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You searched for subject:( fuselage). Showing records 1 – 30 of 63 total matches.

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Drexel University

1. Siromani, Deepak. Crashworthy Design and Analysis of Aircraft Structures.

Degree: 2013, Drexel University

Crashworthiness of an aircraft fuselage and its structural components was investigated experimentally and numerically in this study. A finite element model developed previously for simulating… (more)

Subjects/Keywords: Mechanical engineering; Airplanes – Fuselage; Airplanes – Crashworthiness

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APA (6th Edition):

Siromani, D. (2013). Crashworthy Design and Analysis of Aircraft Structures. (Thesis). Drexel University. Retrieved from http://hdl.handle.net/1860/4380

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):

Siromani, Deepak. “Crashworthy Design and Analysis of Aircraft Structures.” 2013. Thesis, Drexel University. Accessed August 18, 2019. http://hdl.handle.net/1860/4380.

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

MLA Handbook (7th Edition):

Siromani, Deepak. “Crashworthy Design and Analysis of Aircraft Structures.” 2013. Web. 18 Aug 2019.

Vancouver:

Siromani D. Crashworthy Design and Analysis of Aircraft Structures. [Internet] [Thesis]. Drexel University; 2013. [cited 2019 Aug 18]. Available from: http://hdl.handle.net/1860/4380.

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

Council of Science Editors:

Siromani D. Crashworthy Design and Analysis of Aircraft Structures. [Thesis]. Drexel University; 2013. Available from: http://hdl.handle.net/1860/4380

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


Delft University of Technology

2. Van Tooren, M.J.L. Sandwich fuselage design.

Degree: 1998, Delft University of Technology

Subjects/Keywords: sandwich; fuselage; composite

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APA (6th Edition):

Van Tooren, M. J. L. (1998). Sandwich fuselage design. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:5ae43ed1-345f-423a-8285-d151e9bd34d0 ; urn:NBN:nl:ui:24-uuid:5ae43ed1-345f-423a-8285-d151e9bd34d0 ; urn:NBN:nl:ui:24-uuid:5ae43ed1-345f-423a-8285-d151e9bd34d0 ; http://resolver.tudelft.nl/uuid:5ae43ed1-345f-423a-8285-d151e9bd34d0

Chicago Manual of Style (16th Edition):

Van Tooren, M J L. “Sandwich fuselage design.” 1998. Doctoral Dissertation, Delft University of Technology. Accessed August 18, 2019. http://resolver.tudelft.nl/uuid:5ae43ed1-345f-423a-8285-d151e9bd34d0 ; urn:NBN:nl:ui:24-uuid:5ae43ed1-345f-423a-8285-d151e9bd34d0 ; urn:NBN:nl:ui:24-uuid:5ae43ed1-345f-423a-8285-d151e9bd34d0 ; http://resolver.tudelft.nl/uuid:5ae43ed1-345f-423a-8285-d151e9bd34d0.

MLA Handbook (7th Edition):

Van Tooren, M J L. “Sandwich fuselage design.” 1998. Web. 18 Aug 2019.

Vancouver:

Van Tooren MJL. Sandwich fuselage design. [Internet] [Doctoral dissertation]. Delft University of Technology; 1998. [cited 2019 Aug 18]. Available from: http://resolver.tudelft.nl/uuid:5ae43ed1-345f-423a-8285-d151e9bd34d0 ; urn:NBN:nl:ui:24-uuid:5ae43ed1-345f-423a-8285-d151e9bd34d0 ; urn:NBN:nl:ui:24-uuid:5ae43ed1-345f-423a-8285-d151e9bd34d0 ; http://resolver.tudelft.nl/uuid:5ae43ed1-345f-423a-8285-d151e9bd34d0.

Council of Science Editors:

Van Tooren MJL. Sandwich fuselage design. [Doctoral Dissertation]. Delft University of Technology; 1998. Available from: http://resolver.tudelft.nl/uuid:5ae43ed1-345f-423a-8285-d151e9bd34d0 ; urn:NBN:nl:ui:24-uuid:5ae43ed1-345f-423a-8285-d151e9bd34d0 ; urn:NBN:nl:ui:24-uuid:5ae43ed1-345f-423a-8285-d151e9bd34d0 ; http://resolver.tudelft.nl/uuid:5ae43ed1-345f-423a-8285-d151e9bd34d0


The Ohio State University

3. Rhodes, Gregory D. Experimental Investigations of the Propulsive Fuselage Concept.

Degree: MS, Aero/Astro Engineering, 2018, The Ohio State University

 Air traffic across the globe is expected to increase dramatically by the year 2035, with nearly twice as many passengers as compared to 2016 [1].… (more)

Subjects/Keywords: Aerospace Engineering; drag ingestion; propulsive fuselage

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APA (6th Edition):

Rhodes, G. D. (2018). Experimental Investigations of the Propulsive Fuselage Concept. (Masters Thesis). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1523355985000317

Chicago Manual of Style (16th Edition):

Rhodes, Gregory D. “Experimental Investigations of the Propulsive Fuselage Concept.” 2018. Masters Thesis, The Ohio State University. Accessed August 18, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=osu1523355985000317.

MLA Handbook (7th Edition):

Rhodes, Gregory D. “Experimental Investigations of the Propulsive Fuselage Concept.” 2018. Web. 18 Aug 2019.

Vancouver:

Rhodes GD. Experimental Investigations of the Propulsive Fuselage Concept. [Internet] [Masters thesis]. The Ohio State University; 2018. [cited 2019 Aug 18]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1523355985000317.

Council of Science Editors:

Rhodes GD. Experimental Investigations of the Propulsive Fuselage Concept. [Masters Thesis]. The Ohio State University; 2018. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1523355985000317


Brno University of Technology

4. Sadovský, Hynek. Návrh uzlu křídlo-trup kompozitního letounu .

Degree: 2015, Brno University of Technology

 Diplomová práce se zabývá konstrukčním, pevnostním a technologickým návrhem uzlu křídlo-trup celokompozitového čtyřmístného letounu certifikovaného dle předpisu CS-23. Návrh je zaměřen na optimální využití prostoru,… (more)

Subjects/Keywords: křídlo; trup; kompozitní konstrukce; spojení křídlo-trup; wing; fuselage; composite construction; wing-fuselage joint; composite material; wet lay-up; vacuum technology

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APA (6th Edition):

Sadovský, H. (2015). Návrh uzlu křídlo-trup kompozitního letounu . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/40267

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):

Sadovský, Hynek. “Návrh uzlu křídlo-trup kompozitního letounu .” 2015. Thesis, Brno University of Technology. Accessed August 18, 2019. http://hdl.handle.net/11012/40267.

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

MLA Handbook (7th Edition):

Sadovský, Hynek. “Návrh uzlu křídlo-trup kompozitního letounu .” 2015. Web. 18 Aug 2019.

Vancouver:

Sadovský H. Návrh uzlu křídlo-trup kompozitního letounu . [Internet] [Thesis]. Brno University of Technology; 2015. [cited 2019 Aug 18]. Available from: http://hdl.handle.net/11012/40267.

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

Council of Science Editors:

Sadovský H. Návrh uzlu křídlo-trup kompozitního letounu . [Thesis]. Brno University of Technology; 2015. Available from: http://hdl.handle.net/11012/40267

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


The Ohio State University

5. Kim, Jacob Jeong-Geun. Simulation and analysis of airborne antenna radiation patterns.

Degree: PhD, Graduate School, 1985, The Ohio State University

Subjects/Keywords: Engineering; Antennas; Airplanes – Fuselage

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APA (6th Edition):

Kim, J. J. (1985). Simulation and analysis of airborne antenna radiation patterns. (Doctoral Dissertation). The Ohio State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=osu1487257452616436

Chicago Manual of Style (16th Edition):

Kim, Jacob Jeong-Geun. “Simulation and analysis of airborne antenna radiation patterns.” 1985. Doctoral Dissertation, The Ohio State University. Accessed August 18, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=osu1487257452616436.

MLA Handbook (7th Edition):

Kim, Jacob Jeong-Geun. “Simulation and analysis of airborne antenna radiation patterns.” 1985. Web. 18 Aug 2019.

Vancouver:

Kim JJ. Simulation and analysis of airborne antenna radiation patterns. [Internet] [Doctoral dissertation]. The Ohio State University; 1985. [cited 2019 Aug 18]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1487257452616436.

Council of Science Editors:

Kim JJ. Simulation and analysis of airborne antenna radiation patterns. [Doctoral Dissertation]. The Ohio State University; 1985. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=osu1487257452616436


Heriot-Watt University

6. Platten, Michael Francis. Sound and vibration transmission in aircraft using statistical energy analysis.

Degree: 1998, Heriot-Watt University

Subjects/Keywords: 534; Fuselage; acoustic transmission

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APA (6th Edition):

Platten, M. F. (1998). Sound and vibration transmission in aircraft using statistical energy analysis. (Doctoral Dissertation). Heriot-Watt University. Retrieved from http://hdl.handle.net/10399/625

Chicago Manual of Style (16th Edition):

Platten, Michael Francis. “Sound and vibration transmission in aircraft using statistical energy analysis.” 1998. Doctoral Dissertation, Heriot-Watt University. Accessed August 18, 2019. http://hdl.handle.net/10399/625.

MLA Handbook (7th Edition):

Platten, Michael Francis. “Sound and vibration transmission in aircraft using statistical energy analysis.” 1998. Web. 18 Aug 2019.

Vancouver:

Platten MF. Sound and vibration transmission in aircraft using statistical energy analysis. [Internet] [Doctoral dissertation]. Heriot-Watt University; 1998. [cited 2019 Aug 18]. Available from: http://hdl.handle.net/10399/625.

Council of Science Editors:

Platten MF. Sound and vibration transmission in aircraft using statistical energy analysis. [Doctoral Dissertation]. Heriot-Watt University; 1998. Available from: http://hdl.handle.net/10399/625


Georgia Tech

7. Atre, Amarendra. A Finite Element and Experimental Investigation on the Fatigue of Riveted Lap Joints in Aircraft Applications.

Degree: PhD, Mechanical Engineering, 2006, Georgia Tech

 Aircraft fuselage skin panels are joined together by rivets. The initiation and propagation of fatigue cracks in aircraft structures at and around the rivet/skin interface… (more)

Subjects/Keywords: Riveting; Lap joints; Fuselage

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APA (6th Edition):

Atre, A. (2006). A Finite Element and Experimental Investigation on the Fatigue of Riveted Lap Joints in Aircraft Applications. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/10494

Chicago Manual of Style (16th Edition):

Atre, Amarendra. “A Finite Element and Experimental Investigation on the Fatigue of Riveted Lap Joints in Aircraft Applications.” 2006. Doctoral Dissertation, Georgia Tech. Accessed August 18, 2019. http://hdl.handle.net/1853/10494.

MLA Handbook (7th Edition):

Atre, Amarendra. “A Finite Element and Experimental Investigation on the Fatigue of Riveted Lap Joints in Aircraft Applications.” 2006. Web. 18 Aug 2019.

Vancouver:

Atre A. A Finite Element and Experimental Investigation on the Fatigue of Riveted Lap Joints in Aircraft Applications. [Internet] [Doctoral dissertation]. Georgia Tech; 2006. [cited 2019 Aug 18]. Available from: http://hdl.handle.net/1853/10494.

Council of Science Editors:

Atre A. A Finite Element and Experimental Investigation on the Fatigue of Riveted Lap Joints in Aircraft Applications. [Doctoral Dissertation]. Georgia Tech; 2006. Available from: http://hdl.handle.net/1853/10494


Ryerson University

8. Cosentino, Christopher D. Structural repair on a composite aircraft fuselage damaged by fire.

Degree: 2014, Ryerson University

 Composite materials have been used on aircraft for decades with tremendous benefits. Through the use of these advanced materials we have seen a great increase… (more)

Subjects/Keywords: Airplanes  – Fuselage  – Maintenance and repair.; Fibrous composites  – Testing.

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APA (6th Edition):

Cosentino, C. D. (2014). Structural repair on a composite aircraft fuselage damaged by fire. (Thesis). Ryerson University. Retrieved from https://digital.library.ryerson.ca/islandora/object/RULA%3A3280

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):

Cosentino, Christopher D. “Structural repair on a composite aircraft fuselage damaged by fire.” 2014. Thesis, Ryerson University. Accessed August 18, 2019. https://digital.library.ryerson.ca/islandora/object/RULA%3A3280.

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

MLA Handbook (7th Edition):

Cosentino, Christopher D. “Structural repair on a composite aircraft fuselage damaged by fire.” 2014. Web. 18 Aug 2019.

Vancouver:

Cosentino CD. Structural repair on a composite aircraft fuselage damaged by fire. [Internet] [Thesis]. Ryerson University; 2014. [cited 2019 Aug 18]. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A3280.

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

Council of Science Editors:

Cosentino CD. Structural repair on a composite aircraft fuselage damaged by fire. [Thesis]. Ryerson University; 2014. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A3280

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


Lehigh University

9. Fang, Lean. Finite Element Analysis Of A High-Speed Suspension Boat Fuselage.

Degree: MS, Mechanical Engineering, 2017, Lehigh University

 The ongoing suspension boat project at Lehigh University Composites Lab presents new challenges for design since a suspension boat will encounter entirely different loads than… (more)

Subjects/Keywords: Composites; FEA; fuselage design; suspension boat; Mechanical Engineering

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APA (6th Edition):

Fang, L. (2017). Finite Element Analysis Of A High-Speed Suspension Boat Fuselage. (Thesis). Lehigh University. Retrieved from https://preserve.lehigh.edu/etd/2933

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):

Fang, Lean. “Finite Element Analysis Of A High-Speed Suspension Boat Fuselage.” 2017. Thesis, Lehigh University. Accessed August 18, 2019. https://preserve.lehigh.edu/etd/2933.

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

MLA Handbook (7th Edition):

Fang, Lean. “Finite Element Analysis Of A High-Speed Suspension Boat Fuselage.” 2017. Web. 18 Aug 2019.

Vancouver:

Fang L. Finite Element Analysis Of A High-Speed Suspension Boat Fuselage. [Internet] [Thesis]. Lehigh University; 2017. [cited 2019 Aug 18]. Available from: https://preserve.lehigh.edu/etd/2933.

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

Council of Science Editors:

Fang L. Finite Element Analysis Of A High-Speed Suspension Boat Fuselage. [Thesis]. Lehigh University; 2017. Available from: https://preserve.lehigh.edu/etd/2933

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


Drexel University

10. Leone, Frank A Jr. Full-scale testing and progressive damage modeling of sandwich composite aircraft fuselage structure.

Degree: 2010, Drexel University

A comprehensive experimental and computational investigation was conducted to characterize the fracture behavior and structural response of large sandwich composite aircraft fuselage panels containing artificial… (more)

Subjects/Keywords: Mechanical engineering; Airplanes – Fuselage – Materials; Airplanes – Sandwich construction

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APA (6th Edition):

Leone, F. A. J. (2010). Full-scale testing and progressive damage modeling of sandwich composite aircraft fuselage structure. (Thesis). Drexel University. Retrieved from http://hdl.handle.net/1860/3381

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):

Leone, Frank A Jr. “Full-scale testing and progressive damage modeling of sandwich composite aircraft fuselage structure.” 2010. Thesis, Drexel University. Accessed August 18, 2019. http://hdl.handle.net/1860/3381.

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

MLA Handbook (7th Edition):

Leone, Frank A Jr. “Full-scale testing and progressive damage modeling of sandwich composite aircraft fuselage structure.” 2010. Web. 18 Aug 2019.

Vancouver:

Leone FAJ. Full-scale testing and progressive damage modeling of sandwich composite aircraft fuselage structure. [Internet] [Thesis]. Drexel University; 2010. [cited 2019 Aug 18]. Available from: http://hdl.handle.net/1860/3381.

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

Council of Science Editors:

Leone FAJ. Full-scale testing and progressive damage modeling of sandwich composite aircraft fuselage structure. [Thesis]. Drexel University; 2010. Available from: http://hdl.handle.net/1860/3381

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


Delft University of Technology

11. Krakers, L.A. Parametric fuselage design: Integration of mechanics and acoustic & thermal insulation.

Degree: 2009, Delft University of Technology

 Designing a fuselage is a very complex process, which involves many different aspects like strength and stability, fatigue, damage tolerance, fire resistance, thermal and acoustic… (more)

Subjects/Keywords: multidiscipline; parametric; fuselage; DEE

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APA (6th Edition):

Krakers, L. A. (2009). Parametric fuselage design: Integration of mechanics and acoustic & thermal insulation. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:748d5909-dca2-45a3-b04a-31f334223840 ; urn:NBN:nl:ui:24-uuid:748d5909-dca2-45a3-b04a-31f334223840 ; urn:NBN:nl:ui:24-uuid:748d5909-dca2-45a3-b04a-31f334223840 ; http://resolver.tudelft.nl/uuid:748d5909-dca2-45a3-b04a-31f334223840

Chicago Manual of Style (16th Edition):

Krakers, L A. “Parametric fuselage design: Integration of mechanics and acoustic & thermal insulation.” 2009. Doctoral Dissertation, Delft University of Technology. Accessed August 18, 2019. http://resolver.tudelft.nl/uuid:748d5909-dca2-45a3-b04a-31f334223840 ; urn:NBN:nl:ui:24-uuid:748d5909-dca2-45a3-b04a-31f334223840 ; urn:NBN:nl:ui:24-uuid:748d5909-dca2-45a3-b04a-31f334223840 ; http://resolver.tudelft.nl/uuid:748d5909-dca2-45a3-b04a-31f334223840.

MLA Handbook (7th Edition):

Krakers, L A. “Parametric fuselage design: Integration of mechanics and acoustic & thermal insulation.” 2009. Web. 18 Aug 2019.

Vancouver:

Krakers LA. Parametric fuselage design: Integration of mechanics and acoustic & thermal insulation. [Internet] [Doctoral dissertation]. Delft University of Technology; 2009. [cited 2019 Aug 18]. Available from: http://resolver.tudelft.nl/uuid:748d5909-dca2-45a3-b04a-31f334223840 ; urn:NBN:nl:ui:24-uuid:748d5909-dca2-45a3-b04a-31f334223840 ; urn:NBN:nl:ui:24-uuid:748d5909-dca2-45a3-b04a-31f334223840 ; http://resolver.tudelft.nl/uuid:748d5909-dca2-45a3-b04a-31f334223840.

Council of Science Editors:

Krakers LA. Parametric fuselage design: Integration of mechanics and acoustic & thermal insulation. [Doctoral Dissertation]. Delft University of Technology; 2009. Available from: http://resolver.tudelft.nl/uuid:748d5909-dca2-45a3-b04a-31f334223840 ; urn:NBN:nl:ui:24-uuid:748d5909-dca2-45a3-b04a-31f334223840 ; urn:NBN:nl:ui:24-uuid:748d5909-dca2-45a3-b04a-31f334223840 ; http://resolver.tudelft.nl/uuid:748d5909-dca2-45a3-b04a-31f334223840


Brno University of Technology

12. Dula, Jan. Návrh dvoumotorového letounu pro sběrnou dopravu dle předpisu CS-23 .

Degree: 2011, Brno University of Technology

 Cílem diplomové práce je navrhnout letoun pro přepravu cestujících s maximální mírou zachování konstrukčních celků letounu EV-55. Letoun je navržen na základě rozboru požadavků předpisu… (more)

Subjects/Keywords: Kabina cestujících; letoun kategorie Commuter; letoun pro přepravu cestujících; trup; centrážní diagram; obálka zatížení; zatížení trupu; únosnost řezu trupu; Commuter; twin-engined airplane; airplane; fuselage; fuselage stress analysis

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APA (6th Edition):

Dula, J. (2011). Návrh dvoumotorového letounu pro sběrnou dopravu dle předpisu CS-23 . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/2610

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):

Dula, Jan. “Návrh dvoumotorového letounu pro sběrnou dopravu dle předpisu CS-23 .” 2011. Thesis, Brno University of Technology. Accessed August 18, 2019. http://hdl.handle.net/11012/2610.

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

MLA Handbook (7th Edition):

Dula, Jan. “Návrh dvoumotorového letounu pro sběrnou dopravu dle předpisu CS-23 .” 2011. Web. 18 Aug 2019.

Vancouver:

Dula J. Návrh dvoumotorového letounu pro sběrnou dopravu dle předpisu CS-23 . [Internet] [Thesis]. Brno University of Technology; 2011. [cited 2019 Aug 18]. Available from: http://hdl.handle.net/11012/2610.

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

Council of Science Editors:

Dula J. Návrh dvoumotorového letounu pro sběrnou dopravu dle předpisu CS-23 . [Thesis]. Brno University of Technology; 2011. Available from: http://hdl.handle.net/11012/2610

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

13. Constanzo, Fernão de Melo. Análise teórica e experimental da influência da fuselagem sobre a posição do centro aerodinâmico da asa em condições de baixa velocidade.

Degree: Mestrado, Aeronaves, 2009, University of São Paulo

A influência da fuselagem sobre a posição do centro aerodinâmico da asa é complexa e deve ser considerada nos cálculos de equilíbrio e estabilidade estática… (more)

Subjects/Keywords: Aerodynamic center; Aerodynamic interference; Aeronaves; Aircrafts; Centro aerodinâmico; Fuselage influence; Influência da fuselagem; Interferência aerodinâmica

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APA (6th Edition):

Constanzo, F. d. M. (2009). Análise teórica e experimental da influência da fuselagem sobre a posição do centro aerodinâmico da asa em condições de baixa velocidade. (Masters Thesis). University of São Paulo. Retrieved from http://www.teses.usp.br/teses/disponiveis/18/18148/tde-13012011-154655/ ;

Chicago Manual of Style (16th Edition):

Constanzo, Fernão de Melo. “Análise teórica e experimental da influência da fuselagem sobre a posição do centro aerodinâmico da asa em condições de baixa velocidade.” 2009. Masters Thesis, University of São Paulo. Accessed August 18, 2019. http://www.teses.usp.br/teses/disponiveis/18/18148/tde-13012011-154655/ ;.

MLA Handbook (7th Edition):

Constanzo, Fernão de Melo. “Análise teórica e experimental da influência da fuselagem sobre a posição do centro aerodinâmico da asa em condições de baixa velocidade.” 2009. Web. 18 Aug 2019.

Vancouver:

Constanzo FdM. Análise teórica e experimental da influência da fuselagem sobre a posição do centro aerodinâmico da asa em condições de baixa velocidade. [Internet] [Masters thesis]. University of São Paulo; 2009. [cited 2019 Aug 18]. Available from: http://www.teses.usp.br/teses/disponiveis/18/18148/tde-13012011-154655/ ;.

Council of Science Editors:

Constanzo FdM. Análise teórica e experimental da influência da fuselagem sobre a posição do centro aerodinâmico da asa em condições de baixa velocidade. [Masters Thesis]. University of São Paulo; 2009. Available from: http://www.teses.usp.br/teses/disponiveis/18/18148/tde-13012011-154655/ ;


Virginia Tech

14. Pèrez, José G. Energy Absorption and Progressive Failure Response of Composite Fuselage Frames.

Degree: MS, Aerospace and Ocean Engineering, 1999, Virginia Tech

 Vertical drop testing of transport aircraft fuselage sections indicates that the frames play a major role in the process of absorbing the impact energy in… (more)

Subjects/Keywords: Energy Absorption; Braided Composites; Fuselage Frames

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APA (6th Edition):

Pèrez, J. G. (1999). Energy Absorption and Progressive Failure Response of Composite Fuselage Frames. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/34447

Chicago Manual of Style (16th Edition):

Pèrez, José G. “Energy Absorption and Progressive Failure Response of Composite Fuselage Frames.” 1999. Masters Thesis, Virginia Tech. Accessed August 18, 2019. http://hdl.handle.net/10919/34447.

MLA Handbook (7th Edition):

Pèrez, José G. “Energy Absorption and Progressive Failure Response of Composite Fuselage Frames.” 1999. Web. 18 Aug 2019.

Vancouver:

Pèrez JG. Energy Absorption and Progressive Failure Response of Composite Fuselage Frames. [Internet] [Masters thesis]. Virginia Tech; 1999. [cited 2019 Aug 18]. Available from: http://hdl.handle.net/10919/34447.

Council of Science Editors:

Pèrez JG. Energy Absorption and Progressive Failure Response of Composite Fuselage Frames. [Masters Thesis]. Virginia Tech; 1999. Available from: http://hdl.handle.net/10919/34447


Delft University of Technology

15. Şen, I. Aircraft Fuselage Design Study: Parametric Modeling, Structural Analysis, Material Evaluation and Optimization for Aircraft Fuselage:.

Degree: 2010, Delft University of Technology

 The strong search for lightweight materials has become a trend in the aerospace industry. Aircraft manufacturers are responding to this trend and new aerospace materials… (more)

Subjects/Keywords: aircraft design; fuselage design; parametric modeling; structural analysis; optimization; aluminum; Ilhan Sen

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APA (6th Edition):

Şen, I. (2010). Aircraft Fuselage Design Study: Parametric Modeling, Structural Analysis, Material Evaluation and Optimization for Aircraft Fuselage:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:2dbcdb3d-0606-4707-b7ba-6e7ceafd549b

Chicago Manual of Style (16th Edition):

Şen, I. “Aircraft Fuselage Design Study: Parametric Modeling, Structural Analysis, Material Evaluation and Optimization for Aircraft Fuselage:.” 2010. Masters Thesis, Delft University of Technology. Accessed August 18, 2019. http://resolver.tudelft.nl/uuid:2dbcdb3d-0606-4707-b7ba-6e7ceafd549b.

MLA Handbook (7th Edition):

Şen, I. “Aircraft Fuselage Design Study: Parametric Modeling, Structural Analysis, Material Evaluation and Optimization for Aircraft Fuselage:.” 2010. Web. 18 Aug 2019.

Vancouver:

Şen I. Aircraft Fuselage Design Study: Parametric Modeling, Structural Analysis, Material Evaluation and Optimization for Aircraft Fuselage:. [Internet] [Masters thesis]. Delft University of Technology; 2010. [cited 2019 Aug 18]. Available from: http://resolver.tudelft.nl/uuid:2dbcdb3d-0606-4707-b7ba-6e7ceafd549b.

Council of Science Editors:

Şen I. Aircraft Fuselage Design Study: Parametric Modeling, Structural Analysis, Material Evaluation and Optimization for Aircraft Fuselage:. [Masters Thesis]. Delft University of Technology; 2010. Available from: http://resolver.tudelft.nl/uuid:2dbcdb3d-0606-4707-b7ba-6e7ceafd549b


Mississippi State University

16. Simsiriwong, Jutima. STRUCTURAL TESTING OF AN ULTRALIGHT UAV COMPOSITE WING AND FUSELAGE.

Degree: MS, Aerospace Engineering, 2009, Mississippi State University

 The details of an experimental investigation focusing on obtaining the static and vibration characteristics of a full-scale carbon composite wing and fuselage structural assemblies of… (more)

Subjects/Keywords: Wings; Static testing; Vibration analysis; Unmanned aerial vehicles (UAV); Tracking (position); Loads (forces); Accelerometers; Fuselage

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APA (6th Edition):

Simsiriwong, J. (2009). STRUCTURAL TESTING OF AN ULTRALIGHT UAV COMPOSITE WING AND FUSELAGE. (Masters Thesis). Mississippi State University. Retrieved from http://sun.library.msstate.edu/ETD-db/theses/available/etd-04022009-160649/ ;

Chicago Manual of Style (16th Edition):

Simsiriwong, Jutima. “STRUCTURAL TESTING OF AN ULTRALIGHT UAV COMPOSITE WING AND FUSELAGE.” 2009. Masters Thesis, Mississippi State University. Accessed August 18, 2019. http://sun.library.msstate.edu/ETD-db/theses/available/etd-04022009-160649/ ;.

MLA Handbook (7th Edition):

Simsiriwong, Jutima. “STRUCTURAL TESTING OF AN ULTRALIGHT UAV COMPOSITE WING AND FUSELAGE.” 2009. Web. 18 Aug 2019.

Vancouver:

Simsiriwong J. STRUCTURAL TESTING OF AN ULTRALIGHT UAV COMPOSITE WING AND FUSELAGE. [Internet] [Masters thesis]. Mississippi State University; 2009. [cited 2019 Aug 18]. Available from: http://sun.library.msstate.edu/ETD-db/theses/available/etd-04022009-160649/ ;.

Council of Science Editors:

Simsiriwong J. STRUCTURAL TESTING OF AN ULTRALIGHT UAV COMPOSITE WING AND FUSELAGE. [Masters Thesis]. Mississippi State University; 2009. Available from: http://sun.library.msstate.edu/ETD-db/theses/available/etd-04022009-160649/ ;


University of New Mexico

17. Neidigk, Stephen. Detection and characterization of impact damage in carbon fiber aircraft fuselage structure.

Degree: Civil Engineering, 2013, University of New Mexico

 As the use of advanced composite materials continues to grow in the aviation industry, damage detection techniques need to be developed and tested. Impact damage… (more)

Subjects/Keywords: Carbon fiber-reinforced plastics – Fatigue – Measurement; Airplanes – Fuselage – Materials – Fatigue – Measurement; Impact – Measurement.

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APA (6th Edition):

Neidigk, S. (2013). Detection and characterization of impact damage in carbon fiber aircraft fuselage structure. (Masters Thesis). University of New Mexico. Retrieved from http://hdl.handle.net/1928/23289

Chicago Manual of Style (16th Edition):

Neidigk, Stephen. “Detection and characterization of impact damage in carbon fiber aircraft fuselage structure.” 2013. Masters Thesis, University of New Mexico. Accessed August 18, 2019. http://hdl.handle.net/1928/23289.

MLA Handbook (7th Edition):

Neidigk, Stephen. “Detection and characterization of impact damage in carbon fiber aircraft fuselage structure.” 2013. Web. 18 Aug 2019.

Vancouver:

Neidigk S. Detection and characterization of impact damage in carbon fiber aircraft fuselage structure. [Internet] [Masters thesis]. University of New Mexico; 2013. [cited 2019 Aug 18]. Available from: http://hdl.handle.net/1928/23289.

Council of Science Editors:

Neidigk S. Detection and characterization of impact damage in carbon fiber aircraft fuselage structure. [Masters Thesis]. University of New Mexico; 2013. Available from: http://hdl.handle.net/1928/23289

18. Schmidt, R.K. A Semi-Analytical Weight Estimation Method for Oval Fuselages in Novel Aircraft Configurations:.

Degree: 2013, Delft University of Technology

 Research in aircraft design is focusing on novel aircraft configurations in search for a step change in terms of overall transport efficiency. Aircraft design relies… (more)

Subjects/Keywords: class 2.5 weight estimation; oval fuselage; novel aircraft; weight estimation; fuselage; circular fuselage; mdo; first principles; aircraft design; structural analysis

…shown that the fuselage weight is significantly lower in the canard and Prandtl configuration… …designs and a weight estimation is performed on these fuselage to form a basis for future… …x5D; [N/m] [m] Area Stress amplitude Span Width of the fuselage at a… …bending Sectional lift coefficient Plate bending stiffness Diameter of a circular fuselage… …section Height between the top of the fuselage center section and the ceiling Cabin height… 

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APA (6th Edition):

Schmidt, R. K. (2013). A Semi-Analytical Weight Estimation Method for Oval Fuselages in Novel Aircraft Configurations:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:741ac8e3-c4f6-47f8-be74-85bb1fea4cc2

Chicago Manual of Style (16th Edition):

Schmidt, R K. “A Semi-Analytical Weight Estimation Method for Oval Fuselages in Novel Aircraft Configurations:.” 2013. Masters Thesis, Delft University of Technology. Accessed August 18, 2019. http://resolver.tudelft.nl/uuid:741ac8e3-c4f6-47f8-be74-85bb1fea4cc2.

MLA Handbook (7th Edition):

Schmidt, R K. “A Semi-Analytical Weight Estimation Method for Oval Fuselages in Novel Aircraft Configurations:.” 2013. Web. 18 Aug 2019.

Vancouver:

Schmidt RK. A Semi-Analytical Weight Estimation Method for Oval Fuselages in Novel Aircraft Configurations:. [Internet] [Masters thesis]. Delft University of Technology; 2013. [cited 2019 Aug 18]. Available from: http://resolver.tudelft.nl/uuid:741ac8e3-c4f6-47f8-be74-85bb1fea4cc2.

Council of Science Editors:

Schmidt RK. A Semi-Analytical Weight Estimation Method for Oval Fuselages in Novel Aircraft Configurations:. [Masters Thesis]. Delft University of Technology; 2013. Available from: http://resolver.tudelft.nl/uuid:741ac8e3-c4f6-47f8-be74-85bb1fea4cc2

19. Alarie, Nicolas. Conception d’un fuselage en composites pour le Symphony SA-160.

Degree: M. Sc. A., Génie mécanique, 2015, Université de Sherbrooke

 Le SA-160 est un avion monomoteur biplace dont le fuselage est constitué d’un châssis en tubulure d’acier recouvert d’une peau en composites non structurale. Quoi… (more)

Subjects/Keywords: Fuselage; Matériaux composites; Structure d’avion; Caractérisation des matériaux; Procédés de fabrication; Joint collé; Fibres de carbone; Certification aéronautique

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APA (6th Edition):

Alarie, N. (2015). Conception d’un fuselage en composites pour le Symphony SA-160. (Masters Thesis). Université de Sherbrooke. Retrieved from http://www.collectionscanada.gc.ca/obj/thesescanada/vol2/QSHERU/TC-QSHERU-11143_7724.pdf ; http://savoirs.usherbrooke.ca/bitstream/11143/7724/1/Alarie_Nicolas_MScA_2013.pdf

Chicago Manual of Style (16th Edition):

Alarie, Nicolas. “Conception d’un fuselage en composites pour le Symphony SA-160.” 2015. Masters Thesis, Université de Sherbrooke. Accessed August 18, 2019. http://www.collectionscanada.gc.ca/obj/thesescanada/vol2/QSHERU/TC-QSHERU-11143_7724.pdf ; http://savoirs.usherbrooke.ca/bitstream/11143/7724/1/Alarie_Nicolas_MScA_2013.pdf.

MLA Handbook (7th Edition):

Alarie, Nicolas. “Conception d’un fuselage en composites pour le Symphony SA-160.” 2015. Web. 18 Aug 2019.

Vancouver:

Alarie N. Conception d’un fuselage en composites pour le Symphony SA-160. [Internet] [Masters thesis]. Université de Sherbrooke; 2015. [cited 2019 Aug 18]. Available from: http://www.collectionscanada.gc.ca/obj/thesescanada/vol2/QSHERU/TC-QSHERU-11143_7724.pdf ; http://savoirs.usherbrooke.ca/bitstream/11143/7724/1/Alarie_Nicolas_MScA_2013.pdf.

Council of Science Editors:

Alarie N. Conception d’un fuselage en composites pour le Symphony SA-160. [Masters Thesis]. Université de Sherbrooke; 2015. Available from: http://www.collectionscanada.gc.ca/obj/thesescanada/vol2/QSHERU/TC-QSHERU-11143_7724.pdf ; http://savoirs.usherbrooke.ca/bitstream/11143/7724/1/Alarie_Nicolas_MScA_2013.pdf


Ryerson University

20. Isaacs, Romeo. Bonded-bolted combination repair of a composite fuselage section.

Degree: 2017, Ryerson University

 Composite repair is an area of great importance, especially in the aerospace industry, due to the fact that an increasing number of modern aircrafts are… (more)

Subjects/Keywords: Airplanes  – Maintenance and repair  – Materials; Airplanes  – Maintenance and repair; Strains and stresses; Dead loads (Mechanics); Composite materials  – Bonding; Airplanes  – Fuselage

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APA (6th Edition):

Isaacs, R. (2017). Bonded-bolted combination repair of a composite fuselage section. (Thesis). Ryerson University. Retrieved from https://digital.library.ryerson.ca/islandora/object/RULA%3A6773

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):

Isaacs, Romeo. “Bonded-bolted combination repair of a composite fuselage section.” 2017. Thesis, Ryerson University. Accessed August 18, 2019. https://digital.library.ryerson.ca/islandora/object/RULA%3A6773.

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

MLA Handbook (7th Edition):

Isaacs, Romeo. “Bonded-bolted combination repair of a composite fuselage section.” 2017. Web. 18 Aug 2019.

Vancouver:

Isaacs R. Bonded-bolted combination repair of a composite fuselage section. [Internet] [Thesis]. Ryerson University; 2017. [cited 2019 Aug 18]. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A6773.

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

Council of Science Editors:

Isaacs R. Bonded-bolted combination repair of a composite fuselage section. [Thesis]. Ryerson University; 2017. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A6773

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


Université de Sherbrooke

21. Alarie, Nicolas. Conception d’un fuselage en composites pour le Symphony SA-160 .

Degree: 2015, Université de Sherbrooke

 Le SA-160 est un avion monomoteur biplace dont le fuselage est constitué d’un châssis en tubulure d’acier recouvert d’une peau en composites non structurale. Quoi… (more)

Subjects/Keywords: Fuselage; Matériaux composites; Structure d’avion; Caractérisation des matériaux; Procédés de fabrication; Joint collé; Fibres de carbone; Certification aéronautique

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APA (6th Edition):

Alarie, N. (2015). Conception d’un fuselage en composites pour le Symphony SA-160 . (Masters Thesis). Université de Sherbrooke. Retrieved from http://hdl.handle.net/11143/7724

Chicago Manual of Style (16th Edition):

Alarie, Nicolas. “Conception d’un fuselage en composites pour le Symphony SA-160 .” 2015. Masters Thesis, Université de Sherbrooke. Accessed August 18, 2019. http://hdl.handle.net/11143/7724.

MLA Handbook (7th Edition):

Alarie, Nicolas. “Conception d’un fuselage en composites pour le Symphony SA-160 .” 2015. Web. 18 Aug 2019.

Vancouver:

Alarie N. Conception d’un fuselage en composites pour le Symphony SA-160 . [Internet] [Masters thesis]. Université de Sherbrooke; 2015. [cited 2019 Aug 18]. Available from: http://hdl.handle.net/11143/7724.

Council of Science Editors:

Alarie N. Conception d’un fuselage en composites pour le Symphony SA-160 . [Masters Thesis]. Université de Sherbrooke; 2015. Available from: http://hdl.handle.net/11143/7724


Virginia Tech

22. Pilkington, Lawrence O. Impact Response and Failure of a Textile Composite Fuselage Frame.

Degree: MS, Aerospace and Ocean Engineering, 2004, Virginia Tech

 Impact tests are performed on two circular circumferential frame segments using a drop tower apparatus. These frames have a nominal radius of 120 inches, a… (more)

Subjects/Keywords: textile composite; impact response; dynamic response; fuselage

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APA (6th Edition):

Pilkington, L. O. (2004). Impact Response and Failure of a Textile Composite Fuselage Frame. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/10059

Chicago Manual of Style (16th Edition):

Pilkington, Lawrence O. “Impact Response and Failure of a Textile Composite Fuselage Frame.” 2004. Masters Thesis, Virginia Tech. Accessed August 18, 2019. http://hdl.handle.net/10919/10059.

MLA Handbook (7th Edition):

Pilkington, Lawrence O. “Impact Response and Failure of a Textile Composite Fuselage Frame.” 2004. Web. 18 Aug 2019.

Vancouver:

Pilkington LO. Impact Response and Failure of a Textile Composite Fuselage Frame. [Internet] [Masters thesis]. Virginia Tech; 2004. [cited 2019 Aug 18]. Available from: http://hdl.handle.net/10919/10059.

Council of Science Editors:

Pilkington LO. Impact Response and Failure of a Textile Composite Fuselage Frame. [Masters Thesis]. Virginia Tech; 2004. Available from: http://hdl.handle.net/10919/10059


Drexel University

23. Mosinyi, Bao Rasebolai. Fatigue damage assessment of high-usage in-service aircraft fuselage structure.

Degree: 2007, Drexel University

 As the commercial and military aircraft fleets continue to age, there is a growing concern that multiple-site damage (MSD) can compromise structural integrity. Multiple site… (more)

Subjects/Keywords: Mechanical engineering; Airframes – Fatigue; Airplanes – Fuselage – Materials

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APA (6th Edition):

Mosinyi, B. R. (2007). Fatigue damage assessment of high-usage in-service aircraft fuselage structure. (Thesis). Drexel University. Retrieved from http://hdl.handle.net/1860/2762

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):

Mosinyi, Bao Rasebolai. “Fatigue damage assessment of high-usage in-service aircraft fuselage structure.” 2007. Thesis, Drexel University. Accessed August 18, 2019. http://hdl.handle.net/1860/2762.

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

MLA Handbook (7th Edition):

Mosinyi, Bao Rasebolai. “Fatigue damage assessment of high-usage in-service aircraft fuselage structure.” 2007. Web. 18 Aug 2019.

Vancouver:

Mosinyi BR. Fatigue damage assessment of high-usage in-service aircraft fuselage structure. [Internet] [Thesis]. Drexel University; 2007. [cited 2019 Aug 18]. Available from: http://hdl.handle.net/1860/2762.

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

Council of Science Editors:

Mosinyi BR. Fatigue damage assessment of high-usage in-service aircraft fuselage structure. [Thesis]. Drexel University; 2007. Available from: http://hdl.handle.net/1860/2762

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


Delft University of Technology

24. Shroff, S. Design, Analysis, Fabrication and Testing of Grid-Stiffened for Fuselage Applications.

Degree: 2014, Delft University of Technology

 The application of composites in aircraft structures has grown significantly in the past decade, and an increase in this growth in application has recently been… (more)

Subjects/Keywords: grid stiffened; composite fuselage; composite joint; progressive damage

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APA (6th Edition):

Shroff, S. (2014). Design, Analysis, Fabrication and Testing of Grid-Stiffened for Fuselage Applications. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:9993bf69-5a8d-4b50-816e-f685185cea64 ; urn:NBN:nl:ui:24-uuid:9993bf69-5a8d-4b50-816e-f685185cea64 ; urn:NBN:nl:ui:24-uuid:9993bf69-5a8d-4b50-816e-f685185cea64 ; http://resolver.tudelft.nl/uuid:9993bf69-5a8d-4b50-816e-f685185cea64

Chicago Manual of Style (16th Edition):

Shroff, S. “Design, Analysis, Fabrication and Testing of Grid-Stiffened for Fuselage Applications.” 2014. Doctoral Dissertation, Delft University of Technology. Accessed August 18, 2019. http://resolver.tudelft.nl/uuid:9993bf69-5a8d-4b50-816e-f685185cea64 ; urn:NBN:nl:ui:24-uuid:9993bf69-5a8d-4b50-816e-f685185cea64 ; urn:NBN:nl:ui:24-uuid:9993bf69-5a8d-4b50-816e-f685185cea64 ; http://resolver.tudelft.nl/uuid:9993bf69-5a8d-4b50-816e-f685185cea64.

MLA Handbook (7th Edition):

Shroff, S. “Design, Analysis, Fabrication and Testing of Grid-Stiffened for Fuselage Applications.” 2014. Web. 18 Aug 2019.

Vancouver:

Shroff S. Design, Analysis, Fabrication and Testing of Grid-Stiffened for Fuselage Applications. [Internet] [Doctoral dissertation]. Delft University of Technology; 2014. [cited 2019 Aug 18]. Available from: http://resolver.tudelft.nl/uuid:9993bf69-5a8d-4b50-816e-f685185cea64 ; urn:NBN:nl:ui:24-uuid:9993bf69-5a8d-4b50-816e-f685185cea64 ; urn:NBN:nl:ui:24-uuid:9993bf69-5a8d-4b50-816e-f685185cea64 ; http://resolver.tudelft.nl/uuid:9993bf69-5a8d-4b50-816e-f685185cea64.

Council of Science Editors:

Shroff S. Design, Analysis, Fabrication and Testing of Grid-Stiffened for Fuselage Applications. [Doctoral Dissertation]. Delft University of Technology; 2014. Available from: http://resolver.tudelft.nl/uuid:9993bf69-5a8d-4b50-816e-f685185cea64 ; urn:NBN:nl:ui:24-uuid:9993bf69-5a8d-4b50-816e-f685185cea64 ; urn:NBN:nl:ui:24-uuid:9993bf69-5a8d-4b50-816e-f685185cea64 ; http://resolver.tudelft.nl/uuid:9993bf69-5a8d-4b50-816e-f685185cea64


Linköping University

25. Johansson, Helena. Investigation of rotor downwash effects using CFD.

Degree: Electrical Engineering, 2009, Linköping University

  This paper is the result of a master thesis project on helicopter rotor downwash effects using computational fluid dynamics (CFD). The work was performed… (more)

Subjects/Keywords: Helicopter; Momentum Theory; Blade Element Theory; CFD; Rotor-Fuselage Interaction; Simulation; LQ controller; Automatic control; Reglerteknik

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APA (6th Edition):

Johansson, H. (2009). Investigation of rotor downwash effects using CFD. (Thesis). Linköping University. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-17651

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):

Johansson, Helena. “Investigation of rotor downwash effects using CFD.” 2009. Thesis, Linköping University. Accessed August 18, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-17651.

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

MLA Handbook (7th Edition):

Johansson, Helena. “Investigation of rotor downwash effects using CFD.” 2009. Web. 18 Aug 2019.

Vancouver:

Johansson H. Investigation of rotor downwash effects using CFD. [Internet] [Thesis]. Linköping University; 2009. [cited 2019 Aug 18]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-17651.

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

Council of Science Editors:

Johansson H. Investigation of rotor downwash effects using CFD. [Thesis]. Linköping University; 2009. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-17651

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


Brno University of Technology

26. Pělucha, Jiří. Výpočet zatížení kluzáku HPH 2 Twin Shark .

Degree: 2010, Brno University of Technology

 Cílem diplomové práce je stanovení zatížení pro pevnostní výpočty kluzáku HPH 2 Twin Shark podle kategorie CS-22. V práci je stanoveno zatížení křídla, ocasních ploch,… (more)

Subjects/Keywords: Kluzák; manévrovací a poryvová obálka; zatížení; křídlo; ocasní plochy; trup; podvozek.; Glider; manoeuvre and gust envelope; loading; wing; tail; fuselage; undercarriage.

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

APA (6th Edition):

Pělucha, J. (2010). Výpočet zatížení kluzáku HPH 2 Twin Shark . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/1575

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):

Pělucha, Jiří. “Výpočet zatížení kluzáku HPH 2 Twin Shark .” 2010. Thesis, Brno University of Technology. Accessed August 18, 2019. http://hdl.handle.net/11012/1575.

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

MLA Handbook (7th Edition):

Pělucha, Jiří. “Výpočet zatížení kluzáku HPH 2 Twin Shark .” 2010. Web. 18 Aug 2019.

Vancouver:

Pělucha J. Výpočet zatížení kluzáku HPH 2 Twin Shark . [Internet] [Thesis]. Brno University of Technology; 2010. [cited 2019 Aug 18]. Available from: http://hdl.handle.net/11012/1575.

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

Council of Science Editors:

Pělucha J. Výpočet zatížení kluzáku HPH 2 Twin Shark . [Thesis]. Brno University of Technology; 2010. Available from: http://hdl.handle.net/11012/1575

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


Brno University of Technology

27. Trusík, Vojtěch. Aerodynamická analýza a optimalizace konfigurace letounu TL-4000 .

Degree: 2014, Brno University of Technology

 Tato diplomová práce se zabývá aerodynamickou analýzou 3D konfigurace letounu TL – 4000 a provedením tvarových úprav za účelem zlepšení letových výkonů. Úpravy jsou zaměřeny… (more)

Subjects/Keywords: Aerodynamika; analýza; optimalizace; Fluent; CFD; přechod křídlo – trup.; Aerodynamics; analysis; optimization; Fluent; CFD; wing – fuselage junction.

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

APA (6th Edition):

Trusík, V. (2014). Aerodynamická analýza a optimalizace konfigurace letounu TL-4000 . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/34026

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):

Trusík, Vojtěch. “Aerodynamická analýza a optimalizace konfigurace letounu TL-4000 .” 2014. Thesis, Brno University of Technology. Accessed August 18, 2019. http://hdl.handle.net/11012/34026.

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

MLA Handbook (7th Edition):

Trusík, Vojtěch. “Aerodynamická analýza a optimalizace konfigurace letounu TL-4000 .” 2014. Web. 18 Aug 2019.

Vancouver:

Trusík V. Aerodynamická analýza a optimalizace konfigurace letounu TL-4000 . [Internet] [Thesis]. Brno University of Technology; 2014. [cited 2019 Aug 18]. Available from: http://hdl.handle.net/11012/34026.

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

Council of Science Editors:

Trusík V. Aerodynamická analýza a optimalizace konfigurace letounu TL-4000 . [Thesis]. Brno University of Technology; 2014. Available from: http://hdl.handle.net/11012/34026

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


Brno University of Technology

28. Zamazal, Jakub. Návrh rekonstrukce střední části trupu letounu Z 143 náhradou za poloskořepinu .

Degree: 2017, Brno University of Technology

 Diplomová práce se zabývá rekonstrukcí střední části trupu letounu Z 143 z příhradové konstrukce na konstrukci poloskořepinovou. V práci je proveden koncepční návrh poloskořepinové střední… (more)

Subjects/Keywords: trup; centroplán; hmotový rozbor; poloskořepinová konstrukce; centráž; fuselage; centre wing; weight analysis; semi-monocoque frame; center of gravity

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

APA (6th Edition):

Zamazal, J. (2017). Návrh rekonstrukce střední části trupu letounu Z 143 náhradou za poloskořepinu . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/65978

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):

Zamazal, Jakub. “Návrh rekonstrukce střední části trupu letounu Z 143 náhradou za poloskořepinu .” 2017. Thesis, Brno University of Technology. Accessed August 18, 2019. http://hdl.handle.net/11012/65978.

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

MLA Handbook (7th Edition):

Zamazal, Jakub. “Návrh rekonstrukce střední části trupu letounu Z 143 náhradou za poloskořepinu .” 2017. Web. 18 Aug 2019.

Vancouver:

Zamazal J. Návrh rekonstrukce střední části trupu letounu Z 143 náhradou za poloskořepinu . [Internet] [Thesis]. Brno University of Technology; 2017. [cited 2019 Aug 18]. Available from: http://hdl.handle.net/11012/65978.

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

Council of Science Editors:

Zamazal J. Návrh rekonstrukce střední části trupu letounu Z 143 náhradou za poloskořepinu . [Thesis]. Brno University of Technology; 2017. Available from: http://hdl.handle.net/11012/65978

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


Brno University of Technology

29. Derevjanik, Šimon. Aerodynamická analýza a návh úprav přechodu křídlo-trup letounu L 410 NG .

Degree: 2013, Brno University of Technology

 Táto diplomová práca sa zaoberá CFD analýzou prechodových krytov letúna L 410 NG a návrhom úprav. Kalibračná úloha riešená v úvodnej časti slúži ako prostriedok… (more)

Subjects/Keywords: CFD; L 410 NG; optimalizácia; analýza prúdenia; prechodový kryt krídlo – trup; CFD; L 410 NG; optimization; flow analysis; wing-fuselage junction

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

APA (6th Edition):

Derevjanik, . (2013). Aerodynamická analýza a návh úprav přechodu křídlo-trup letounu L 410 NG . (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/25704

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):

Derevjanik, Šimon. “Aerodynamická analýza a návh úprav přechodu křídlo-trup letounu L 410 NG .” 2013. Thesis, Brno University of Technology. Accessed August 18, 2019. http://hdl.handle.net/11012/25704.

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

MLA Handbook (7th Edition):

Derevjanik, Šimon. “Aerodynamická analýza a návh úprav přechodu křídlo-trup letounu L 410 NG .” 2013. Web. 18 Aug 2019.

Vancouver:

Derevjanik . Aerodynamická analýza a návh úprav přechodu křídlo-trup letounu L 410 NG . [Internet] [Thesis]. Brno University of Technology; 2013. [cited 2019 Aug 18]. Available from: http://hdl.handle.net/11012/25704.

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

Council of Science Editors:

Derevjanik . Aerodynamická analýza a návh úprav přechodu křídlo-trup letounu L 410 NG . [Thesis]. Brno University of Technology; 2013. Available from: http://hdl.handle.net/11012/25704

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

30. Mazella, Ivan José de Godoy. Sobre metodologias de modelagem computacional de propagação de trincas por fadiga em fuselagens aeronáuticas.

Degree: PhD, Engenharia de Estruturas, 2007, University of São Paulo

Uma metodologia para simular o crescimento de trincas por fadiga em estruturas pressurizadas de cascas delgadas e enrijecidas é implementada por meio de uma estrutura… (more)

Subjects/Keywords: Aircraft fuselage; Cascas delgadas; Fadiga em estruturas; Finite element method; Fracture of structures; Fratura das estruturas; Fuselagem; Método dos elementos finitos; Structural fatigue; Thin shells

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

APA (6th Edition):

Mazella, I. J. d. G. (2007). Sobre metodologias de modelagem computacional de propagação de trincas por fadiga em fuselagens aeronáuticas. (Doctoral Dissertation). University of São Paulo. Retrieved from http://www.teses.usp.br/teses/disponiveis/3/3144/tde-06072007-151257/ ;

Chicago Manual of Style (16th Edition):

Mazella, Ivan José de Godoy. “Sobre metodologias de modelagem computacional de propagação de trincas por fadiga em fuselagens aeronáuticas.” 2007. Doctoral Dissertation, University of São Paulo. Accessed August 18, 2019. http://www.teses.usp.br/teses/disponiveis/3/3144/tde-06072007-151257/ ;.

MLA Handbook (7th Edition):

Mazella, Ivan José de Godoy. “Sobre metodologias de modelagem computacional de propagação de trincas por fadiga em fuselagens aeronáuticas.” 2007. Web. 18 Aug 2019.

Vancouver:

Mazella IJdG. Sobre metodologias de modelagem computacional de propagação de trincas por fadiga em fuselagens aeronáuticas. [Internet] [Doctoral dissertation]. University of São Paulo; 2007. [cited 2019 Aug 18]. Available from: http://www.teses.usp.br/teses/disponiveis/3/3144/tde-06072007-151257/ ;.

Council of Science Editors:

Mazella IJdG. Sobre metodologias de modelagem computacional de propagação de trincas por fadiga em fuselagens aeronáuticas. [Doctoral Dissertation]. University of São Paulo; 2007. Available from: http://www.teses.usp.br/teses/disponiveis/3/3144/tde-06072007-151257/ ;

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