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You searched for subject:(sonic boom). Showing records 1 – 30 of 31 total matches.

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Penn State University

1. Palmer, Joshua David. Quantifying Sonic Boom Metric Variability.

Degree: 2017, Penn State University

 Various sonic boom noise metrics have been calculated for a number of sonic booms, N-wave signatures. The newly computed metrics dataset utilized high-quality recordings from… (more)

Subjects/Keywords: Sonic Boom; Acoustics; Sonic boom metrics

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

APA (6th Edition):

Palmer, J. D. (2017). Quantifying Sonic Boom Metric Variability. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/12142jdp995

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):

Palmer, Joshua David. “Quantifying Sonic Boom Metric Variability.” 2017. Thesis, Penn State University. Accessed January 18, 2021. https://submit-etda.libraries.psu.edu/catalog/12142jdp995.

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

MLA Handbook (7th Edition):

Palmer, Joshua David. “Quantifying Sonic Boom Metric Variability.” 2017. Web. 18 Jan 2021.

Vancouver:

Palmer JD. Quantifying Sonic Boom Metric Variability. [Internet] [Thesis]. Penn State University; 2017. [cited 2021 Jan 18]. Available from: https://submit-etda.libraries.psu.edu/catalog/12142jdp995.

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

Council of Science Editors:

Palmer JD. Quantifying Sonic Boom Metric Variability. [Thesis]. Penn State University; 2017. Available from: https://submit-etda.libraries.psu.edu/catalog/12142jdp995

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


Penn State University

2. Lind, Amanda Blair. Modeling specular reflections and post boom noise to augment synthesized outdoor sonic boom signatures .

Degree: 2011, Penn State University

 In order to increase the fidelity and perceived realism of synthesized sonic booms, a model was created which superimposes specular reflections, arising from simple terrain… (more)

Subjects/Keywords: synthesized sonic boom specular reflections terrai

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APA (6th Edition):

Lind, A. B. (2011). Modeling specular reflections and post boom noise to augment synthesized outdoor sonic boom signatures . (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/10520

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):

Lind, Amanda Blair. “Modeling specular reflections and post boom noise to augment synthesized outdoor sonic boom signatures .” 2011. Thesis, Penn State University. Accessed January 18, 2021. https://submit-etda.libraries.psu.edu/catalog/10520.

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

MLA Handbook (7th Edition):

Lind, Amanda Blair. “Modeling specular reflections and post boom noise to augment synthesized outdoor sonic boom signatures .” 2011. Web. 18 Jan 2021.

Vancouver:

Lind AB. Modeling specular reflections and post boom noise to augment synthesized outdoor sonic boom signatures . [Internet] [Thesis]. Penn State University; 2011. [cited 2021 Jan 18]. Available from: https://submit-etda.libraries.psu.edu/catalog/10520.

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

Council of Science Editors:

Lind AB. Modeling specular reflections and post boom noise to augment synthesized outdoor sonic boom signatures . [Thesis]. Penn State University; 2011. Available from: https://submit-etda.libraries.psu.edu/catalog/10520

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


Penn State University

3. Salamone, Joseph Anthony. Solution of the Lossy Nonlinear Tricomi Equation with Application to Sonic Boom Focusing.

Degree: 2013, Penn State University

Sonic boom focusing theory has been augmented with new terms that account for mean flow effects in the direction of propagation and also for atmospheric… (more)

Subjects/Keywords: sonic boom; focusing; caustic; absorption; dispersion

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APA (6th Edition):

Salamone, J. A. (2013). Solution of the Lossy Nonlinear Tricomi Equation with Application to Sonic Boom Focusing. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/19710

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):

Salamone, Joseph Anthony. “Solution of the Lossy Nonlinear Tricomi Equation with Application to Sonic Boom Focusing.” 2013. Thesis, Penn State University. Accessed January 18, 2021. https://submit-etda.libraries.psu.edu/catalog/19710.

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

MLA Handbook (7th Edition):

Salamone, Joseph Anthony. “Solution of the Lossy Nonlinear Tricomi Equation with Application to Sonic Boom Focusing.” 2013. Web. 18 Jan 2021.

Vancouver:

Salamone JA. Solution of the Lossy Nonlinear Tricomi Equation with Application to Sonic Boom Focusing. [Internet] [Thesis]. Penn State University; 2013. [cited 2021 Jan 18]. Available from: https://submit-etda.libraries.psu.edu/catalog/19710.

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

Council of Science Editors:

Salamone JA. Solution of the Lossy Nonlinear Tricomi Equation with Application to Sonic Boom Focusing. [Thesis]. Penn State University; 2013. Available from: https://submit-etda.libraries.psu.edu/catalog/19710

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


Penn State University

4. Cho, Sang Terry. Finite-Difference Time-Domain Modeling of Low-Amplitude Sonic Boom Diffraction Around Building Structures.

Degree: 2013, Penn State University

 Overland civilian supersonic fights have been banned since 1973 because of the unacceptably loud and intrusive sonic booms generated by supersonic aircraft. However, the continued… (more)

Subjects/Keywords: FDTD; finite-difference; numerical model; sonic boom; low-boom; diffraction

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APA (6th Edition):

Cho, S. T. (2013). Finite-Difference Time-Domain Modeling of Low-Amplitude Sonic Boom Diffraction Around Building Structures. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/17472

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):

Cho, Sang Terry. “Finite-Difference Time-Domain Modeling of Low-Amplitude Sonic Boom Diffraction Around Building Structures.” 2013. Thesis, Penn State University. Accessed January 18, 2021. https://submit-etda.libraries.psu.edu/catalog/17472.

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

MLA Handbook (7th Edition):

Cho, Sang Terry. “Finite-Difference Time-Domain Modeling of Low-Amplitude Sonic Boom Diffraction Around Building Structures.” 2013. Web. 18 Jan 2021.

Vancouver:

Cho ST. Finite-Difference Time-Domain Modeling of Low-Amplitude Sonic Boom Diffraction Around Building Structures. [Internet] [Thesis]. Penn State University; 2013. [cited 2021 Jan 18]. Available from: https://submit-etda.libraries.psu.edu/catalog/17472.

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

Council of Science Editors:

Cho ST. Finite-Difference Time-Domain Modeling of Low-Amplitude Sonic Boom Diffraction Around Building Structures. [Thesis]. Penn State University; 2013. Available from: https://submit-etda.libraries.psu.edu/catalog/17472

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


Penn State University

5. Stout, Trevor. Simulation of N-wave and shaped supersonic signature turbulent variations.

Degree: 2018, Penn State University

 One of the design paradigms for the next generation of civil supersonic aircraft targets a reduction in sonic boom amplitude and impulsivity, creating a “shaped”… (more)

Subjects/Keywords: Sonic boom; Acoustic propagation; Turbulence; KZK; Shaped signature; Low boom; N-wave; Supersonic

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APA (6th Edition):

Stout, T. (2018). Simulation of N-wave and shaped supersonic signature turbulent variations. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/15959tqs5346

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):

Stout, Trevor. “Simulation of N-wave and shaped supersonic signature turbulent variations.” 2018. Thesis, Penn State University. Accessed January 18, 2021. https://submit-etda.libraries.psu.edu/catalog/15959tqs5346.

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

MLA Handbook (7th Edition):

Stout, Trevor. “Simulation of N-wave and shaped supersonic signature turbulent variations.” 2018. Web. 18 Jan 2021.

Vancouver:

Stout T. Simulation of N-wave and shaped supersonic signature turbulent variations. [Internet] [Thesis]. Penn State University; 2018. [cited 2021 Jan 18]. Available from: https://submit-etda.libraries.psu.edu/catalog/15959tqs5346.

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

Council of Science Editors:

Stout T. Simulation of N-wave and shaped supersonic signature turbulent variations. [Thesis]. Penn State University; 2018. Available from: https://submit-etda.libraries.psu.edu/catalog/15959tqs5346

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


Penn State University

6. Locey, Lance Lester. Sonic Boom Postprocessing Functions to Simulate Atmospheric Turbulence Effects .

Degree: 2008, Penn State University

 Two methods of representing the effects of atmospheric turbulence on sonic boom propagation are developed. The first method involves estimating a finite impulse response (FIR)… (more)

Subjects/Keywords: Sonic Boom propagation; turbulence

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

APA (6th Edition):

Locey, L. L. (2008). Sonic Boom Postprocessing Functions to Simulate Atmospheric Turbulence Effects . (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/8848

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):

Locey, Lance Lester. “Sonic Boom Postprocessing Functions to Simulate Atmospheric Turbulence Effects .” 2008. Thesis, Penn State University. Accessed January 18, 2021. https://submit-etda.libraries.psu.edu/catalog/8848.

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

MLA Handbook (7th Edition):

Locey, Lance Lester. “Sonic Boom Postprocessing Functions to Simulate Atmospheric Turbulence Effects .” 2008. Web. 18 Jan 2021.

Vancouver:

Locey LL. Sonic Boom Postprocessing Functions to Simulate Atmospheric Turbulence Effects . [Internet] [Thesis]. Penn State University; 2008. [cited 2021 Jan 18]. Available from: https://submit-etda.libraries.psu.edu/catalog/8848.

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

Council of Science Editors:

Locey LL. Sonic Boom Postprocessing Functions to Simulate Atmospheric Turbulence Effects . [Thesis]. Penn State University; 2008. Available from: https://submit-etda.libraries.psu.edu/catalog/8848

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


Penn State University

7. Riegel, Kimberly A. Propagation of Sonic Booms in Urban Landscapes.

Degree: 2012, Penn State University

 A combined ray tracing/radiosity method for propagation of sonic booms was developed. The method was developed modularly so that complexity can be added and the… (more)

Subjects/Keywords: Sonic Boom; Ray Tracing; Radiosity; Acoustics; Urban Environment

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

APA (6th Edition):

Riegel, K. A. (2012). Propagation of Sonic Booms in Urban Landscapes. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/13881

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):

Riegel, Kimberly A. “Propagation of Sonic Booms in Urban Landscapes.” 2012. Thesis, Penn State University. Accessed January 18, 2021. https://submit-etda.libraries.psu.edu/catalog/13881.

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

MLA Handbook (7th Edition):

Riegel, Kimberly A. “Propagation of Sonic Booms in Urban Landscapes.” 2012. Web. 18 Jan 2021.

Vancouver:

Riegel KA. Propagation of Sonic Booms in Urban Landscapes. [Internet] [Thesis]. Penn State University; 2012. [cited 2021 Jan 18]. Available from: https://submit-etda.libraries.psu.edu/catalog/13881.

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

Council of Science Editors:

Riegel KA. Propagation of Sonic Booms in Urban Landscapes. [Thesis]. Penn State University; 2012. Available from: https://submit-etda.libraries.psu.edu/catalog/13881

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


University of Illinois – Urbana-Champaign

8. Yeong, Yong Han. Wind tunnel testing of a nacelle bypass concept for a quiet supersonic aircraft.

Degree: MS, 4048, 2010, University of Illinois – Urbana-Champaign

Sonic boom attenuation is a considerable design challenge to enable civilian aircraft to operate at supersonic flight conditions. One technology proposed by Gulfstream Aerospace Corporation… (more)

Subjects/Keywords: Sonic Boom; Supersonic; Nacelle Bypass

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

APA (6th Edition):

Yeong, Y. H. (2010). Wind tunnel testing of a nacelle bypass concept for a quiet supersonic aircraft. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/14621

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):

Yeong, Yong Han. “Wind tunnel testing of a nacelle bypass concept for a quiet supersonic aircraft.” 2010. Thesis, University of Illinois – Urbana-Champaign. Accessed January 18, 2021. http://hdl.handle.net/2142/14621.

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

MLA Handbook (7th Edition):

Yeong, Yong Han. “Wind tunnel testing of a nacelle bypass concept for a quiet supersonic aircraft.” 2010. Web. 18 Jan 2021.

Vancouver:

Yeong YH. Wind tunnel testing of a nacelle bypass concept for a quiet supersonic aircraft. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2010. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/2142/14621.

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

Council of Science Editors:

Yeong YH. Wind tunnel testing of a nacelle bypass concept for a quiet supersonic aircraft. [Thesis]. University of Illinois – Urbana-Champaign; 2010. Available from: http://hdl.handle.net/2142/14621

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


Delft University of Technology

9. Nijsse, Jordy (author). Design and Noise Acceptability of Future Supersonic Transport Aircraft.

Degree: 2020, Delft University of Technology

Because of the expected return of civil supersonic flight, research is required to update supersonic noise regulations to allow public acceptance of civil supersonic flights.… (more)

Subjects/Keywords: supersonic; Noise prediction; sonic boom; ICAO; aircraft design; Design program

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

APA (6th Edition):

Nijsse, J. (. (2020). Design and Noise Acceptability of Future Supersonic Transport Aircraft. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:b791a46c-2380-4fb7-b1a5-d3bbd24c9e08

Chicago Manual of Style (16th Edition):

Nijsse, Jordy (author). “Design and Noise Acceptability of Future Supersonic Transport Aircraft.” 2020. Masters Thesis, Delft University of Technology. Accessed January 18, 2021. http://resolver.tudelft.nl/uuid:b791a46c-2380-4fb7-b1a5-d3bbd24c9e08.

MLA Handbook (7th Edition):

Nijsse, Jordy (author). “Design and Noise Acceptability of Future Supersonic Transport Aircraft.” 2020. Web. 18 Jan 2021.

Vancouver:

Nijsse J(. Design and Noise Acceptability of Future Supersonic Transport Aircraft. [Internet] [Masters thesis]. Delft University of Technology; 2020. [cited 2021 Jan 18]. Available from: http://resolver.tudelft.nl/uuid:b791a46c-2380-4fb7-b1a5-d3bbd24c9e08.

Council of Science Editors:

Nijsse J(. Design and Noise Acceptability of Future Supersonic Transport Aircraft. [Masters Thesis]. Delft University of Technology; 2020. Available from: http://resolver.tudelft.nl/uuid:b791a46c-2380-4fb7-b1a5-d3bbd24c9e08


Virginia Tech

10. Haac, Thomas Ryan. Experimental Characterization and Analysis of Simple Residential Structures Subjected to Simulated Sonic Booms.

Degree: MS, Mechanical Engineering, 2010, Virginia Tech

 Commercial aircraft are subject to noise regulations imposed by the Federal Aviation Administration. Currently, the FAA limits overland flight of supersonic airplanes due to the… (more)

Subjects/Keywords: interior acoustic response.; pressure loading; structural forcing; sonic boom simulation; Sonic boom

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

APA (6th Edition):

Haac, T. R. (2010). Experimental Characterization and Analysis of Simple Residential Structures Subjected to Simulated Sonic Booms. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/32921

Chicago Manual of Style (16th Edition):

Haac, Thomas Ryan. “Experimental Characterization and Analysis of Simple Residential Structures Subjected to Simulated Sonic Booms.” 2010. Masters Thesis, Virginia Tech. Accessed January 18, 2021. http://hdl.handle.net/10919/32921.

MLA Handbook (7th Edition):

Haac, Thomas Ryan. “Experimental Characterization and Analysis of Simple Residential Structures Subjected to Simulated Sonic Booms.” 2010. Web. 18 Jan 2021.

Vancouver:

Haac TR. Experimental Characterization and Analysis of Simple Residential Structures Subjected to Simulated Sonic Booms. [Internet] [Masters thesis]. Virginia Tech; 2010. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/10919/32921.

Council of Science Editors:

Haac TR. Experimental Characterization and Analysis of Simple Residential Structures Subjected to Simulated Sonic Booms. [Masters Thesis]. Virginia Tech; 2010. Available from: http://hdl.handle.net/10919/32921


Penn State University

11. Petersen, Erik A. Absorption and dispersion predictions of noise from en-route subsonic and supersonic aircraft.

Degree: 2015, Penn State University

 Predictions of absorption and dispersion of en-route aircraft noise in the atmosphere are produced using the ANSI S1.26 [1] algorithm and an updated algorithm by… (more)

Subjects/Keywords: Acoustics; noise; subsonic; supersonic; aircraft; prediction; Sutherland; Bass; sonic; boom; shock; absorption; dispersion

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

APA (6th Edition):

Petersen, E. A. (2015). Absorption and dispersion predictions of noise from en-route subsonic and supersonic aircraft. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/27351

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):

Petersen, Erik A. “Absorption and dispersion predictions of noise from en-route subsonic and supersonic aircraft.” 2015. Thesis, Penn State University. Accessed January 18, 2021. https://submit-etda.libraries.psu.edu/catalog/27351.

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

MLA Handbook (7th Edition):

Petersen, Erik A. “Absorption and dispersion predictions of noise from en-route subsonic and supersonic aircraft.” 2015. Web. 18 Jan 2021.

Vancouver:

Petersen EA. Absorption and dispersion predictions of noise from en-route subsonic and supersonic aircraft. [Internet] [Thesis]. Penn State University; 2015. [cited 2021 Jan 18]. Available from: https://submit-etda.libraries.psu.edu/catalog/27351.

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

Council of Science Editors:

Petersen EA. Absorption and dispersion predictions of noise from en-route subsonic and supersonic aircraft. [Thesis]. Penn State University; 2015. Available from: https://submit-etda.libraries.psu.edu/catalog/27351

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

12. Khasdeo, Nitin. Sonic Boom Focusing Prediction and Delta Wing Shape Optimization for Boom Mitigation Studies.

Degree: PhD, Aerospace Engineering, 2007, Old Dominion University

  Supersonic travel over land would be a reality if new aircraft are designed such that they produce quieter ground sonic booms, no louder than… (more)

Subjects/Keywords: Boom mitigation; Focusing prediction; Sonic boom; Supersonic aircraft; Wing shape; Aerospace Engineering

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

APA (6th Edition):

Khasdeo, N. (2007). Sonic Boom Focusing Prediction and Delta Wing Shape Optimization for Boom Mitigation Studies. (Doctoral Dissertation). Old Dominion University. Retrieved from 9780549329459 ; https://digitalcommons.odu.edu/mae_etds/72

Chicago Manual of Style (16th Edition):

Khasdeo, Nitin. “Sonic Boom Focusing Prediction and Delta Wing Shape Optimization for Boom Mitigation Studies.” 2007. Doctoral Dissertation, Old Dominion University. Accessed January 18, 2021. 9780549329459 ; https://digitalcommons.odu.edu/mae_etds/72.

MLA Handbook (7th Edition):

Khasdeo, Nitin. “Sonic Boom Focusing Prediction and Delta Wing Shape Optimization for Boom Mitigation Studies.” 2007. Web. 18 Jan 2021.

Vancouver:

Khasdeo N. Sonic Boom Focusing Prediction and Delta Wing Shape Optimization for Boom Mitigation Studies. [Internet] [Doctoral dissertation]. Old Dominion University; 2007. [cited 2021 Jan 18]. Available from: 9780549329459 ; https://digitalcommons.odu.edu/mae_etds/72.

Council of Science Editors:

Khasdeo N. Sonic Boom Focusing Prediction and Delta Wing Shape Optimization for Boom Mitigation Studies. [Doctoral Dissertation]. Old Dominion University; 2007. Available from: 9780549329459 ; https://digitalcommons.odu.edu/mae_etds/72


Penn State University

13. Doebler, William J. The Minimum Number of Ground Measurements Required for Narrow Sonic Boom Metric 90% Confidence Intervals.

Degree: 2017, Penn State University

 For subsonic aircraft noise certification, the value of the effective perceived noise level EPNL must be known within an adequately narrow 90% confidence interval at… (more)

Subjects/Keywords: sonic boom; SCAMP; NASA; FAA; ICAO; confidence interval; metric; certification; noise; sound; supersonic; 90% confidence interval

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

APA (6th Edition):

Doebler, W. J. (2017). The Minimum Number of Ground Measurements Required for Narrow Sonic Boom Metric 90% Confidence Intervals. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/14826wfd5057

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):

Doebler, William J. “The Minimum Number of Ground Measurements Required for Narrow Sonic Boom Metric 90% Confidence Intervals.” 2017. Thesis, Penn State University. Accessed January 18, 2021. https://submit-etda.libraries.psu.edu/catalog/14826wfd5057.

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

MLA Handbook (7th Edition):

Doebler, William J. “The Minimum Number of Ground Measurements Required for Narrow Sonic Boom Metric 90% Confidence Intervals.” 2017. Web. 18 Jan 2021.

Vancouver:

Doebler WJ. The Minimum Number of Ground Measurements Required for Narrow Sonic Boom Metric 90% Confidence Intervals. [Internet] [Thesis]. Penn State University; 2017. [cited 2021 Jan 18]. Available from: https://submit-etda.libraries.psu.edu/catalog/14826wfd5057.

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

Council of Science Editors:

Doebler WJ. The Minimum Number of Ground Measurements Required for Narrow Sonic Boom Metric 90% Confidence Intervals. [Thesis]. Penn State University; 2017. Available from: https://submit-etda.libraries.psu.edu/catalog/14826wfd5057

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


Penn State University

14. Lind, Amanda Blair. Auralizing Impulsive Sounds Outdoors Among Buildings.

Degree: 2017, Penn State University

 Industry partners have identified a market for at least 450 supersonic business jets. Since The Concorde, current legislation prohibits overland supersonic flight, due to the… (more)

Subjects/Keywords: Sonic Boom; Auralization; BTM; Biot Tolstoy Mediwn; Diffraction; Edge Diffraction; Impulsive; Low Frequency; Outdoor; Sound Propagation

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

APA (6th Edition):

Lind, A. B. (2017). Auralizing Impulsive Sounds Outdoors Among Buildings. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/10717abl128

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):

Lind, Amanda Blair. “Auralizing Impulsive Sounds Outdoors Among Buildings.” 2017. Thesis, Penn State University. Accessed January 18, 2021. https://submit-etda.libraries.psu.edu/catalog/10717abl128.

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

MLA Handbook (7th Edition):

Lind, Amanda Blair. “Auralizing Impulsive Sounds Outdoors Among Buildings.” 2017. Web. 18 Jan 2021.

Vancouver:

Lind AB. Auralizing Impulsive Sounds Outdoors Among Buildings. [Internet] [Thesis]. Penn State University; 2017. [cited 2021 Jan 18]. Available from: https://submit-etda.libraries.psu.edu/catalog/10717abl128.

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

Council of Science Editors:

Lind AB. Auralizing Impulsive Sounds Outdoors Among Buildings. [Thesis]. Penn State University; 2017. Available from: https://submit-etda.libraries.psu.edu/catalog/10717abl128

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

15. Yuldashev, Petr. Propagation d'ondes de choc dans les milieux aléatoires avec des inhomogénéités distribuées dans l'espace ou dans une couche mince : Nonlinear shock waves propagation in random media with inhomogeneities distributed in space or concentrated in a thin layer.

Degree: Docteur es, Acoustique, 2011, Ecully, Ecole centrale de Lyon; Université Lomonossov (Moscou)

Pas de résumé

Propagation of nonlinear acoustic waves in inhomogeneous media is an important problem inmany research domains of modern theoretical and applied acoustics. For… (more)

Subjects/Keywords: Ondes de choc; Weak shock waves; Nonlinear acoustics; Shadowgraphy; Sonic boom; Turbulence; Phase screen; Ultrasound; HIFU; Therapeutic arrays

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

APA (6th Edition):

Yuldashev, P. (2011). Propagation d'ondes de choc dans les milieux aléatoires avec des inhomogénéités distribuées dans l'espace ou dans une couche mince : Nonlinear shock waves propagation in random media with inhomogeneities distributed in space or concentrated in a thin layer. (Doctoral Dissertation). Ecully, Ecole centrale de Lyon; Université Lomonossov (Moscou). Retrieved from http://www.theses.fr/2011ECDL0034

Chicago Manual of Style (16th Edition):

Yuldashev, Petr. “Propagation d'ondes de choc dans les milieux aléatoires avec des inhomogénéités distribuées dans l'espace ou dans une couche mince : Nonlinear shock waves propagation in random media with inhomogeneities distributed in space or concentrated in a thin layer.” 2011. Doctoral Dissertation, Ecully, Ecole centrale de Lyon; Université Lomonossov (Moscou). Accessed January 18, 2021. http://www.theses.fr/2011ECDL0034.

MLA Handbook (7th Edition):

Yuldashev, Petr. “Propagation d'ondes de choc dans les milieux aléatoires avec des inhomogénéités distribuées dans l'espace ou dans une couche mince : Nonlinear shock waves propagation in random media with inhomogeneities distributed in space or concentrated in a thin layer.” 2011. Web. 18 Jan 2021.

Vancouver:

Yuldashev P. Propagation d'ondes de choc dans les milieux aléatoires avec des inhomogénéités distribuées dans l'espace ou dans une couche mince : Nonlinear shock waves propagation in random media with inhomogeneities distributed in space or concentrated in a thin layer. [Internet] [Doctoral dissertation]. Ecully, Ecole centrale de Lyon; Université Lomonossov (Moscou); 2011. [cited 2021 Jan 18]. Available from: http://www.theses.fr/2011ECDL0034.

Council of Science Editors:

Yuldashev P. Propagation d'ondes de choc dans les milieux aléatoires avec des inhomogénéités distribuées dans l'espace ou dans une couche mince : Nonlinear shock waves propagation in random media with inhomogeneities distributed in space or concentrated in a thin layer. [Doctoral Dissertation]. Ecully, Ecole centrale de Lyon; Université Lomonossov (Moscou); 2011. Available from: http://www.theses.fr/2011ECDL0034

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

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

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

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

APA (6th Edition):

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

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

Chicago Manual of Style (16th Edition):

山下, 礼. “全空間シミュレーションによる極超音速飛行体のソニックブーム解析(要旨).” 2017. Thesis, The University of Tokyo / 東京大学. Accessed January 18, 2021. http://hdl.handle.net/2261/48849.

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

MLA Handbook (7th Edition):

山下, 礼. “全空間シミュレーションによる極超音速飛行体のソニックブーム解析(要旨).” 2017. Web. 18 Jan 2021.

Vancouver:

山下 . 全空間シミュレーションによる極超音速飛行体のソニックブーム解析(要旨). [Internet] [Thesis]. The University of Tokyo / 東京大学; 2017. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/2261/48849.

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

Council of Science Editors:

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

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


University of Colorado

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

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

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Jung, Timothy Paul. “Modified Linear Theory Aircraft Design Tools and Sonic Boom Minimization Strategy Applied to Signature Freezing via F-function Lobe Balancing.” 2012. Doctoral Dissertation, University of Colorado. Accessed January 18, 2021. https://scholar.colorado.edu/asen_gradetds/49.

MLA Handbook (7th Edition):

Jung, Timothy Paul. “Modified Linear Theory Aircraft Design Tools and Sonic Boom Minimization Strategy Applied to Signature Freezing via F-function Lobe Balancing.” 2012. Web. 18 Jan 2021.

Vancouver:

Jung TP. Modified Linear Theory Aircraft Design Tools and Sonic Boom Minimization Strategy Applied to Signature Freezing via F-function Lobe Balancing. [Internet] [Doctoral dissertation]. University of Colorado; 2012. [cited 2021 Jan 18]. Available from: https://scholar.colorado.edu/asen_gradetds/49.

Council of Science Editors:

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


Delft University of Technology

18. Kinderman, Hendrik Wisse (author). The impact of vertical wing placement on the wave drag and sonic-boom performance at supersonic speeds.

Degree: 2017, Delft University of Technology

 This research project aims at obtaining a better understanding of vertically translating the wing and the related wing-body interference effects on the drag and sonic(more)

Subjects/Keywords: sonic boom; vertical wing placement; wave drag; drag; supersonic; pressure signature; lift; zero-lift; area ruling; area rule; Mach; cone

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APA (6th Edition):

Kinderman, H. W. (. (2017). The impact of vertical wing placement on the wave drag and sonic-boom performance at supersonic speeds. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:b5eaa808-6067-46a5-8d45-0e14d18ceeef

Chicago Manual of Style (16th Edition):

Kinderman, Hendrik Wisse (author). “The impact of vertical wing placement on the wave drag and sonic-boom performance at supersonic speeds.” 2017. Masters Thesis, Delft University of Technology. Accessed January 18, 2021. http://resolver.tudelft.nl/uuid:b5eaa808-6067-46a5-8d45-0e14d18ceeef.

MLA Handbook (7th Edition):

Kinderman, Hendrik Wisse (author). “The impact of vertical wing placement on the wave drag and sonic-boom performance at supersonic speeds.” 2017. Web. 18 Jan 2021.

Vancouver:

Kinderman HW(. The impact of vertical wing placement on the wave drag and sonic-boom performance at supersonic speeds. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2021 Jan 18]. Available from: http://resolver.tudelft.nl/uuid:b5eaa808-6067-46a5-8d45-0e14d18ceeef.

Council of Science Editors:

Kinderman HW(. The impact of vertical wing placement on the wave drag and sonic-boom performance at supersonic speeds. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:b5eaa808-6067-46a5-8d45-0e14d18ceeef

19. Ozcer, Isik A. Multidisciplinary Design Optimization for Sonic Boom Mitigation.

Degree: PhD, Aerospace Engineering, 2009, Old Dominion University

  Automated, parallelized, time-efficient surface definition and grid generation and flow simulation methods are developed for sharp and accurate sonic boom signal computation in three… (more)

Subjects/Keywords: Sonic boom; Supersonic flow; Unstructured Grid Adaptation; Aerospace Engineering

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APA (6th Edition):

Ozcer, I. A. (2009). Multidisciplinary Design Optimization for Sonic Boom Mitigation. (Doctoral Dissertation). Old Dominion University. Retrieved from 9781109142815 ; https://digitalcommons.odu.edu/mae_etds/79

Chicago Manual of Style (16th Edition):

Ozcer, Isik A. “Multidisciplinary Design Optimization for Sonic Boom Mitigation.” 2009. Doctoral Dissertation, Old Dominion University. Accessed January 18, 2021. 9781109142815 ; https://digitalcommons.odu.edu/mae_etds/79.

MLA Handbook (7th Edition):

Ozcer, Isik A. “Multidisciplinary Design Optimization for Sonic Boom Mitigation.” 2009. Web. 18 Jan 2021.

Vancouver:

Ozcer IA. Multidisciplinary Design Optimization for Sonic Boom Mitigation. [Internet] [Doctoral dissertation]. Old Dominion University; 2009. [cited 2021 Jan 18]. Available from: 9781109142815 ; https://digitalcommons.odu.edu/mae_etds/79.

Council of Science Editors:

Ozcer IA. Multidisciplinary Design Optimization for Sonic Boom Mitigation. [Doctoral Dissertation]. Old Dominion University; 2009. Available from: 9781109142815 ; https://digitalcommons.odu.edu/mae_etds/79


Indian Institute of Science

20. Gupta, Hari Shanker. Numerical Study Of Regularization Methods For Elliptic Cauchy Problems.

Degree: PhD, Faculty of Science, 2011, Indian Institute of Science

 Cauchy problems for elliptic partial differential equations arise in many important applications, such as, cardiography, nondestructive testing, heat transfer, sonic boom produced by a maneuvering… (more)

Subjects/Keywords: Numerical Analysis; Manifolds Geometry; Inverse Problems; Elliptic Cauchy Problems; Sonic Boom Problem; Iterated Tikhonov Regularization; Elliptic Inverse Problems; Iterative Tikhonov Regularization; Geometry

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

APA (6th Edition):

Gupta, H. S. (2011). Numerical Study Of Regularization Methods For Elliptic Cauchy Problems. (Doctoral Dissertation). Indian Institute of Science. Retrieved from http://etd.iisc.ac.in/handle/2005/1249

Chicago Manual of Style (16th Edition):

Gupta, Hari Shanker. “Numerical Study Of Regularization Methods For Elliptic Cauchy Problems.” 2011. Doctoral Dissertation, Indian Institute of Science. Accessed January 18, 2021. http://etd.iisc.ac.in/handle/2005/1249.

MLA Handbook (7th Edition):

Gupta, Hari Shanker. “Numerical Study Of Regularization Methods For Elliptic Cauchy Problems.” 2011. Web. 18 Jan 2021.

Vancouver:

Gupta HS. Numerical Study Of Regularization Methods For Elliptic Cauchy Problems. [Internet] [Doctoral dissertation]. Indian Institute of Science; 2011. [cited 2021 Jan 18]. Available from: http://etd.iisc.ac.in/handle/2005/1249.

Council of Science Editors:

Gupta HS. Numerical Study Of Regularization Methods For Elliptic Cauchy Problems. [Doctoral Dissertation]. Indian Institute of Science; 2011. Available from: http://etd.iisc.ac.in/handle/2005/1249

21. Minelli, Andrea. Optimisation aéro-acoustique de forme d'un aéronef supersonique d'affaire : Aero-acoustic shape optimization of a supersonic business jet.

Degree: Docteur es, Mathématiques appliquées, 2013, Nice

Ce travail porte sur le développement de méthodes numériques innovantes pour la conception aéro-acoustique optimale de forme des configurations supersoniques. Ce manuscrit présente tout d'abord… (more)

Subjects/Keywords: Optimisation; Bang sonique; Adaptation de maillage; MDO; Conception inverse; Jeux de Nash; Conception d'avion; Optimization; Sonic boom; Mesh adaptation; MDO; Inverse design; Nash games; Aircraft design

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APA (6th Edition):

Minelli, A. (2013). Optimisation aéro-acoustique de forme d'un aéronef supersonique d'affaire : Aero-acoustic shape optimization of a supersonic business jet. (Doctoral Dissertation). Nice. Retrieved from http://www.theses.fr/2013NICE4107

Chicago Manual of Style (16th Edition):

Minelli, Andrea. “Optimisation aéro-acoustique de forme d'un aéronef supersonique d'affaire : Aero-acoustic shape optimization of a supersonic business jet.” 2013. Doctoral Dissertation, Nice. Accessed January 18, 2021. http://www.theses.fr/2013NICE4107.

MLA Handbook (7th Edition):

Minelli, Andrea. “Optimisation aéro-acoustique de forme d'un aéronef supersonique d'affaire : Aero-acoustic shape optimization of a supersonic business jet.” 2013. Web. 18 Jan 2021.

Vancouver:

Minelli A. Optimisation aéro-acoustique de forme d'un aéronef supersonique d'affaire : Aero-acoustic shape optimization of a supersonic business jet. [Internet] [Doctoral dissertation]. Nice; 2013. [cited 2021 Jan 18]. Available from: http://www.theses.fr/2013NICE4107.

Council of Science Editors:

Minelli A. Optimisation aéro-acoustique de forme d'un aéronef supersonique d'affaire : Aero-acoustic shape optimization of a supersonic business jet. [Doctoral Dissertation]. Nice; 2013. Available from: http://www.theses.fr/2013NICE4107

22. 山﨑, 大地. 水面上を飛行する超音速飛翔体のソニックブームに関するバリスティックレンジ実験(要旨).

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

Subjects/Keywords: Sonic Boom; Ballistic Range; Shock wave; Gas-liquid flow; Underwater overpressure

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APA (6th Edition):

山﨑, . (2017). 水面上を飛行する超音速飛翔体のソニックブームに関するバリスティックレンジ実験(要旨). (Thesis). The University of Tokyo / 東京大学. Retrieved from http://hdl.handle.net/2261/52279

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

Chicago Manual of Style (16th Edition):

山﨑, 大地. “水面上を飛行する超音速飛翔体のソニックブームに関するバリスティックレンジ実験(要旨).” 2017. Thesis, The University of Tokyo / 東京大学. Accessed January 18, 2021. http://hdl.handle.net/2261/52279.

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

MLA Handbook (7th Edition):

山﨑, 大地. “水面上を飛行する超音速飛翔体のソニックブームに関するバリスティックレンジ実験(要旨).” 2017. Web. 18 Jan 2021.

Vancouver:

山﨑 . 水面上を飛行する超音速飛翔体のソニックブームに関するバリスティックレンジ実験(要旨). [Internet] [Thesis]. The University of Tokyo / 東京大学; 2017. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/2261/52279.

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

Council of Science Editors:

山﨑 . 水面上を飛行する超音速飛翔体のソニックブームに関するバリスティックレンジ実験(要旨). [Thesis]. The University of Tokyo / 東京大学; 2017. Available from: http://hdl.handle.net/2261/52279

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


Virginia Tech

23. Corcoran, Joseph Michael. Output-Only Experimental Modal Testing of Large Residential Structures and Acoustic Cavities Using Sonic Booms.

Degree: MS, Mechanical Engineering, 2010, Virginia Tech

 In this thesis, an output-only experimental modal testing and analysis technique known as the Natural Excitation Technique (NExT) is examined for use with large residential… (more)

Subjects/Keywords: acoustic cavity; residential structure; sonic boom; Natural Excitation Technique (NExT); Modal testing

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APA (6th Edition):

Corcoran, J. M. (2010). Output-Only Experimental Modal Testing of Large Residential Structures and Acoustic Cavities Using Sonic Booms. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/31329

Chicago Manual of Style (16th Edition):

Corcoran, Joseph Michael. “Output-Only Experimental Modal Testing of Large Residential Structures and Acoustic Cavities Using Sonic Booms.” 2010. Masters Thesis, Virginia Tech. Accessed January 18, 2021. http://hdl.handle.net/10919/31329.

MLA Handbook (7th Edition):

Corcoran, Joseph Michael. “Output-Only Experimental Modal Testing of Large Residential Structures and Acoustic Cavities Using Sonic Booms.” 2010. Web. 18 Jan 2021.

Vancouver:

Corcoran JM. Output-Only Experimental Modal Testing of Large Residential Structures and Acoustic Cavities Using Sonic Booms. [Internet] [Masters thesis]. Virginia Tech; 2010. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/10919/31329.

Council of Science Editors:

Corcoran JM. Output-Only Experimental Modal Testing of Large Residential Structures and Acoustic Cavities Using Sonic Booms. [Masters Thesis]. Virginia Tech; 2010. Available from: http://hdl.handle.net/10919/31329


Georgia Tech

24. Rallabhandi, Sriram Kishore. Sonic Boom Minimization through Vehicle Shape Optimization and Probabilistic Acoustic Propagation.

Degree: PhD, Aerospace Engineering, 2005, Georgia Tech

Sonic boom annoyance is an important technical showstopper for commercial supersonic aircraft operations. It has been proposed that aircraft can be shaped to alleviate sonic(more)

Subjects/Keywords: Aeroacoustics; Linearized aerodynamics; Shape optimization; Sonic boom; Aircraft design; Structural optimization Mathematics; Vehicles Design and construction; Noise control; Sonic boom; Sound-waves Transmission Mathematical models

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APA (6th Edition):

Rallabhandi, S. K. (2005). Sonic Boom Minimization through Vehicle Shape Optimization and Probabilistic Acoustic Propagation. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/6937

Chicago Manual of Style (16th Edition):

Rallabhandi, Sriram Kishore. “Sonic Boom Minimization through Vehicle Shape Optimization and Probabilistic Acoustic Propagation.” 2005. Doctoral Dissertation, Georgia Tech. Accessed January 18, 2021. http://hdl.handle.net/1853/6937.

MLA Handbook (7th Edition):

Rallabhandi, Sriram Kishore. “Sonic Boom Minimization through Vehicle Shape Optimization and Probabilistic Acoustic Propagation.” 2005. Web. 18 Jan 2021.

Vancouver:

Rallabhandi SK. Sonic Boom Minimization through Vehicle Shape Optimization and Probabilistic Acoustic Propagation. [Internet] [Doctoral dissertation]. Georgia Tech; 2005. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/1853/6937.

Council of Science Editors:

Rallabhandi SK. Sonic Boom Minimization through Vehicle Shape Optimization and Probabilistic Acoustic Propagation. [Doctoral Dissertation]. Georgia Tech; 2005. Available from: http://hdl.handle.net/1853/6937

25. Li, Junhui. Shape Optimization of Supersonic Bodies to Reduce Sonic Boom Signature.

Degree: MS, Mechanical Engineering & Materials Science, 2016, Washington University in St. Louis

  In recent years there has been resurgence of interest by aerospace industry and NASA in supersonic transport aircraft. In recent studies, the emphasis has… (more)

Subjects/Keywords: Sonic boom signature; supersonic aircraft; shape optimization; GA optimization; Aerodynamics and Fluid Mechanics; Engineering

…Optimization of Supersonic Bodies to Reduce Sonic Boom Signature Junhui Li Department of Mechanical… …plane to reduce the acoustic signature of sonic boom resulting from the supersonic aircraft at… …thesis, two cases from the recent AIAA Sonic Boom Prediction Workshop have been simulated and… …one of them is optimized to reduce the sonic boom signature. The AIAA Sonic Boom Prediction… …Workshop has three models for the study of predicting sonic boom signatures and sonic boom… 

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APA (6th Edition):

Li, J. (2016). Shape Optimization of Supersonic Bodies to Reduce Sonic Boom Signature. (Thesis). Washington University in St. Louis. Retrieved from https://openscholarship.wustl.edu/eng_etds/178

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):

Li, Junhui. “Shape Optimization of Supersonic Bodies to Reduce Sonic Boom Signature.” 2016. Thesis, Washington University in St. Louis. Accessed January 18, 2021. https://openscholarship.wustl.edu/eng_etds/178.

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

MLA Handbook (7th Edition):

Li, Junhui. “Shape Optimization of Supersonic Bodies to Reduce Sonic Boom Signature.” 2016. Web. 18 Jan 2021.

Vancouver:

Li J. Shape Optimization of Supersonic Bodies to Reduce Sonic Boom Signature. [Internet] [Thesis]. Washington University in St. Louis; 2016. [cited 2021 Jan 18]. Available from: https://openscholarship.wustl.edu/eng_etds/178.

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

Council of Science Editors:

Li J. Shape Optimization of Supersonic Bodies to Reduce Sonic Boom Signature. [Thesis]. Washington University in St. Louis; 2016. Available from: https://openscholarship.wustl.edu/eng_etds/178

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


Virginia Tech

26. Remillieux, Marcel C. Development of a Model for Predicting the Transmission of Sonic Booms into Buildings at Low Frequency.

Degree: PhD, Mechanical Engineering, 2010, Virginia Tech

 Recent progresses by the aircraft industry in the development of a quieter supersonic transport have opened the possibility of overland supersonic flights, which are currently… (more)

Subjects/Keywords: sonic boom; residential building; fluid-structure interaction; vibration response; finite-element method; modal decomposition; interior acoustic response

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

APA (6th Edition):

Remillieux, M. C. (2010). Development of a Model for Predicting the Transmission of Sonic Booms into Buildings at Low Frequency. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/27543

Chicago Manual of Style (16th Edition):

Remillieux, Marcel C. “Development of a Model for Predicting the Transmission of Sonic Booms into Buildings at Low Frequency.” 2010. Doctoral Dissertation, Virginia Tech. Accessed January 18, 2021. http://hdl.handle.net/10919/27543.

MLA Handbook (7th Edition):

Remillieux, Marcel C. “Development of a Model for Predicting the Transmission of Sonic Booms into Buildings at Low Frequency.” 2010. Web. 18 Jan 2021.

Vancouver:

Remillieux MC. Development of a Model for Predicting the Transmission of Sonic Booms into Buildings at Low Frequency. [Internet] [Doctoral dissertation]. Virginia Tech; 2010. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/10919/27543.

Council of Science Editors:

Remillieux MC. Development of a Model for Predicting the Transmission of Sonic Booms into Buildings at Low Frequency. [Doctoral Dissertation]. Virginia Tech; 2010. Available from: http://hdl.handle.net/10919/27543

27. Giblette, Ted N. Rapid Prediction of Low-Boom and Aerodynamic Performance of Supersonic Transport Aircraft Using Panel Methods.

Degree: MS, Mechanical and Aerospace Engineering, 2019, Utah State University

  The Utah State University Aerolab developed and tested a set of tools for rapid prediction of the loudness of a sonic boom generated by… (more)

Subjects/Keywords: panel methods; sonic boom; class-shape transformations; PANAIR; supersonic; PyLdB; Mechanical Engineering

…Benchmark Against Euler Solution . Sonic Boom and Aerodynamic Performance… …for predicting sonic boom loudness. . . . . . . . . . . . . . . . . . . 3 2.1 Nearfield… …framework for sonic boom optimization. . . . . . . . . . . . . . . 12 3.1 Overview of tool… …in the air cause an audible noise often referred to as a sonic boom. In addition to the… …noise of the sonic boom, these pressure changes can cause other disturbances such as rattling… 

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

APA (6th Edition):

Giblette, T. N. (2019). Rapid Prediction of Low-Boom and Aerodynamic Performance of Supersonic Transport Aircraft Using Panel Methods. (Masters Thesis). Utah State University. Retrieved from https://digitalcommons.usu.edu/etd/7603

Chicago Manual of Style (16th Edition):

Giblette, Ted N. “Rapid Prediction of Low-Boom and Aerodynamic Performance of Supersonic Transport Aircraft Using Panel Methods.” 2019. Masters Thesis, Utah State University. Accessed January 18, 2021. https://digitalcommons.usu.edu/etd/7603.

MLA Handbook (7th Edition):

Giblette, Ted N. “Rapid Prediction of Low-Boom and Aerodynamic Performance of Supersonic Transport Aircraft Using Panel Methods.” 2019. Web. 18 Jan 2021.

Vancouver:

Giblette TN. Rapid Prediction of Low-Boom and Aerodynamic Performance of Supersonic Transport Aircraft Using Panel Methods. [Internet] [Masters thesis]. Utah State University; 2019. [cited 2021 Jan 18]. Available from: https://digitalcommons.usu.edu/etd/7603.

Council of Science Editors:

Giblette TN. Rapid Prediction of Low-Boom and Aerodynamic Performance of Supersonic Transport Aircraft Using Panel Methods. [Masters Thesis]. Utah State University; 2019. Available from: https://digitalcommons.usu.edu/etd/7603

28. Jain, Nishan. Computational Assessment of Flow through a High-Flow Nacelle Bypass for Low Supersonic Boom.

Degree: MS, 4048, 2011, University of Illinois – Urbana-Champaign

Sonic boom minimization is a challenge faced by the aviation community to enable high- speed civilian aircraft flying supersonically over populated land. One of the… (more)

Subjects/Keywords: Reynolds-averaged Navier-Stokes (RANS); turbulence modeling; sonic boom minimization; high-flow nacelle bypass; gearbox; fairing; blockage; turbulence shock interaction

…challenges are 1) the formation and propagation of a sonic boom to the ground during overland… …required thrust. For supersonic flight over land, mitigation of sonic boom is the key to public… …have confirmed that regular occurrences of sonic boom may cause increased community annoyance… …mitigate sonic boom. The strength of the boom is dependent on the size, shape, and weight of the… …concentrated on achieving acceptable sonic boom for small, supersonic business jets. Most of the… 

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

APA (6th Edition):

Jain, N. (2011). Computational Assessment of Flow through a High-Flow Nacelle Bypass for Low Supersonic Boom. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/26111

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):

Jain, Nishan. “Computational Assessment of Flow through a High-Flow Nacelle Bypass for Low Supersonic Boom.” 2011. Thesis, University of Illinois – Urbana-Champaign. Accessed January 18, 2021. http://hdl.handle.net/2142/26111.

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

MLA Handbook (7th Edition):

Jain, Nishan. “Computational Assessment of Flow through a High-Flow Nacelle Bypass for Low Supersonic Boom.” 2011. Web. 18 Jan 2021.

Vancouver:

Jain N. Computational Assessment of Flow through a High-Flow Nacelle Bypass for Low Supersonic Boom. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2011. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/2142/26111.

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

Council of Science Editors:

Jain N. Computational Assessment of Flow through a High-Flow Nacelle Bypass for Low Supersonic Boom. [Thesis]. University of Illinois – Urbana-Champaign; 2011. Available from: http://hdl.handle.net/2142/26111

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

29. Herrera, Arthur A. An experimental study of the forward guide vanes of an engine bypass nacelle for low-boom supersonic flight.

Degree: MS, 4048, 2011, University of Illinois – Urbana-Champaign

 Current FAA regulations limit the speed of civilian passenger jets to subsonic or transonic speeds due to the effects of the sonic boom produced by… (more)

Subjects/Keywords: Supersonic Business Jet (SSBJ); Sonic Boom; Engine Nacelle; Annular Flow; Annular Blockage; Guide Vanes; Wind Tunnel Testing; Experimental Testing

Sonic Boom Demonstrator Root-Sum-Square Variable Frequency Drive xii Chapter 1… …plagued by the negative effects of the sonic boom. Therefore, boom suppression technologies have… …motivated the present experimental study. 1.1 Background A sonic boom is formed by the… …dampened through the atmosphere. This portion of the sonic boom is known as the secondary or… …sonic boom have been a prime focus of research. Not only were boom signatures found to cause… 

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

APA (6th Edition):

Herrera, A. A. (2011). An experimental study of the forward guide vanes of an engine bypass nacelle for low-boom supersonic flight. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/26159

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):

Herrera, Arthur A. “An experimental study of the forward guide vanes of an engine bypass nacelle for low-boom supersonic flight.” 2011. Thesis, University of Illinois – Urbana-Champaign. Accessed January 18, 2021. http://hdl.handle.net/2142/26159.

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

MLA Handbook (7th Edition):

Herrera, Arthur A. “An experimental study of the forward guide vanes of an engine bypass nacelle for low-boom supersonic flight.” 2011. Web. 18 Jan 2021.

Vancouver:

Herrera AA. An experimental study of the forward guide vanes of an engine bypass nacelle for low-boom supersonic flight. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2011. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/2142/26159.

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

Council of Science Editors:

Herrera AA. An experimental study of the forward guide vanes of an engine bypass nacelle for low-boom supersonic flight. [Thesis]. University of Illinois – Urbana-Champaign; 2011. Available from: http://hdl.handle.net/2142/26159

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

30. Hortensius, Ruben. An experimental study of the aft guide vanes of an engine bypass nacelle for low-boom supersonic flight.

Degree: MS, 4048, 2012, University of Illinois – Urbana-Champaign

 Due to the large disturbance created by the sonic boom, supersonic flight is strictly controlled by the FAA. One way in which to minimize the… (more)

Subjects/Keywords: Gulfstream; Rolls-Royce; supersonic engine; bypass; high-flow bypass nacelle; Guide Vanes; oil flow visualization; schlieren; supersonic business jet; quiet supersonic business jet; flow through vanes; choked flow; sonic boom; annular flow; wind tunnel testing; experimental testing

…8 Fig. 1.2. Measured “N” wave pressure signature of a sonic boom from an F-15… …underside of the nacelles generating additional drag and contributing to sonic boom, while b)… …the presence of a sonic boom which accompanies supersonic flight. The sonic boom is an… …By coalescing on the Mach cone, a wave front, or shockwave, known as a sonic boom is formed… …No evidence of the coming body is propagated upstream, but when the sonic boom reaches a… 

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

APA (6th Edition):

Hortensius, R. (2012). An experimental study of the aft guide vanes of an engine bypass nacelle for low-boom supersonic flight. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/29820

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):

Hortensius, Ruben. “An experimental study of the aft guide vanes of an engine bypass nacelle for low-boom supersonic flight.” 2012. Thesis, University of Illinois – Urbana-Champaign. Accessed January 18, 2021. http://hdl.handle.net/2142/29820.

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

MLA Handbook (7th Edition):

Hortensius, Ruben. “An experimental study of the aft guide vanes of an engine bypass nacelle for low-boom supersonic flight.” 2012. Web. 18 Jan 2021.

Vancouver:

Hortensius R. An experimental study of the aft guide vanes of an engine bypass nacelle for low-boom supersonic flight. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2012. [cited 2021 Jan 18]. Available from: http://hdl.handle.net/2142/29820.

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

Council of Science Editors:

Hortensius R. An experimental study of the aft guide vanes of an engine bypass nacelle for low-boom supersonic flight. [Thesis]. University of Illinois – Urbana-Champaign; 2012. Available from: http://hdl.handle.net/2142/29820

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

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