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dc.contributor.authorPatil, Ankur Santaji
dc.contributor.authorArnold, Emily J.
dc.date.accessioned2019-11-25T23:22:59Z
dc.date.available2019-11-25T23:22:59Z
dc.date.issued2018-07-02
dc.identifier.citationAnkur S. Patil and Emily J. Arnold, “Sensor-Driven Preliminary Wing Ground Plane Sizing Approach and Applications,” International Journal of Aerospace Engineering, vol. 2018, Article ID 6378635, 15 pages, 2018. https://doi.org/10.1155/2018/6378635.en_US
dc.identifier.urihttp://hdl.handle.net/1808/29812
dc.descriptionThis work is licensed under a Creative Commons Attribution 4.0 International License.en_US
dc.description.abstractStructurally integrated antenna arrays provide synergies allowing the integration of large apertures onto airborne platforms. However, the surrounding airframe can greatly impact the performance of the antenna array. This paper presents a sensor-driven preliminary wing ground plane sizing approach to provide insight into the implications of design decisions on payload performance. The improvement of a wing-integrated antenna array that utilizes the wing as a ground plane motivated this study. Relationships for wing span, wing chord, and thickness are derived from extensive parametric electromagnetic simulations based on optimum antenna performance. It is expected that these equations would be used after an initial wing-loading design point has been selected to provide the designer guidance into how various wing parameters might affect the integrated antenna performance.en_US
dc.publisherHindawien_US
dc.rightsCopyright © 2018 Ankur S. Patil and Emily J. Arnold. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.en_US
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/en_US
dc.titleSensor driven preliminary wing-ground plane sizing approach and applicationsen_US
dc.typeArticleen_US
kusw.kuauthorPatil, Ankur Santaji
kusw.kuauthorArnold, Emily J.
kusw.kudepartmentAerospace Engineeringen_US
dc.identifier.doi10.1155/2018/6378635en_US
dc.identifier.orcidhttps://orcid.org/0000-0002-4114-7012en_US
dc.identifier.orcidhttps://orcid.org/0000-0002-4427-6362en_US
kusw.oaversionScholarly/refereed, publisher versionen_US
kusw.oapolicyThis item meets KU Open Access policy criteria.en_US
dc.rights.accessrightsopenAccessen_US


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Copyright © 2018 Ankur S. Patil and Emily J. Arnold. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
Except where otherwise noted, this item's license is described as: Copyright © 2018 Ankur S. Patil and Emily J. Arnold. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.