Modeling and analysis of a maneuvering aircraft and cable towed body with wake effects
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2010. === Cataloged from PDF version of thesis. === Includes bibliographical references (p. 105-107). === This thesis report covers the analysis and modeling of a cable towed endbody that incorporates an air...
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ndltd-MIT-oai-dspace.mit.edu-1721.1-596712019-05-02T15:37:19Z Modeling and analysis of a maneuvering aircraft and cable towed body with wake effects Hall, Jacob Thomas Jaurne Peraire and Eric Burcsu. Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Aeronautics and Astronautics. Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2010. Cataloged from PDF version of thesis. Includes bibliographical references (p. 105-107). This thesis report covers the analysis and modeling of a cable towed endbody that incorporates an aircraft, wake effects, a towline, and a tow body. The aircraft is modeled as a generic tactical aircraft which is able to conduct maneuvers. The towline is treated as an elastic cable that connects the aircraft and endbody while also being affected by the aircraft wake. The endbody is treated as a simple drag sphere with allocation to continue to various shapes and sizes. A parametric study is conducted which highlights the effect of changing the parameters of towline material, length, and load factor. Three maneuvers are conducted including a turn and acceleration. The results show that longer cable lengths, those of 500 m or greater, exhibit little response to the addition of a trailing wake. However, shorter cables are affected, especially during the turn and climb maneuvers. A 50 m cable experiences an extra 8m deflection when compared to a wake-less example. During the climb maneuver, it is shown that an endbody may pass ahead of the towing aircraft, as well as above it. The effect of changing cable material is shown to be minimal, with small differences expected due to the difference in cable mass. by Jacob Thomas Hall. S.M. 2010-10-29T18:08:02Z 2010-10-29T18:08:02Z 2010 2010 Thesis http://hdl.handle.net/1721.1/59671 668211624 eng M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission. http://dspace.mit.edu/handle/1721.1/7582 107 p. application/pdf Massachusetts Institute of Technology |
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Aeronautics and Astronautics. Hall, Jacob Thomas Modeling and analysis of a maneuvering aircraft and cable towed body with wake effects |
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Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2010. === Cataloged from PDF version of thesis. === Includes bibliographical references (p. 105-107). === This thesis report covers the analysis and modeling of a cable towed endbody that incorporates an aircraft, wake effects, a towline, and a tow body. The aircraft is modeled as a generic tactical aircraft which is able to conduct maneuvers. The towline is treated as an elastic cable that connects the aircraft and endbody while also being affected by the aircraft wake. The endbody is treated as a simple drag sphere with allocation to continue to various shapes and sizes. A parametric study is conducted which highlights the effect of changing the parameters of towline material, length, and load factor. Three maneuvers are conducted including a turn and acceleration. The results show that longer cable lengths, those of 500 m or greater, exhibit little response to the addition of a trailing wake. However, shorter cables are affected, especially during the turn and climb maneuvers. A 50 m cable experiences an extra 8m deflection when compared to a wake-less example. During the climb maneuver, it is shown that an endbody may pass ahead of the towing aircraft, as well as above it. The effect of changing cable material is shown to be minimal, with small differences expected due to the difference in cable mass. === by Jacob Thomas Hall. === S.M. |
author2 |
Jaurne Peraire and Eric Burcsu. |
author_facet |
Jaurne Peraire and Eric Burcsu. Hall, Jacob Thomas |
author |
Hall, Jacob Thomas |
author_sort |
Hall, Jacob Thomas |
title |
Modeling and analysis of a maneuvering aircraft and cable towed body with wake effects |
title_short |
Modeling and analysis of a maneuvering aircraft and cable towed body with wake effects |
title_full |
Modeling and analysis of a maneuvering aircraft and cable towed body with wake effects |
title_fullStr |
Modeling and analysis of a maneuvering aircraft and cable towed body with wake effects |
title_full_unstemmed |
Modeling and analysis of a maneuvering aircraft and cable towed body with wake effects |
title_sort |
modeling and analysis of a maneuvering aircraft and cable towed body with wake effects |
publisher |
Massachusetts Institute of Technology |
publishDate |
2010 |
url |
http://hdl.handle.net/1721.1/59671 |
work_keys_str_mv |
AT halljacobthomas modelingandanalysisofamaneuveringaircraftandcabletowedbodywithwakeeffects |
_version_ |
1719025007078670336 |