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You searched for subject:(Aerodynamics Transonic). Showing records 1 – 30 of 70 total matches.

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Georgia Tech

1. 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 December 03, 2020. 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. 03 Dec 2020.

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 2020 Dec 03]. 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


University of Tennessee – Knoxville

2. 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 December 03, 2020. 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. 03 Dec 2020.

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 2020 Dec 03]. 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


Stellenbosch University

3. 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 (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 December 03, 2020. 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. 03 Dec 2020.

Vancouver:

Nel P. Computational fluid dynamics-modelling of a multi-stage transonic axial-flow compressor. [Internet] [Thesis]. Stellenbosch University; 2017. [cited 2020 Dec 03]. 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


Virginia Tech

4. 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 December 03, 2020. 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. 03 Dec 2020.

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 2020 Dec 03]. 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

5. Abraham, Santosh. Aerodynamic Performance of High Turning Airfoils and the Effect of Endwall Contouring on Turbine Performance.

Degree: PhD, Mechanical Engineering, 2011, Virginia Tech

 Gas turbine companies are always focused on reducing capital costs and increasing overall efficiency. There are numerous advantages in reducing the number of airfoils per… (more)

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

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APA (6th Edition):

Abraham, S. (2011). Aerodynamic Performance of High Turning Airfoils and the Effect of Endwall Contouring on Turbine Performance. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/77196

Chicago Manual of Style (16th Edition):

Abraham, Santosh. “Aerodynamic Performance of High Turning Airfoils and the Effect of Endwall Contouring on Turbine Performance.” 2011. Doctoral Dissertation, Virginia Tech. Accessed December 03, 2020. http://hdl.handle.net/10919/77196.

MLA Handbook (7th Edition):

Abraham, Santosh. “Aerodynamic Performance of High Turning Airfoils and the Effect of Endwall Contouring on Turbine Performance.” 2011. Web. 03 Dec 2020.

Vancouver:

Abraham S. Aerodynamic Performance of High Turning Airfoils and the Effect of Endwall Contouring on Turbine Performance. [Internet] [Doctoral dissertation]. Virginia Tech; 2011. [cited 2020 Dec 03]. Available from: http://hdl.handle.net/10919/77196.

Council of Science Editors:

Abraham S. Aerodynamic Performance of High Turning Airfoils and the Effect of Endwall Contouring on Turbine Performance. [Doctoral Dissertation]. Virginia Tech; 2011. Available from: http://hdl.handle.net/10919/77196


University of Arizona

6. Shieh, Teng-Hua. Prediction and analysis of wing flutter at transonic speeds.

Degree: 1991, University of Arizona

 This dissertation deals with the instability, known as flutter, of the lifting and control surfaces of aircraft of advanced design at high altitudes and speeds.… (more)

Subjects/Keywords: Flutter (Aerodynamics); Oscillating wings (Aerodynamics); Aerodynamics; Transonic; Aerofoils.

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APA (6th Edition):

Shieh, T. (1991). Prediction and analysis of wing flutter at transonic speeds. (Doctoral Dissertation). University of Arizona. Retrieved from http://hdl.handle.net/10150/185694

Chicago Manual of Style (16th Edition):

Shieh, Teng-Hua. “Prediction and analysis of wing flutter at transonic speeds. ” 1991. Doctoral Dissertation, University of Arizona. Accessed December 03, 2020. http://hdl.handle.net/10150/185694.

MLA Handbook (7th Edition):

Shieh, Teng-Hua. “Prediction and analysis of wing flutter at transonic speeds. ” 1991. Web. 03 Dec 2020.

Vancouver:

Shieh T. Prediction and analysis of wing flutter at transonic speeds. [Internet] [Doctoral dissertation]. University of Arizona; 1991. [cited 2020 Dec 03]. Available from: http://hdl.handle.net/10150/185694.

Council of Science Editors:

Shieh T. Prediction and analysis of wing flutter at transonic speeds. [Doctoral Dissertation]. University of Arizona; 1991. Available from: http://hdl.handle.net/10150/185694


University of Cambridge

7. Melzer, Andrew Philip. Aerodynamics of Transonic Turbine Trailing Edges.

Degree: PhD, 2018, University of Cambridge

Subjects/Keywords: Turbomachinery; Turbines; Aerodynamics; Trailing Edges; Transonic

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APA (6th Edition):

Melzer, A. P. (2018). Aerodynamics of Transonic Turbine Trailing Edges. (Doctoral Dissertation). University of Cambridge. Retrieved from https://www.repository.cam.ac.uk/handle/1810/276280

Chicago Manual of Style (16th Edition):

Melzer, Andrew Philip. “Aerodynamics of Transonic Turbine Trailing Edges.” 2018. Doctoral Dissertation, University of Cambridge. Accessed December 03, 2020. https://www.repository.cam.ac.uk/handle/1810/276280.

MLA Handbook (7th Edition):

Melzer, Andrew Philip. “Aerodynamics of Transonic Turbine Trailing Edges.” 2018. Web. 03 Dec 2020.

Vancouver:

Melzer AP. Aerodynamics of Transonic Turbine Trailing Edges. [Internet] [Doctoral dissertation]. University of Cambridge; 2018. [cited 2020 Dec 03]. Available from: https://www.repository.cam.ac.uk/handle/1810/276280.

Council of Science Editors:

Melzer AP. Aerodynamics of Transonic Turbine Trailing Edges. [Doctoral Dissertation]. University of Cambridge; 2018. Available from: https://www.repository.cam.ac.uk/handle/1810/276280


Virginia Tech

8. Mezynski, Alexis. Measurements of pressure and thermal wakes in a transonic turbine cascade.

Degree: MS, Mechanical Engineering, 1994, Virginia Tech

Subjects/Keywords: Aerodynamics, Transonic.; LD5655.V855 1994.M499

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APA (6th Edition):

Mezynski, A. (1994). Measurements of pressure and thermal wakes in a transonic turbine cascade. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/43142

Chicago Manual of Style (16th Edition):

Mezynski, Alexis. “Measurements of pressure and thermal wakes in a transonic turbine cascade.” 1994. Masters Thesis, Virginia Tech. Accessed December 03, 2020. http://hdl.handle.net/10919/43142.

MLA Handbook (7th Edition):

Mezynski, Alexis. “Measurements of pressure and thermal wakes in a transonic turbine cascade.” 1994. Web. 03 Dec 2020.

Vancouver:

Mezynski A. Measurements of pressure and thermal wakes in a transonic turbine cascade. [Internet] [Masters thesis]. Virginia Tech; 1994. [cited 2020 Dec 03]. Available from: http://hdl.handle.net/10919/43142.

Council of Science Editors:

Mezynski A. Measurements of pressure and thermal wakes in a transonic turbine cascade. [Masters Thesis]. Virginia Tech; 1994. Available from: http://hdl.handle.net/10919/43142


Virginia Tech

9. Janakiraman, S. V. Fluid flow and heat transfer in transonic turbine cascades.

Degree: MS, Mechanical Engineering, 1993, Virginia Tech

 The aerodynamic and thermodynamic performance of an aircraft gas turbine directly affects the fuel consumption of the engine and the life of the turbine components.… (more)

Subjects/Keywords: Aerodynamics; Transonic; LD5655.V855 1993.J363

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APA (6th Edition):

Janakiraman, S. V. (1993). Fluid flow and heat transfer in transonic turbine cascades. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/43173

Chicago Manual of Style (16th Edition):

Janakiraman, S V. “Fluid flow and heat transfer in transonic turbine cascades.” 1993. Masters Thesis, Virginia Tech. Accessed December 03, 2020. http://hdl.handle.net/10919/43173.

MLA Handbook (7th Edition):

Janakiraman, S V. “Fluid flow and heat transfer in transonic turbine cascades.” 1993. Web. 03 Dec 2020.

Vancouver:

Janakiraman SV. Fluid flow and heat transfer in transonic turbine cascades. [Internet] [Masters thesis]. Virginia Tech; 1993. [cited 2020 Dec 03]. Available from: http://hdl.handle.net/10919/43173.

Council of Science Editors:

Janakiraman SV. Fluid flow and heat transfer in transonic turbine cascades. [Masters Thesis]. Virginia Tech; 1993. Available from: http://hdl.handle.net/10919/43173


Virginia Tech

10. Blaesser, Nathaniel James. Interference Drag Due to Engine Nacelle Location for a Single-Aisle, Transonic Aircraft.

Degree: PhD, Aerospace Engineering, 2020, Virginia Tech

 Engine placement on an aircraft is dependent on multiple disciplines. Engine placement affects the noise of the aircraft because the wing can shield or reflect… (more)

Subjects/Keywords: Propulsion-Airframe Integration; Interference Drag; Computational Fluid Dynamics; Transonic Aerodynamics; Wing Design; Aircraft Design

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APA (6th Edition):

Blaesser, N. J. (2020). Interference Drag Due to Engine Nacelle Location for a Single-Aisle, Transonic Aircraft. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/96446

Chicago Manual of Style (16th Edition):

Blaesser, Nathaniel James. “Interference Drag Due to Engine Nacelle Location for a Single-Aisle, Transonic Aircraft.” 2020. Doctoral Dissertation, Virginia Tech. Accessed December 03, 2020. http://hdl.handle.net/10919/96446.

MLA Handbook (7th Edition):

Blaesser, Nathaniel James. “Interference Drag Due to Engine Nacelle Location for a Single-Aisle, Transonic Aircraft.” 2020. Web. 03 Dec 2020.

Vancouver:

Blaesser NJ. Interference Drag Due to Engine Nacelle Location for a Single-Aisle, Transonic Aircraft. [Internet] [Doctoral dissertation]. Virginia Tech; 2020. [cited 2020 Dec 03]. Available from: http://hdl.handle.net/10919/96446.

Council of Science Editors:

Blaesser NJ. Interference Drag Due to Engine Nacelle Location for a Single-Aisle, Transonic Aircraft. [Doctoral Dissertation]. Virginia Tech; 2020. Available from: http://hdl.handle.net/10919/96446


Virginia Tech

11. Luehr, Luke Emerson. Step Misaligned and Film Cooled Nozzle Guide Vanes at Transonic Conditions: Heat Transfer.

Degree: MS, Mechanical Engineering, 2018, Virginia Tech

 This study describes a detailed investigation on the effects that upstream step misalignment and upstream purge film cooling have on the endwall heat transfer for… (more)

Subjects/Keywords: Heat Transfer; Transonic; Film Cooling; Endwall Heat Transfer; Secondary Flows; Endwall Aerodynamics

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APA (6th Edition):

Luehr, L. E. (2018). Step Misaligned and Film Cooled Nozzle Guide Vanes at Transonic Conditions: Heat Transfer. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/83237

Chicago Manual of Style (16th Edition):

Luehr, Luke Emerson. “Step Misaligned and Film Cooled Nozzle Guide Vanes at Transonic Conditions: Heat Transfer.” 2018. Masters Thesis, Virginia Tech. Accessed December 03, 2020. http://hdl.handle.net/10919/83237.

MLA Handbook (7th Edition):

Luehr, Luke Emerson. “Step Misaligned and Film Cooled Nozzle Guide Vanes at Transonic Conditions: Heat Transfer.” 2018. Web. 03 Dec 2020.

Vancouver:

Luehr LE. Step Misaligned and Film Cooled Nozzle Guide Vanes at Transonic Conditions: Heat Transfer. [Internet] [Masters thesis]. Virginia Tech; 2018. [cited 2020 Dec 03]. Available from: http://hdl.handle.net/10919/83237.

Council of Science Editors:

Luehr LE. Step Misaligned and Film Cooled Nozzle Guide Vanes at Transonic Conditions: Heat Transfer. [Masters Thesis]. Virginia Tech; 2018. Available from: http://hdl.handle.net/10919/83237


Virginia Tech

12. Collie, Jeffery C. Unsteady shock wave effects on transonic turbine cascade performance.

Degree: MS, Mechanical Engineering, 1991, Virginia Tech

see document Advisors/Committee Members: Moses, Hal L. (committeechair), Schetz, Joseph A. (committee member), O'Brien, Walter F. Jr. (committee member).

Subjects/Keywords: Aerodynamics; Transonic.; LD5655.V855 1991.C653

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APA (6th Edition):

Collie, J. C. (1991). Unsteady shock wave effects on transonic turbine cascade performance. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/44281

Chicago Manual of Style (16th Edition):

Collie, Jeffery C. “Unsteady shock wave effects on transonic turbine cascade performance.” 1991. Masters Thesis, Virginia Tech. Accessed December 03, 2020. http://hdl.handle.net/10919/44281.

MLA Handbook (7th Edition):

Collie, Jeffery C. “Unsteady shock wave effects on transonic turbine cascade performance.” 1991. Web. 03 Dec 2020.

Vancouver:

Collie JC. Unsteady shock wave effects on transonic turbine cascade performance. [Internet] [Masters thesis]. Virginia Tech; 1991. [cited 2020 Dec 03]. Available from: http://hdl.handle.net/10919/44281.

Council of Science Editors:

Collie JC. Unsteady shock wave effects on transonic turbine cascade performance. [Masters Thesis]. Virginia Tech; 1991. Available from: http://hdl.handle.net/10919/44281


Virginia Tech

13. Nunes, Bonaventure R. Numerical Loss Prediction of high Pressure Steam Turbine airfoils.

Degree: MS, Aerospace Engineering, 2013, Virginia Tech

 Steam turbines are widely used in various industrial applications, primarily for power extraction. However, deviation for operating design conditions is a frequent occurrence for such… (more)

Subjects/Keywords: Steam; Turbines; Transonic Cascade; Aerodynamics; Pressure Loss; Computational Fluid Dynamics (CFD); Ansys CFX

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APA (6th Edition):

Nunes, B. R. (2013). Numerical Loss Prediction of high Pressure Steam Turbine airfoils. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/51742

Chicago Manual of Style (16th Edition):

Nunes, Bonaventure R. “Numerical Loss Prediction of high Pressure Steam Turbine airfoils.” 2013. Masters Thesis, Virginia Tech. Accessed December 03, 2020. http://hdl.handle.net/10919/51742.

MLA Handbook (7th Edition):

Nunes, Bonaventure R. “Numerical Loss Prediction of high Pressure Steam Turbine airfoils.” 2013. Web. 03 Dec 2020.

Vancouver:

Nunes BR. Numerical Loss Prediction of high Pressure Steam Turbine airfoils. [Internet] [Masters thesis]. Virginia Tech; 2013. [cited 2020 Dec 03]. Available from: http://hdl.handle.net/10919/51742.

Council of Science Editors:

Nunes BR. Numerical Loss Prediction of high Pressure Steam Turbine airfoils. [Masters Thesis]. Virginia Tech; 2013. Available from: http://hdl.handle.net/10919/51742


Texas A&M University

14. Elbanna, Hesham Mahmoud. Numerical computation of aerodynamic sensitivity coefficients in the transonic and supersonic regimes.

Degree: MS, aerospace engineering, 2012, Texas A&M University

Subjects/Keywords: aerospace engineering.; Major aerospace engineering.; Aerodynamics, Transonic.; Aerodynamics, Supersonic.

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APA (6th Edition):

Elbanna, H. M. (2012). Numerical computation of aerodynamic sensitivity coefficients in the transonic and supersonic regimes. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1988-THESIS-E37

Chicago Manual of Style (16th Edition):

Elbanna, Hesham Mahmoud. “Numerical computation of aerodynamic sensitivity coefficients in the transonic and supersonic regimes.” 2012. Masters Thesis, Texas A&M University. Accessed December 03, 2020. http://hdl.handle.net/1969.1/ETD-TAMU-1988-THESIS-E37.

MLA Handbook (7th Edition):

Elbanna, Hesham Mahmoud. “Numerical computation of aerodynamic sensitivity coefficients in the transonic and supersonic regimes.” 2012. Web. 03 Dec 2020.

Vancouver:

Elbanna HM. Numerical computation of aerodynamic sensitivity coefficients in the transonic and supersonic regimes. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2020 Dec 03]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1988-THESIS-E37.

Council of Science Editors:

Elbanna HM. Numerical computation of aerodynamic sensitivity coefficients in the transonic and supersonic regimes. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1988-THESIS-E37


Penn State University

15. Oliveira Vieira, Bernardo A. Consideration of Unsteady Aerodynamics and Boundary-Layer Transition in Rotorcraft Airfoil Design.

Degree: 2017, Penn State University

 Traditional rotorcraft airfoil design is based on steady-state aerodynamics, despite the many sources of unsteady-flow in forward flight. At high-thrust and high-speed conditions, the rotor… (more)

Subjects/Keywords: Airfoil Design; Boundary-Layer Transition; Unsteady Aerodynamics; Dynamic Stall; Helicopter Aerodynamics; Transonic Flow; Compressible Flow; Computational Fluid Dynamics; CFD

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APA (6th Edition):

Oliveira Vieira, B. A. (2017). Consideration of Unsteady Aerodynamics and Boundary-Layer Transition in Rotorcraft Airfoil Design. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/13934bao137

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):

Oliveira Vieira, Bernardo A. “Consideration of Unsteady Aerodynamics and Boundary-Layer Transition in Rotorcraft Airfoil Design.” 2017. Thesis, Penn State University. Accessed December 03, 2020. https://submit-etda.libraries.psu.edu/catalog/13934bao137.

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

MLA Handbook (7th Edition):

Oliveira Vieira, Bernardo A. “Consideration of Unsteady Aerodynamics and Boundary-Layer Transition in Rotorcraft Airfoil Design.” 2017. Web. 03 Dec 2020.

Vancouver:

Oliveira Vieira BA. Consideration of Unsteady Aerodynamics and Boundary-Layer Transition in Rotorcraft Airfoil Design. [Internet] [Thesis]. Penn State University; 2017. [cited 2020 Dec 03]. Available from: https://submit-etda.libraries.psu.edu/catalog/13934bao137.

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

Council of Science Editors:

Oliveira Vieira BA. Consideration of Unsteady Aerodynamics and Boundary-Layer Transition in Rotorcraft Airfoil Design. [Thesis]. Penn State University; 2017. Available from: https://submit-etda.libraries.psu.edu/catalog/13934bao137

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


University of Arizona

16. Goble, Brian Dean. A truncation error injection approach to viscous-inviscid interaction.

Degree: 1988, University of Arizona

 A numerical procedure is presented which uses the truncation error injection methodology to efficiently achieve accurate approximations to complex problems having disparate length scales in… (more)

Subjects/Keywords: Aerodynamics, Transonic  – Mathematical models.; Lift (Aerodynamics)  – Mathematical models.

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APA (6th Edition):

Goble, B. D. (1988). A truncation error injection approach to viscous-inviscid interaction. (Doctoral Dissertation). University of Arizona. Retrieved from http://hdl.handle.net/10150/184318

Chicago Manual of Style (16th Edition):

Goble, Brian Dean. “A truncation error injection approach to viscous-inviscid interaction. ” 1988. Doctoral Dissertation, University of Arizona. Accessed December 03, 2020. http://hdl.handle.net/10150/184318.

MLA Handbook (7th Edition):

Goble, Brian Dean. “A truncation error injection approach to viscous-inviscid interaction. ” 1988. Web. 03 Dec 2020.

Vancouver:

Goble BD. A truncation error injection approach to viscous-inviscid interaction. [Internet] [Doctoral dissertation]. University of Arizona; 1988. [cited 2020 Dec 03]. Available from: http://hdl.handle.net/10150/184318.

Council of Science Editors:

Goble BD. A truncation error injection approach to viscous-inviscid interaction. [Doctoral Dissertation]. University of Arizona; 1988. Available from: http://hdl.handle.net/10150/184318


University of Arizona

17. 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 December 03, 2020. http://hdl.handle.net/10150/186568.

MLA Handbook (7th Edition):

PRZYBYTKOWSKI, STANISLAW MACIEY. “EFFECTS OF WALL INTERFERENCE ON UNSTEADY TRANSONIC FLOWS. ” 1983. Web. 03 Dec 2020.

Vancouver:

PRZYBYTKOWSKI SM. EFFECTS OF WALL INTERFERENCE ON UNSTEADY TRANSONIC FLOWS. [Internet] [Doctoral dissertation]. University of Arizona; 1983. [cited 2020 Dec 03]. 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

18. 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 December 03, 2020. 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. 03 Dec 2020.

Vancouver:

Karnick PT. Shocks, Shock-Boundary Layer Interaction, And Transonic Flutter. [Internet] [Doctoral dissertation]. Indian Institute of Science; 2017. [cited 2020 Dec 03]. 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


Texas A&M University

19. Anderson, William Kyle. Inverse transonic wing design on a vector processer.

Degree: MS, aerospace engineering, 2012, Texas A&M University

Subjects/Keywords: aerospace engineering.; Major aerospace engineering.; Aerodynamics, Transonic.; Aerofoils.

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APA (6th Edition):

Anderson, W. K. (2012). Inverse transonic wing design on a vector processer. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1982-THESIS-A552

Chicago Manual of Style (16th Edition):

Anderson, William Kyle. “Inverse transonic wing design on a vector processer.” 2012. Masters Thesis, Texas A&M University. Accessed December 03, 2020. http://hdl.handle.net/1969.1/ETD-TAMU-1982-THESIS-A552.

MLA Handbook (7th Edition):

Anderson, William Kyle. “Inverse transonic wing design on a vector processer.” 2012. Web. 03 Dec 2020.

Vancouver:

Anderson WK. Inverse transonic wing design on a vector processer. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2020 Dec 03]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1982-THESIS-A552.

Council of Science Editors:

Anderson WK. Inverse transonic wing design on a vector processer. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1982-THESIS-A552


Texas A&M University

20. Reed, Christopher L. Grid embedment as applied to viscous transonic airfoil flowfield analysis.

Degree: MS, aerospace engineering, 2012, Texas A&M University

Subjects/Keywords: aerospace engineering.; Major aerospace engineering.; Aerodynamics, Transonic.; Aerofoils.

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APA (6th Edition):

Reed, C. L. (2012). Grid embedment as applied to viscous transonic airfoil flowfield analysis. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/ETD-TAMU-1981-THESIS-R323

Chicago Manual of Style (16th Edition):

Reed, Christopher L. “Grid embedment as applied to viscous transonic airfoil flowfield analysis.” 2012. Masters Thesis, Texas A&M University. Accessed December 03, 2020. http://hdl.handle.net/1969.1/ETD-TAMU-1981-THESIS-R323.

MLA Handbook (7th Edition):

Reed, Christopher L. “Grid embedment as applied to viscous transonic airfoil flowfield analysis.” 2012. Web. 03 Dec 2020.

Vancouver:

Reed CL. Grid embedment as applied to viscous transonic airfoil flowfield analysis. [Internet] [Masters thesis]. Texas A&M University; 2012. [cited 2020 Dec 03]. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1981-THESIS-R323.

Council of Science Editors:

Reed CL. Grid embedment as applied to viscous transonic airfoil flowfield analysis. [Masters Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/ETD-TAMU-1981-THESIS-R323

21. Cuenca, Rafael Gigena. Otimização de desempenho de aerofólios supercríticos: uma abordagem baseada em algoritmos genéticos.

Degree: Mestrado, Ciências de Computação e Matemática Computacional, 2009, University of São Paulo

O presente trabalho tem por objetivo o estudo da otimização multiobjetivo aplicada ao projeto de perfis aerodinâmicos em regime transônico, analisando comparativamente diferentes formas de… (more)

Subjects/Keywords: Aerodinâmica compressíveis; Algoritmos genéticos; CFD; CFD; Compressible aerodynamics; Equações de Euler; Euler equations; Genetic algorithms; Optimization; Otimização; Perfis transônicos; Transonic airfoils

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

APA (6th Edition):

Cuenca, R. G. (2009). Otimização de desempenho de aerofólios supercríticos: uma abordagem baseada em algoritmos genéticos. (Masters Thesis). University of São Paulo. Retrieved from http://www.teses.usp.br/teses/disponiveis/55/55134/tde-16062009-162726/ ;

Chicago Manual of Style (16th Edition):

Cuenca, Rafael Gigena. “Otimização de desempenho de aerofólios supercríticos: uma abordagem baseada em algoritmos genéticos.” 2009. Masters Thesis, University of São Paulo. Accessed December 03, 2020. http://www.teses.usp.br/teses/disponiveis/55/55134/tde-16062009-162726/ ;.

MLA Handbook (7th Edition):

Cuenca, Rafael Gigena. “Otimização de desempenho de aerofólios supercríticos: uma abordagem baseada em algoritmos genéticos.” 2009. Web. 03 Dec 2020.

Vancouver:

Cuenca RG. Otimização de desempenho de aerofólios supercríticos: uma abordagem baseada em algoritmos genéticos. [Internet] [Masters thesis]. University of São Paulo; 2009. [cited 2020 Dec 03]. Available from: http://www.teses.usp.br/teses/disponiveis/55/55134/tde-16062009-162726/ ;.

Council of Science Editors:

Cuenca RG. Otimização de desempenho de aerofólios supercríticos: uma abordagem baseada em algoritmos genéticos. [Masters Thesis]. University of São Paulo; 2009. Available from: http://www.teses.usp.br/teses/disponiveis/55/55134/tde-16062009-162726/ ;


Iowa State University

22. Wear, Richard Rodney. Numerical computation of transonic flow in nozzles with small throat radii of curvature.

Degree: 1971, Iowa State University

Subjects/Keywords: Nozzles; Aerodynamics; Transonic; Aerospace Engineering; Mechanical Engineering; Aerospace Engineering

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

APA (6th Edition):

Wear, R. R. (1971). Numerical computation of transonic flow in nozzles with small throat radii of curvature. (Thesis). Iowa State University. Retrieved from https://lib.dr.iastate.edu/rtd/4519

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):

Wear, Richard Rodney. “Numerical computation of transonic flow in nozzles with small throat radii of curvature.” 1971. Thesis, Iowa State University. Accessed December 03, 2020. https://lib.dr.iastate.edu/rtd/4519.

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

MLA Handbook (7th Edition):

Wear, Richard Rodney. “Numerical computation of transonic flow in nozzles with small throat radii of curvature.” 1971. Web. 03 Dec 2020.

Vancouver:

Wear RR. Numerical computation of transonic flow in nozzles with small throat radii of curvature. [Internet] [Thesis]. Iowa State University; 1971. [cited 2020 Dec 03]. Available from: https://lib.dr.iastate.edu/rtd/4519.

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

Council of Science Editors:

Wear RR. Numerical computation of transonic flow in nozzles with small throat radii of curvature. [Thesis]. Iowa State University; 1971. Available from: https://lib.dr.iastate.edu/rtd/4519

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


University of Notre Dame

23. Mark Hamilton Ross. Tip Clearance Flow Interaction with Circumferential Groove Casing Treatment in a Transonic Axial Compressor</h1>.

Degree: Aerospace and Mechanical Engineering, 2013, University of Notre Dame

  Experimental and computational studies were conducted to study the role of the tip leakage flow in axial compressor stall and the relationship between the… (more)

Subjects/Keywords: tip leakage flow; circumferential groove casing treatment; compressor aerodynamics; transonic axial compressor; surge margin extension; tip clearance axial momentum flux

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APA (6th Edition):

Ross, M. H. (2013). Tip Clearance Flow Interaction with Circumferential Groove Casing Treatment in a Transonic Axial Compressor</h1>. (Thesis). University of Notre Dame. Retrieved from https://curate.nd.edu/show/vq27zk54d16

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):

Ross, Mark Hamilton. “Tip Clearance Flow Interaction with Circumferential Groove Casing Treatment in a Transonic Axial Compressor</h1>.” 2013. Thesis, University of Notre Dame. Accessed December 03, 2020. https://curate.nd.edu/show/vq27zk54d16.

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

MLA Handbook (7th Edition):

Ross, Mark Hamilton. “Tip Clearance Flow Interaction with Circumferential Groove Casing Treatment in a Transonic Axial Compressor</h1>.” 2013. Web. 03 Dec 2020.

Vancouver:

Ross MH. Tip Clearance Flow Interaction with Circumferential Groove Casing Treatment in a Transonic Axial Compressor</h1>. [Internet] [Thesis]. University of Notre Dame; 2013. [cited 2020 Dec 03]. Available from: https://curate.nd.edu/show/vq27zk54d16.

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

Council of Science Editors:

Ross MH. Tip Clearance Flow Interaction with Circumferential Groove Casing Treatment in a Transonic Axial Compressor</h1>. [Thesis]. University of Notre Dame; 2013. Available from: https://curate.nd.edu/show/vq27zk54d16

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


Delft University of Technology

24. Payanda, Qais (author). The Effect of Nozzle Length and Exhaust Plume on Transonic and Supersonic Axisymmetric Base Flows: An Experimental Study.

Degree: 2017, Delft University of Technology

 A combined PIV and Schlieren measurements have been carried out in the transonic-supersonic wind tunnel (TST-27) to investigate the effect of exhaust plume and the… (more)

Subjects/Keywords: Space launcher base flow; Aerodynamics; experimental; PIV; Schlieren; buffet; shock wave; Transonic and supersonic wake; Base-nozzle flow interaction

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APA (6th Edition):

Payanda, Q. (. (2017). The Effect of Nozzle Length and Exhaust Plume on Transonic and Supersonic Axisymmetric Base Flows: An Experimental Study. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:c3064f32-76fc-4b5d-8394-ac5bef450782

Chicago Manual of Style (16th Edition):

Payanda, Qais (author). “The Effect of Nozzle Length and Exhaust Plume on Transonic and Supersonic Axisymmetric Base Flows: An Experimental Study.” 2017. Masters Thesis, Delft University of Technology. Accessed December 03, 2020. http://resolver.tudelft.nl/uuid:c3064f32-76fc-4b5d-8394-ac5bef450782.

MLA Handbook (7th Edition):

Payanda, Qais (author). “The Effect of Nozzle Length and Exhaust Plume on Transonic and Supersonic Axisymmetric Base Flows: An Experimental Study.” 2017. Web. 03 Dec 2020.

Vancouver:

Payanda Q(. The Effect of Nozzle Length and Exhaust Plume on Transonic and Supersonic Axisymmetric Base Flows: An Experimental Study. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2020 Dec 03]. Available from: http://resolver.tudelft.nl/uuid:c3064f32-76fc-4b5d-8394-ac5bef450782.

Council of Science Editors:

Payanda Q(. The Effect of Nozzle Length and Exhaust Plume on Transonic and Supersonic Axisymmetric Base Flows: An Experimental Study. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:c3064f32-76fc-4b5d-8394-ac5bef450782


University of Western Ontario

25. Ali, Shady Mohamed Mohamed. Numerical Simulation of Air Flow in Aeroengine Compressors.

Degree: 2017, University of Western Ontario

 The performance of an aeroengine is influenced by the performance of the compressor system. A typical compressor consists of multistage axial compressors followed by a… (more)

Subjects/Keywords: CFD; centrifugal compressor; axial transonic compressor; flow blockage; rotor-stator gap; curvature correction; Aerodynamics and Fluid Mechanics

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APA (6th Edition):

Ali, S. M. M. (2017). Numerical Simulation of Air Flow in Aeroengine Compressors. (Thesis). University of Western Ontario. Retrieved from https://ir.lib.uwo.ca/etd/4392

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):

Ali, Shady Mohamed Mohamed. “Numerical Simulation of Air Flow in Aeroengine Compressors.” 2017. Thesis, University of Western Ontario. Accessed December 03, 2020. https://ir.lib.uwo.ca/etd/4392.

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

MLA Handbook (7th Edition):

Ali, Shady Mohamed Mohamed. “Numerical Simulation of Air Flow in Aeroengine Compressors.” 2017. Web. 03 Dec 2020.

Vancouver:

Ali SMM. Numerical Simulation of Air Flow in Aeroengine Compressors. [Internet] [Thesis]. University of Western Ontario; 2017. [cited 2020 Dec 03]. Available from: https://ir.lib.uwo.ca/etd/4392.

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

Council of Science Editors:

Ali SMM. Numerical Simulation of Air Flow in Aeroengine Compressors. [Thesis]. University of Western Ontario; 2017. Available from: https://ir.lib.uwo.ca/etd/4392

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


University of New Mexico

26. Atkinson, John Hopkins. A Shock Tube for Transonic and Supersonic Aerodynamic Research.

Degree: Mechanical Engineering, 1955, University of New Mexico

  The purpose of building a shock tube was to give the University another research tool and demonstration instrument for aerodynamic studies since the present… (more)

Subjects/Keywords: Shock Tube; Aerodynamics; Transonic; Supersonic; Mechanical Engineering

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APA (6th Edition):

Atkinson, J. H. (1955). A Shock Tube for Transonic and Supersonic Aerodynamic Research. (Masters Thesis). University of New Mexico. Retrieved from https://digitalrepository.unm.edu/me_etds/105

Chicago Manual of Style (16th Edition):

Atkinson, John Hopkins. “A Shock Tube for Transonic and Supersonic Aerodynamic Research.” 1955. Masters Thesis, University of New Mexico. Accessed December 03, 2020. https://digitalrepository.unm.edu/me_etds/105.

MLA Handbook (7th Edition):

Atkinson, John Hopkins. “A Shock Tube for Transonic and Supersonic Aerodynamic Research.” 1955. Web. 03 Dec 2020.

Vancouver:

Atkinson JH. A Shock Tube for Transonic and Supersonic Aerodynamic Research. [Internet] [Masters thesis]. University of New Mexico; 1955. [cited 2020 Dec 03]. Available from: https://digitalrepository.unm.edu/me_etds/105.

Council of Science Editors:

Atkinson JH. A Shock Tube for Transonic and Supersonic Aerodynamic Research. [Masters Thesis]. University of New Mexico; 1955. Available from: https://digitalrepository.unm.edu/me_etds/105


University of Arizona

27. LIANG, SHEN-MIN. REFINED NUMERICAL SOLUTIONS OF THE TRANSONIC FLOW PAST A WEDGE (OBLIQUE SHOCK).

Degree: 1985, University of Arizona

 An adaptive refinement procedure combining the ideas of solving a modified difference equation and of adaptive mesh refinement is introduced. The numerical solution on a… (more)

Subjects/Keywords: Aerodynamics, Transonic  – Mathematical models.; Numerical grid generation (Numerical analysis)

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APA (6th Edition):

LIANG, S. (1985). REFINED NUMERICAL SOLUTIONS OF THE TRANSONIC FLOW PAST A WEDGE (OBLIQUE SHOCK). (Doctoral Dissertation). University of Arizona. Retrieved from http://hdl.handle.net/10150/187911

Chicago Manual of Style (16th Edition):

LIANG, SHEN-MIN. “REFINED NUMERICAL SOLUTIONS OF THE TRANSONIC FLOW PAST A WEDGE (OBLIQUE SHOCK). ” 1985. Doctoral Dissertation, University of Arizona. Accessed December 03, 2020. http://hdl.handle.net/10150/187911.

MLA Handbook (7th Edition):

LIANG, SHEN-MIN. “REFINED NUMERICAL SOLUTIONS OF THE TRANSONIC FLOW PAST A WEDGE (OBLIQUE SHOCK). ” 1985. Web. 03 Dec 2020.

Vancouver:

LIANG S. REFINED NUMERICAL SOLUTIONS OF THE TRANSONIC FLOW PAST A WEDGE (OBLIQUE SHOCK). [Internet] [Doctoral dissertation]. University of Arizona; 1985. [cited 2020 Dec 03]. Available from: http://hdl.handle.net/10150/187911.

Council of Science Editors:

LIANG S. REFINED NUMERICAL SOLUTIONS OF THE TRANSONIC FLOW PAST A WEDGE (OBLIQUE SHOCK). [Doctoral Dissertation]. University of Arizona; 1985. Available from: http://hdl.handle.net/10150/187911


Virginia Tech

28. Mayo, David Earl Jr. The Effect of Combustor Exit to Nozzle Guide Vane Platform Misalignment on Heat Transfer over an Axisymmetric Endwall at Transonic Conditions.

Degree: MS, Mechanical Engineering, 2016, Virginia Tech

 This paper presents details of an experimental and computational investigation on the effect of misalignment between the combustor exit and nozzle guide vane endwall on… (more)

Subjects/Keywords: Computational Fluid Dynamics; Endwall Heat Transfer; Endwall Aerodynamics; Transonic; Experimental Heat Transfer; Gas Turbines; Secondary Flows

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APA (6th Edition):

Mayo, D. E. J. (2016). The Effect of Combustor Exit to Nozzle Guide Vane Platform Misalignment on Heat Transfer over an Axisymmetric Endwall at Transonic Conditions. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/78110

Chicago Manual of Style (16th Edition):

Mayo, David Earl Jr. “The Effect of Combustor Exit to Nozzle Guide Vane Platform Misalignment on Heat Transfer over an Axisymmetric Endwall at Transonic Conditions.” 2016. Masters Thesis, Virginia Tech. Accessed December 03, 2020. http://hdl.handle.net/10919/78110.

MLA Handbook (7th Edition):

Mayo, David Earl Jr. “The Effect of Combustor Exit to Nozzle Guide Vane Platform Misalignment on Heat Transfer over an Axisymmetric Endwall at Transonic Conditions.” 2016. Web. 03 Dec 2020.

Vancouver:

Mayo DEJ. The Effect of Combustor Exit to Nozzle Guide Vane Platform Misalignment on Heat Transfer over an Axisymmetric Endwall at Transonic Conditions. [Internet] [Masters thesis]. Virginia Tech; 2016. [cited 2020 Dec 03]. Available from: http://hdl.handle.net/10919/78110.

Council of Science Editors:

Mayo DEJ. The Effect of Combustor Exit to Nozzle Guide Vane Platform Misalignment on Heat Transfer over an Axisymmetric Endwall at Transonic Conditions. [Masters Thesis]. Virginia Tech; 2016. Available from: http://hdl.handle.net/10919/78110


Virginia Tech

29. Blot, Dorian Matthew. Aerodynamics of Endwall Contouring with Discrete Holes and an Upstream Purge Slot Under Transonic Conditions  with and without Blowing.

Degree: MS, Mechanical Engineering, 2013, Virginia Tech

 Endwall contouring has been widely studied as an effective measure to improve aerodynamic performance by reducing secondary flow strength. The effects of endwall contouring with… (more)

Subjects/Keywords: Gas Turbines; Transonic Cascade; Aerodynamics. Heat Transfer; Film Cooling; Upstream Purge Slot; Discrete Hole Cooling; Endwall

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APA (6th Edition):

Blot, D. M. (2013). Aerodynamics of Endwall Contouring with Discrete Holes and an Upstream Purge Slot Under Transonic Conditions  with and without Blowing. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/19257

Chicago Manual of Style (16th Edition):

Blot, Dorian Matthew. “Aerodynamics of Endwall Contouring with Discrete Holes and an Upstream Purge Slot Under Transonic Conditions  with and without Blowing.” 2013. Masters Thesis, Virginia Tech. Accessed December 03, 2020. http://hdl.handle.net/10919/19257.

MLA Handbook (7th Edition):

Blot, Dorian Matthew. “Aerodynamics of Endwall Contouring with Discrete Holes and an Upstream Purge Slot Under Transonic Conditions  with and without Blowing.” 2013. Web. 03 Dec 2020.

Vancouver:

Blot DM. Aerodynamics of Endwall Contouring with Discrete Holes and an Upstream Purge Slot Under Transonic Conditions  with and without Blowing. [Internet] [Masters thesis]. Virginia Tech; 2013. [cited 2020 Dec 03]. Available from: http://hdl.handle.net/10919/19257.

Council of Science Editors:

Blot DM. Aerodynamics of Endwall Contouring with Discrete Holes and an Upstream Purge Slot Under Transonic Conditions  with and without Blowing. [Masters Thesis]. Virginia Tech; 2013. Available from: http://hdl.handle.net/10919/19257


University of Sydney

30. Giannelis, Nicholas Frank. Transonic Shock Buffet in Rigid and Aeroelastic Systems .

Degree: University of Sydney

 For limited flight conditions in the transonic regime, self-sustained shock oscillations may develop. This transonic shock buffet phenomenon limits the flight envelope and is detrimental… (more)

Subjects/Keywords: transonic shock buffet; Aeroelasticity; Compressible Aerodynamics; Modal analysis

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APA (6th Edition):

Giannelis, N. F. (n.d.). Transonic Shock Buffet in Rigid and Aeroelastic Systems . (Thesis). University of Sydney. Retrieved from http://hdl.handle.net/2123/21515

Note: this citation may be lacking information needed for this citation format:
No year of publication.
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Giannelis, Nicholas Frank. “Transonic Shock Buffet in Rigid and Aeroelastic Systems .” Thesis, University of Sydney. Accessed December 03, 2020. http://hdl.handle.net/2123/21515.

Note: this citation may be lacking information needed for this citation format:
No year of publication.
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Giannelis, Nicholas Frank. “Transonic Shock Buffet in Rigid and Aeroelastic Systems .” Web. 03 Dec 2020.

Note: this citation may be lacking information needed for this citation format:
No year of publication.

Vancouver:

Giannelis NF. Transonic Shock Buffet in Rigid and Aeroelastic Systems . [Internet] [Thesis]. University of Sydney; [cited 2020 Dec 03]. Available from: http://hdl.handle.net/2123/21515.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation
No year of publication.

Council of Science Editors:

Giannelis NF. Transonic Shock Buffet in Rigid and Aeroelastic Systems . [Thesis]. University of Sydney; Available from: http://hdl.handle.net/2123/21515

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation
No year of publication.

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