Please use this identifier to cite or link to this item: https://doi.org/10.21256/zhaw-4058
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dc.contributor.authorSteinegger, Rolf-
dc.date.accessioned2017-12-19T16:10:57Z-
dc.date.available2017-12-19T16:10:57Z-
dc.date.issued2017-04-26-
dc.identifier.urihttps://digitalcollection.zhaw.ch/handle/11475/1901-
dc.description.abstractA comparison of lifted weight as a function of altitude and depth reveals big differences by a factor of about 3’000 in total from 11 km above sea level to 10 km below sea level, divided into factors of: ~   4 between summit and sea level, ~   400 between flying close to the ground and planing on water, ~   2 between planing on water and in a fully submerged state. The most dramatic changes are due to different fluids and levels of altitude. The most interesting sector to discuss lift is close to sea level: aircraft approaching the ground, plates planing on water and hydrofoils only barely submerged in water. There is one basic similarity across of these: Almost any shape, as long as it is not too thick, will work as an (air)foil and produce lift when the angle of attack is in the right range.de_CH
dc.format.extent10de_CH
dc.language.isoende_CH
dc.publisherZHAW Zürcher Hochschule für Angewandte Wissenschaftende_CH
dc.rightsNot specifiedde_CH
dc.subjectSurfboardde_CH
dc.subjectLiftde_CH
dc.subjectHydrofoilde_CH
dc.subjectAirfoilde_CH
dc.subjectLifted weightde_CH
dc.subject.ddc620: Ingenieurwesende_CH
dc.titleFrom summit to seafloor : lifted weight as a function of altitude and depthde_CH
dc.typeWorking Paper – Gutachten – Studiede_CH
dc.typeTextde_CH
zhaw.departementSchool of Engineeringde_CH
zhaw.organisationalunitZentrum für Aviatik (ZAV)de_CH
zhaw.publisher.placeWinterthurde_CH
dc.identifier.doi10.21256/zhaw-4058de_CH
zhaw.funding.euNode_CH
zhaw.originated.zhawYesde_CH
Appears in Collections:Publikationen School of Engineering

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