transonic Wind Tunnel Wall Interference on High Aspect Ratio Models in the Arnold Engineering Development Complex 16 Foot Transonic Tunnel.” 2016. Thesis, University of Tennessee – Knoxville. Accessed January 22, 2021. https://trace.tennessee.edu/utk_gradthes/3808.

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

MLA Handbook (7th Edition):

Schuman, William Calain. “A Computational Evaluation of Transonic Wind Tunnel Wall Interference on High Aspect Ratio Models in the Arnold Engineering Development Complex 16 Foot Transonic Tunnel.” 2016. Web. 22 Jan 2021.

Vancouver:

Schuman WC. A Computational Evaluation of Transonic Wind Tunnel Wall Interference on High Aspect Ratio Models in the Arnold Engineering Development Complex 16 Foot Transonic Tunnel. [Internet] [Thesis]. University of Tennessee – Knoxville; 2016. [cited 2021 Jan 22]. Available from: https://trace.tennessee.edu/utk_gradthes/3808.

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

Council of Science Editors:

Schuman WC. A Computational Evaluation of Transonic Wind Tunnel Wall Interference on High Aspect Ratio Models in the Arnold Engineering Development Complex 16 Foot Transonic Tunnel. [Thesis]. University of Tennessee – Knoxville; 2016. Available from: https://trace.tennessee.edu/utk_gradthes/3808

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


University of Miami

11. Coronado Domenge, Patricia X. Delayed-Detached-Eddy Simulation of Shock Wave/TurbulentBoundary Layer Interaction.

Degree: MS, Mechanical Engineering (Engineering), 2009, University of Miami

  The purpose of this thesis is to study the shock/wave turbulent boundary layer interaction by using delayed-detached-eddy simulation (DDES) model with a low diffusion… (more)

Subjects/Keywords: DDES; Boundary Layer Interaction; Transonic Inlet-diffuser; Transonic Channel

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APA (6th Edition):

Coronado Domenge, P. X. (2009). Delayed-Detached-Eddy Simulation of Shock Wave/TurbulentBoundary Layer Interaction. (Thesis). University of Miami. Retrieved from https://scholarlyrepository.miami.edu/oa_theses/220

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):

Coronado Domenge, Patricia X. “Delayed-Detached-Eddy Simulation of Shock Wave/TurbulentBoundary Layer Interaction.” 2009. Thesis, University of Miami. Accessed January 22, 2021. https://scholarlyrepository.miami.edu/oa_theses/220.

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

MLA Handbook (7th Edition):

Coronado Domenge, Patricia X. “Delayed-Detached-Eddy Simulation of Shock Wave/TurbulentBoundary Layer Interaction.” 2009. Web. 22 Jan 2021.

Vancouver:

Coronado Domenge PX. Delayed-Detached-Eddy Simulation of Shock Wave/TurbulentBoundary Layer Interaction. [Internet] [Thesis]. University of Miami; 2009. [cited 2021 Jan 22]. Available from: https://scholarlyrepository.miami.edu/oa_theses/220.

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

Council of Science Editors:

Coronado Domenge PX. Delayed-Detached-Eddy Simulation of Shock Wave/TurbulentBoundary Layer Interaction. [Thesis]. University of Miami; 2009. Available from: https://scholarlyrepository.miami.edu/oa_theses/220

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


KTH

12. Stasolla, Vincenzo. Numerical analysis of aerodynamic damping in a transonic compressor.

Degree: Industrial Engineering and Management (ITM), 2019, KTH

  Aeromechanics is one of the main limitations for more efficient, lighter, cheaper and reliable turbomachines, such as steam or gas turbines, as well as… (more)

Subjects/Keywords: transonic compressor; flutter; vibration; CFD; transonic kompressor; fladder; vibration; CFD; Engineering and Technology; Teknik och teknologier

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APA (6th Edition):

Stasolla, V. (2019). Numerical analysis of aerodynamic damping in a transonic compressor. (Thesis). KTH. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-264359

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):

Stasolla, Vincenzo. “Numerical analysis of aerodynamic damping in a transonic compressor.” 2019. Thesis, KTH. Accessed January 22, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-264359.

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

MLA Handbook (7th Edition):

Stasolla, Vincenzo. “Numerical analysis of aerodynamic damping in a transonic compressor.” 2019. Web. 22 Jan 2021.

Vancouver:

Stasolla V. Numerical analysis of aerodynamic damping in a transonic compressor. [Internet] [Thesis]. KTH; 2019. [cited 2021 Jan 22]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-264359.

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

Council of Science Editors:

Stasolla V. Numerical analysis of aerodynamic damping in a transonic compressor. [Thesis]. KTH; 2019. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-264359

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


UCLA

13. Gariffo, James Michael. Generalized Reduced Order Modeling of Aeroservoelastic Systems.

Degree: Mechanical Engineering, 2013, UCLA

Transonic aeroelastic and aeroservoelastic (ASE) modeling presents a significant technical and computational challenge. Flow fields with a mixture of subsonic and supersonic flow, as well… (more)

Subjects/Keywords: Mechanical engineering; Aerospace engineering; aeroelasticity; aeroservoelasticity; flutter; reduced-order modeling; transonic

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APA (6th Edition):

Gariffo, J. M. (2013). Generalized Reduced Order Modeling of Aeroservoelastic Systems. (Thesis). UCLA. Retrieved from http://www.escholarship.org/uc/item/0rc0c11t

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):

Gariffo, James Michael. “Generalized Reduced Order Modeling of Aeroservoelastic Systems.” 2013. Thesis, UCLA. Accessed January 22, 2021. http://www.escholarship.org/uc/item/0rc0c11t.

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

MLA Handbook (7th Edition):

Gariffo, James Michael. “Generalized Reduced Order Modeling of Aeroservoelastic Systems.” 2013. Web. 22 Jan 2021.

Vancouver:

Gariffo JM. Generalized Reduced Order Modeling of Aeroservoelastic Systems. [Internet] [Thesis]. UCLA; 2013. [cited 2021 Jan 22]. Available from: http://www.escholarship.org/uc/item/0rc0c11t.

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

Council of Science Editors:

Gariffo JM. Generalized Reduced Order Modeling of Aeroservoelastic Systems. [Thesis]. UCLA; 2013. Available from: http://www.escholarship.org/uc/item/0rc0c11t

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


UCLA

14. Larsen, Bradley Robert. Parallel Nonlinear Aeroelastic Computation for Fighter Wings in the Transonic Region.

Degree: Aerospace Engineering, 2015, UCLA

 In this dissertation, a parallel three-dimensional aeroelastic simulation is appliedto current and next generation fighter aircraft wings. The computational model is anonlinear fluid and structural… (more)

Subjects/Keywords: Aerospace engineering; Aeroelastic; Fighter Wing; Flutter; Nonlinear; Parallel; Transonic

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APA (6th Edition):

Larsen, B. R. (2015). Parallel Nonlinear Aeroelastic Computation for Fighter Wings in the Transonic Region. (Thesis). UCLA. Retrieved from http://www.escholarship.org/uc/item/47c3914t

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):

Larsen, Bradley Robert. “Parallel Nonlinear Aeroelastic Computation for Fighter Wings in the Transonic Region.” 2015. Thesis, UCLA. Accessed January 22, 2021. http://www.escholarship.org/uc/item/47c3914t.

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

MLA Handbook (7th Edition):

Larsen, Bradley Robert. “Parallel Nonlinear Aeroelastic Computation for Fighter Wings in the Transonic Region.” 2015. Web. 22 Jan 2021.

Vancouver:

Larsen BR. Parallel Nonlinear Aeroelastic Computation for Fighter Wings in the Transonic Region. [Internet] [Thesis]. UCLA; 2015. [cited 2021 Jan 22]. Available from: http://www.escholarship.org/uc/item/47c3914t.

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

Council of Science Editors:

Larsen BR. Parallel Nonlinear Aeroelastic Computation for Fighter Wings in the Transonic Region. [Thesis]. UCLA; 2015. Available from: http://www.escholarship.org/uc/item/47c3914t

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


Stellenbosch University

15. Nel, Philip. Computational fluid dynamics-modelling of a multi-stage transonic axial-flow compressor.

Degree: MEng, Mechanical and Mechatronic Engineering, 2017, Stellenbosch University

ENGLISH ABSTRACT: This research originates from commercial interest in the numerical modelling of transonic axial compressors. The Darmstadt R-1/S-1 and NASA Stage-37 transonic stages are… (more)

Subjects/Keywords: Compressor industry; Shock waves; Aerodynamics, Transonic; Computational Fluid Dynamics

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

APA (6th Edition):

Nel, P. (2017). Computational fluid dynamics-modelling of a multi-stage transonic axial-flow compressor. (Thesis). Stellenbosch University. Retrieved from http://hdl.handle.net/10019.1/107297

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):

Nel, Philip. “Computational fluid dynamics-modelling of a multi-stage transonic axial-flow compressor.” 2017. Thesis, Stellenbosch University. Accessed January 22, 2021. http://hdl.handle.net/10019.1/107297.

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

MLA Handbook (7th Edition):

Nel, Philip. “Computational fluid dynamics-modelling of a multi-stage transonic axial-flow compressor.” 2017. Web. 22 Jan 2021.

Vancouver:

Nel P. Computational fluid dynamics-modelling of a multi-stage transonic axial-flow compressor. [Internet] [Thesis]. Stellenbosch University; 2017. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/10019.1/107297.

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

Council of Science Editors:

Nel P. Computational fluid dynamics-modelling of a multi-stage transonic axial-flow compressor. [Thesis]. Stellenbosch University; 2017. Available from: http://hdl.handle.net/10019.1/107297

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


University of Miami

16. Wang, Luchen. Investigations of Double Surface Co-Flow Jet Transonic Airfoil.

Degree: MS, Mechanical Engineering (Engineering), 2019, University of Miami

  The objective of this thesis is to investigate The objective of this thesis is to investigate the double surface Co-Flow Jet (CFJ) on the… (more)

Subjects/Keywords: Co-Flow Jet; CFJ; RAE2822; Transonic Airfoil; Circulation Control; CFD

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APA (6th Edition):

Wang, L. (2019). Investigations of Double Surface Co-Flow Jet Transonic Airfoil. (Thesis). University of Miami. Retrieved from https://scholarlyrepository.miami.edu/oa_theses/744

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):

Wang, Luchen. “Investigations of Double Surface Co-Flow Jet Transonic Airfoil.” 2019. Thesis, University of Miami. Accessed January 22, 2021. https://scholarlyrepository.miami.edu/oa_theses/744.

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

MLA Handbook (7th Edition):

Wang, Luchen. “Investigations of Double Surface Co-Flow Jet Transonic Airfoil.” 2019. Web. 22 Jan 2021.

Vancouver:

Wang L. Investigations of Double Surface Co-Flow Jet Transonic Airfoil. [Internet] [Thesis]. University of Miami; 2019. [cited 2021 Jan 22]. Available from: https://scholarlyrepository.miami.edu/oa_theses/744.

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

Council of Science Editors:

Wang L. Investigations of Double Surface Co-Flow Jet Transonic Airfoil. [Thesis]. University of Miami; 2019. Available from: https://scholarlyrepository.miami.edu/oa_theses/744

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


Queen Mary, University of London

17. Saleh, Zainab Jabbar. An investigation into turbine blade tip leakage flows at high speeds.

Degree: PhD, 2015, Queen Mary, University of London

 This investigation studies the leakage flows over the high pressure turbine blade tip at high speed flow conditions. There is an unavoidable gap between the… (more)

Subjects/Keywords: 621.406; high pressure turbine blade tip; transonic tip flows

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APA (6th Edition):

Saleh, Z. J. (2015). An investigation into turbine blade tip leakage flows at high speeds. (Doctoral Dissertation). Queen Mary, University of London. Retrieved from http://qmro.qmul.ac.uk/xmlui/handle/123456789/33937 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.667337

Chicago Manual of Style (16th Edition):

Saleh, Zainab Jabbar. “An investigation into turbine blade tip leakage flows at high speeds.” 2015. Doctoral Dissertation, Queen Mary, University of London. Accessed January 22, 2021. http://qmro.qmul.ac.uk/xmlui/handle/123456789/33937 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.667337.

MLA Handbook (7th Edition):

Saleh, Zainab Jabbar. “An investigation into turbine blade tip leakage flows at high speeds.” 2015. Web. 22 Jan 2021.

Vancouver:

Saleh ZJ. An investigation into turbine blade tip leakage flows at high speeds. [Internet] [Doctoral dissertation]. Queen Mary, University of London; 2015. [cited 2021 Jan 22]. Available from: http://qmro.qmul.ac.uk/xmlui/handle/123456789/33937 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.667337.

Council of Science Editors:

Saleh ZJ. An investigation into turbine blade tip leakage flows at high speeds. [Doctoral Dissertation]. Queen Mary, University of London; 2015. Available from: http://qmro.qmul.ac.uk/xmlui/handle/123456789/33937 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.667337


University of Manchester

18. Yumashev, Dmitry. Viscous-inviscid interaction in a transonic flow caused by a discontinuity in wall curvature.

Degree: PhD, 2010, University of Manchester

 The work addresses an important question of whether a discontinuity in wall curvature can cause boundary layer separation at transonic speeds. Firstly an inviscid transonic(more)

Subjects/Keywords: 519; transonic boundary layer separation

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APA (6th Edition):

Yumashev, D. (2010). Viscous-inviscid interaction in a transonic flow caused by a discontinuity in wall curvature. (Doctoral Dissertation). University of Manchester. Retrieved from http://www.manchester.ac.uk/escholar/uk-ac-man-scw:87020 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.509398

Chicago Manual of Style (16th Edition):

Yumashev, Dmitry. “Viscous-inviscid interaction in a transonic flow caused by a discontinuity in wall curvature.” 2010. Doctoral Dissertation, University of Manchester. Accessed January 22, 2021. http://www.manchester.ac.uk/escholar/uk-ac-man-scw:87020 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.509398.

MLA Handbook (7th Edition):

Yumashev, Dmitry. “Viscous-inviscid interaction in a transonic flow caused by a discontinuity in wall curvature.” 2010. Web. 22 Jan 2021.

Vancouver:

Yumashev D. Viscous-inviscid interaction in a transonic flow caused by a discontinuity in wall curvature. [Internet] [Doctoral dissertation]. University of Manchester; 2010. [cited 2021 Jan 22]. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:87020 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.509398.

Council of Science Editors:

Yumashev D. Viscous-inviscid interaction in a transonic flow caused by a discontinuity in wall curvature. [Doctoral Dissertation]. University of Manchester; 2010. Available from: http://www.manchester.ac.uk/escholar/uk-ac-man-scw:87020 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.509398


Iowa State University

19. Amrit, Anand. Multi-objective optimization of transonic airfoils using variable-fidelity models, co-kriging surrogates, and design space reduction.

Degree: 2016, Iowa State University

 Computationally efficient constrained multi-objective design optimization of transonic airfoils is considered. The proposed methodology focuses on fixed-lift design aimed at finding the best possible trade-offs… (more)

Subjects/Keywords: Aerospace Engineering; design space reduction; optimization; space mapping; transonic; Aerospace Engineering

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APA (6th Edition):

Amrit, A. (2016). Multi-objective optimization of transonic airfoils using variable-fidelity models, co-kriging surrogates, and design space reduction. (Thesis). Iowa State University. Retrieved from https://lib.dr.iastate.edu/etd/15148

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):

Amrit, Anand. “Multi-objective optimization of transonic airfoils using variable-fidelity models, co-kriging surrogates, and design space reduction.” 2016. Thesis, Iowa State University. Accessed January 22, 2021. https://lib.dr.iastate.edu/etd/15148.

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

MLA Handbook (7th Edition):

Amrit, Anand. “Multi-objective optimization of transonic airfoils using variable-fidelity models, co-kriging surrogates, and design space reduction.” 2016. Web. 22 Jan 2021.

Vancouver:

Amrit A. Multi-objective optimization of transonic airfoils using variable-fidelity models, co-kriging surrogates, and design space reduction. [Internet] [Thesis]. Iowa State University; 2016. [cited 2021 Jan 22]. Available from: https://lib.dr.iastate.edu/etd/15148.

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

Council of Science Editors:

Amrit A. Multi-objective optimization of transonic airfoils using variable-fidelity models, co-kriging surrogates, and design space reduction. [Thesis]. Iowa State University; 2016. Available from: https://lib.dr.iastate.edu/etd/15148

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


Virginia Tech

20. Phillips, James Milton Jr. Experimental Study of the Heat Transfer on a Squealer Tip Transonic Turbine Blade with Purge Flow.

Degree: MS, Mechanical Engineering, 2014, Virginia Tech

 The objective of this work is to examine the flow structure and heat transfer distribution of a squealer tip rotor blade with purge flow cooling… (more)

Subjects/Keywords: Squealer Tip; Experimental Heat Transfer; Purge Flow; Transonic

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APA (6th Edition):

Phillips, J. M. J. (2014). Experimental Study of the Heat Transfer on a Squealer Tip Transonic Turbine Blade with Purge Flow. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/24827

Chicago Manual of Style (16th Edition):

Phillips, James Milton Jr. “Experimental Study of the Heat Transfer on a Squealer Tip Transonic Turbine Blade with Purge Flow.” 2014. Masters Thesis, Virginia Tech. Accessed January 22, 2021. http://hdl.handle.net/10919/24827.

MLA Handbook (7th Edition):

Phillips, James Milton Jr. “Experimental Study of the Heat Transfer on a Squealer Tip Transonic Turbine Blade with Purge Flow.” 2014. Web. 22 Jan 2021.

Vancouver:

Phillips JMJ. Experimental Study of the Heat Transfer on a Squealer Tip Transonic Turbine Blade with Purge Flow. [Internet] [Masters thesis]. Virginia Tech; 2014. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/10919/24827.

Council of Science Editors:

Phillips JMJ. Experimental Study of the Heat Transfer on a Squealer Tip Transonic Turbine Blade with Purge Flow. [Masters Thesis]. Virginia Tech; 2014. Available from: http://hdl.handle.net/10919/24827


Virginia Tech

21. Panchal, Kapil V. Development of a robust numerical optimization methodology for turbine endwalls and effect of endwall contouring on turbine passage performance.

Degree: PhD, Mechanical Engineering, 2011, Virginia Tech

 Airfoil endwall contouring has been widely studied during the past two decades for the reduction of secondary losses in turbine passages. Although many endwall contouring… (more)

Subjects/Keywords: Gas Turbines; Endwall Contouring Optimization; Aerodynamics; Transonic Cascade; Heat Transfer

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APA (6th Edition):

Panchal, K. V. (2011). Development of a robust numerical optimization methodology for turbine endwalls and effect of endwall contouring on turbine passage performance. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/77242

Chicago Manual of Style (16th Edition):

Panchal, Kapil V. “Development of a robust numerical optimization methodology for turbine endwalls and effect of endwall contouring on turbine passage performance.” 2011. Doctoral Dissertation, Virginia Tech. Accessed January 22, 2021. http://hdl.handle.net/10919/77242.

MLA Handbook (7th Edition):

Panchal, Kapil V. “Development of a robust numerical optimization methodology for turbine endwalls and effect of endwall contouring on turbine passage performance.” 2011. Web. 22 Jan 2021.

Vancouver:

Panchal KV. Development of a robust numerical optimization methodology for turbine endwalls and effect of endwall contouring on turbine passage performance. [Internet] [Doctoral dissertation]. Virginia Tech; 2011. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/10919/77242.

Council of Science Editors:

Panchal KV. Development of a robust numerical optimization methodology for turbine endwalls and effect of endwall contouring on turbine passage performance. [Doctoral Dissertation]. Virginia Tech; 2011. Available from: http://hdl.handle.net/10919/77242


Virginia Tech

22. Anto, Karu. Effects of Tip Clearance Gap and Exit Mach Number on Turbine Blade Tip and Near-Tip Heat Transfer.

Degree: MS, Mechanical Engineering, 2012, Virginia Tech

 The present study focuses on local heat transfer characteristics on the tip and near-tip regions of a turbine blade with a flat tip, tested under… (more)

Subjects/Keywords: Thin Film Gage; Turbine Blade; Tip Clearance; Heat Transfer; Transonic

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APA (6th Edition):

Anto, K. (2012). Effects of Tip Clearance Gap and Exit Mach Number on Turbine Blade Tip and Near-Tip Heat Transfer. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/76764

Chicago Manual of Style (16th Edition):

Anto, Karu. “Effects of Tip Clearance Gap and Exit Mach Number on Turbine Blade Tip and Near-Tip Heat Transfer.” 2012. Masters Thesis, Virginia Tech. Accessed January 22, 2021. http://hdl.handle.net/10919/76764.

MLA Handbook (7th Edition):

Anto, Karu. “Effects of Tip Clearance Gap and Exit Mach Number on Turbine Blade Tip and Near-Tip Heat Transfer.” 2012. Web. 22 Jan 2021.

Vancouver:

Anto K. Effects of Tip Clearance Gap and Exit Mach Number on Turbine Blade Tip and Near-Tip Heat Transfer. [Internet] [Masters thesis]. Virginia Tech; 2012. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/10919/76764.

Council of Science Editors:

Anto K. Effects of Tip Clearance Gap and Exit Mach Number on Turbine Blade Tip and Near-Tip Heat Transfer. [Masters Thesis]. Virginia Tech; 2012. Available from: http://hdl.handle.net/10919/76764


Virginia Tech

23. Cahill, Joseph E. Identification and Evaluation of Loss and Deviation Models for use in Transonic Compressor Stage Performance Prediction.

Degree: MS, Mechanical Engineering, 1997, Virginia Tech

 The correlation of cascade experimental data is one method for obtaining compressor stage characteristics. These correlations specify pressure loss and flow turning caused by the… (more)

Subjects/Keywords: Axial Compressors; Deviation; Loss; Transonic

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APA (6th Edition):

Cahill, J. E. (1997). Identification and Evaluation of Loss and Deviation Models for use in Transonic Compressor Stage Performance Prediction. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/37041

Chicago Manual of Style (16th Edition):

Cahill, Joseph E. “Identification and Evaluation of Loss and Deviation Models for use in Transonic Compressor Stage Performance Prediction.” 1997. Masters Thesis, Virginia Tech. Accessed January 22, 2021. http://hdl.handle.net/10919/37041.

MLA Handbook (7th Edition):

Cahill, Joseph E. “Identification and Evaluation of Loss and Deviation Models for use in Transonic Compressor Stage Performance Prediction.” 1997. Web. 22 Jan 2021.

Vancouver:

Cahill JE. Identification and Evaluation of Loss and Deviation Models for use in Transonic Compressor Stage Performance Prediction. [Internet] [Masters thesis]. Virginia Tech; 1997. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/10919/37041.

Council of Science Editors:

Cahill JE. Identification and Evaluation of Loss and Deviation Models for use in Transonic Compressor Stage Performance Prediction. [Masters Thesis]. Virginia Tech; 1997. Available from: http://hdl.handle.net/10919/37041


Virginia Tech

24. Roy, Arnab. Experimental Study of Gas Turbine Endwall Cooling with Endwall Contouring under Transonic Conditions.

Degree: PhD, Mechanical Engineering, 2014, Virginia Tech

 The effect of global warming due to increased level of greenhouse gas emissions from coal fired thermal power plants and crisis of reliable energy resources… (more)

Subjects/Keywords: Heat Transfer; Film Cooling; Gas Turbine; Endwall Contouring; Transonic Cascade

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

APA (6th Edition):

Roy, A. (2014). Experimental Study of Gas Turbine Endwall Cooling with Endwall Contouring under Transonic Conditions. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/25801

Chicago Manual of Style (16th Edition):

Roy, Arnab. “Experimental Study of Gas Turbine Endwall Cooling with Endwall Contouring under Transonic Conditions.” 2014. Doctoral Dissertation, Virginia Tech. Accessed January 22, 2021. http://hdl.handle.net/10919/25801.

MLA Handbook (7th Edition):

Roy, Arnab. “Experimental Study of Gas Turbine Endwall Cooling with Endwall Contouring under Transonic Conditions.” 2014. Web. 22 Jan 2021.

Vancouver:

Roy A. Experimental Study of Gas Turbine Endwall Cooling with Endwall Contouring under Transonic Conditions. [Internet] [Doctoral dissertation]. Virginia Tech; 2014. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/10919/25801.

Council of Science Editors:

Roy A. Experimental Study of Gas Turbine Endwall Cooling with Endwall Contouring under Transonic Conditions. [Doctoral Dissertation]. Virginia Tech; 2014. Available from: http://hdl.handle.net/10919/25801


Virginia Tech

25. Lee, Yeong Jin. Aerodynamic Investigation of Upstream Misalignment over the Nozzle Guide Vane in a Transonic Cascade.

Degree: MS, Mechanical Engineering, 2017, Virginia Tech

 The possibility of misalignments at interfaces would be increased due to individual parts' assembly and external factors during its operation. In actual engine representative conditions,… (more)

Subjects/Keywords: Aerodynamic; Misalignment; Vane; Transonic; Secondary Flows; Endwall; Gas turbine

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APA (6th Edition):

Lee, Y. J. (2017). Aerodynamic Investigation of Upstream Misalignment over the Nozzle Guide Vane in a Transonic Cascade. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/77924

Chicago Manual of Style (16th Edition):

Lee, Yeong Jin. “Aerodynamic Investigation of Upstream Misalignment over the Nozzle Guide Vane in a Transonic Cascade.” 2017. Masters Thesis, Virginia Tech. Accessed January 22, 2021. http://hdl.handle.net/10919/77924.

MLA Handbook (7th Edition):

Lee, Yeong Jin. “Aerodynamic Investigation of Upstream Misalignment over the Nozzle Guide Vane in a Transonic Cascade.” 2017. Web. 22 Jan 2021.

Vancouver:

Lee YJ. Aerodynamic Investigation of Upstream Misalignment over the Nozzle Guide Vane in a Transonic Cascade. [Internet] [Masters thesis]. Virginia Tech; 2017. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/10919/77924.

Council of Science Editors:

Lee YJ. Aerodynamic Investigation of Upstream Misalignment over the Nozzle Guide Vane in a Transonic Cascade. [Masters Thesis]. Virginia Tech; 2017. Available from: http://hdl.handle.net/10919/77924


University of Cincinnati

26. Heberling, Brian. A Numerical Analysis on the Effects of Self-Excited Tip Flow Unsteadiness and Upstream Blade Row Interactions on the Performance Predictions of a Transonic Compressor.

Degree: MS, Engineering and Applied Science: Aerospace Engineering, 2017, University of Cincinnati

 Computational fluid dynamics (CFD) simulations can offer a detailed view of the complex flow fields within an axial compressor and greatly aid the design process.… (more)

Subjects/Keywords: Aerospace Materials; computational fluid dynamics; turbomachinery; transonic compressor; cfd; compressor stall

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APA (6th Edition):

Heberling, B. (2017). A Numerical Analysis on the Effects of Self-Excited Tip Flow Unsteadiness and Upstream Blade Row Interactions on the Performance Predictions of a Transonic Compressor. (Masters Thesis). University of Cincinnati. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=ucin150479438822623

Chicago Manual of Style (16th Edition):

Heberling, Brian. “A Numerical Analysis on the Effects of Self-Excited Tip Flow Unsteadiness and Upstream Blade Row Interactions on the Performance Predictions of a Transonic Compressor.” 2017. Masters Thesis, University of Cincinnati. Accessed January 22, 2021. http://rave.ohiolink.edu/etdc/view?acc_num=ucin150479438822623.

MLA Handbook (7th Edition):

Heberling, Brian. “A Numerical Analysis on the Effects of Self-Excited Tip Flow Unsteadiness and Upstream Blade Row Interactions on the Performance Predictions of a Transonic Compressor.” 2017. Web. 22 Jan 2021.

Vancouver:

Heberling B. A Numerical Analysis on the Effects of Self-Excited Tip Flow Unsteadiness and Upstream Blade Row Interactions on the Performance Predictions of a Transonic Compressor. [Internet] [Masters thesis]. University of Cincinnati; 2017. [cited 2021 Jan 22]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin150479438822623.

Council of Science Editors:

Heberling B. A Numerical Analysis on the Effects of Self-Excited Tip Flow Unsteadiness and Upstream Blade Row Interactions on the Performance Predictions of a Transonic Compressor. [Masters Thesis]. University of Cincinnati; 2017. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=ucin150479438822623


The Ohio State University

27. Davis, James A. Transonic interference effects in testing of oscillating airfoils.

Degree: PhD, Graduate School, 1982, The Ohio State University

Subjects/Keywords: Engineering; Aerofoils; Transonic wind tunnels

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APA (6th Edition):

Davis, J. A. (1982). Transonic interference effects in testing of oscillating airfoils. (Doctoral Dissertation). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu14871745550051

Chicago Manual of Style (16th Edition):

Davis, James A. “Transonic interference effects in testing of oscillating airfoils.” 1982. Doctoral Dissertation, The Ohio State University. Accessed January 22, 2021. http://rave.ohiolink.edu/etdc/view?acc_num=osu14871745550051.

MLA Handbook (7th Edition):

Davis, James A. “Transonic interference effects in testing of oscillating airfoils.” 1982. Web. 22 Jan 2021.

Vancouver:

Davis JA. Transonic interference effects in testing of oscillating airfoils. [Internet] [Doctoral dissertation]. The Ohio State University; 1982. [cited 2021 Jan 22]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu14871745550051.

Council of Science Editors:

Davis JA. Transonic interference effects in testing of oscillating airfoils. [Doctoral Dissertation]. The Ohio State University; 1982. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu14871745550051


University of Arizona

28. PRZYBYTKOWSKI, STANISLAW MACIEY. EFFECTS OF WALL INTERFERENCE ON UNSTEADY TRANSONIC FLOWS.

Degree: 1983, University of Arizona

 Various sources of error can cause discrepancies among flight test results, experimental measurements and numerical predictions in the transonic regime. For unsteady flow, the effects… (more)

Subjects/Keywords: Aerodynamics, Transonic  – Mathematical models.; Transonic wind tunnels  – Mathematical models.; Wind tunnels  – Mathematical models.

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APA (6th Edition):

PRZYBYTKOWSKI, S. M. (1983). EFFECTS OF WALL INTERFERENCE ON UNSTEADY TRANSONIC FLOWS. (Doctoral Dissertation). University of Arizona. Retrieved from http://hdl.handle.net/10150/186568

Chicago Manual of Style (16th Edition):

PRZYBYTKOWSKI, STANISLAW MACIEY. “EFFECTS OF WALL INTERFERENCE ON UNSTEADY TRANSONIC FLOWS. ” 1983. Doctoral Dissertation, University of Arizona. Accessed January 22, 2021. http://hdl.handle.net/10150/186568.

MLA Handbook (7th Edition):

PRZYBYTKOWSKI, STANISLAW MACIEY. “EFFECTS OF WALL INTERFERENCE ON UNSTEADY TRANSONIC FLOWS. ” 1983. Web. 22 Jan 2021.

Vancouver:

PRZYBYTKOWSKI SM. EFFECTS OF WALL INTERFERENCE ON UNSTEADY TRANSONIC FLOWS. [Internet] [Doctoral dissertation]. University of Arizona; 1983. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/10150/186568.

Council of Science Editors:

PRZYBYTKOWSKI SM. EFFECTS OF WALL INTERFERENCE ON UNSTEADY TRANSONIC FLOWS. [Doctoral Dissertation]. University of Arizona; 1983. Available from: http://hdl.handle.net/10150/186568


Indian Institute of Science

29. Karnick, Pradeepa Tumkur. Shocks, Shock-Boundary Layer Interaction, And Transonic Flutter.

Degree: PhD, Faculty of Engineering, 2017, Indian Institute of Science

Transonic utter is an aeroelastic instability characterized by part-chord shocks over an airfoil and single mode oscillations leading to a drop in the utter boundary.… (more)

Subjects/Keywords: Aerodynamics; Airfoil; Transonic Flutter; Shock-Boundry Layer; Airplanes; Turbulent Viscous Flow; Flutter Boundary; Shock Dynamics; Aeroelasticity; Euler Flow; Turbulence; Transonic Flow; Aerospace Engineering

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

APA (6th Edition):

Karnick, P. T. (2017). Shocks, Shock-Boundary Layer Interaction, And Transonic Flutter. (Doctoral Dissertation). Indian Institute of Science. Retrieved from http://etd.iisc.ac.in/handle/2005/2688

Chicago Manual of Style (16th Edition):

Karnick, Pradeepa Tumkur. “Shocks, Shock-Boundary Layer Interaction, And Transonic Flutter.” 2017. Doctoral Dissertation, Indian Institute of Science. Accessed January 22, 2021. http://etd.iisc.ac.in/handle/2005/2688.

MLA Handbook (7th Edition):

Karnick, Pradeepa Tumkur. “Shocks, Shock-Boundary Layer Interaction, And Transonic Flutter.” 2017. Web. 22 Jan 2021.

Vancouver:

Karnick PT. Shocks, Shock-Boundary Layer Interaction, And Transonic Flutter. [Internet] [Doctoral dissertation]. Indian Institute of Science; 2017. [cited 2021 Jan 22]. Available from: http://etd.iisc.ac.in/handle/2005/2688.

Council of Science Editors:

Karnick PT. Shocks, Shock-Boundary Layer Interaction, And Transonic Flutter. [Doctoral Dissertation]. Indian Institute of Science; 2017. Available from: http://etd.iisc.ac.in/handle/2005/2688

30. Hu, Hong. Full-Potential Integral Solutions for Steady and Unsteady Transonic Airfoils With and Without Embedded Euler Domains.

Degree: PhD, Mechanical & Aerospace Engineering, 1988, Old Dominion University

  The integral equation solution of the full-potential equation is presented for steady and unsteady transonic airfoil flow problems. The method is also coupled with… (more)

Subjects/Keywords: Integral equation solutions; Euler domains; Transonic airfoils; Transonic flows; Aerospace Engineering

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

APA (6th Edition):

Hu, H. (1988). Full-Potential Integral Solutions for Steady and Unsteady Transonic Airfoils With and Without Embedded Euler Domains. (Doctoral Dissertation). Old Dominion University. Retrieved from https://digitalcommons.odu.edu/mae_etds/250

Chicago Manual of Style (16th Edition):

Hu, Hong. “Full-Potential Integral Solutions for Steady and Unsteady Transonic Airfoils With and Without Embedded Euler Domains.” 1988. Doctoral Dissertation, Old Dominion University. Accessed January 22, 2021. https://digitalcommons.odu.edu/mae_etds/250.

MLA Handbook (7th Edition):

Hu, Hong. “Full-Potential Integral Solutions for Steady and Unsteady Transonic Airfoils With and Without Embedded Euler Domains.” 1988. Web. 22 Jan 2021.

Vancouver:

Hu H. Full-Potential Integral Solutions for Steady and Unsteady Transonic Airfoils With and Without Embedded Euler Domains. [Internet] [Doctoral dissertation]. Old Dominion University; 1988. [cited 2021 Jan 22]. Available from: https://digitalcommons.odu.edu/mae_etds/250.

Council of Science Editors:

Hu H. Full-Potential Integral Solutions for Steady and Unsteady Transonic Airfoils With and Without Embedded Euler Domains. [Doctoral Dissertation]. Old Dominion University; 1988. Available from: https://digitalcommons.odu.edu/mae_etds/250

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