dc.contributor.author | Guttag, Mark Andrew | |
dc.contributor.author | Reis, Pedro Miguel | |
dc.date.accessioned | 2018-03-27T15:43:15Z | |
dc.date.available | 2018-03-27T15:43:15Z | |
dc.date.issued | 2017-12 | |
dc.date.submitted | 2017-02 | |
dc.identifier.issn | 2469-990X | |
dc.identifier.issn | 2469-9918 | |
dc.identifier.uri | http://hdl.handle.net/1721.1/114398 | |
dc.description.abstract | We study a mechanism for active aerodynamic drag reduction on morphable grooved cylinders, whose topography can be modified pneumatically. Our design is inspired by the morphology of the Saguaro cactus (Carnegiea gigantea), which possesses an array of axial grooves, thought to help reduce aerodynamic drag, thereby enhancing the structural robustness of the plant under wind loading. Our analog experimental samples comprise a spoked rigid skeleton with axial cavities, covered by a stretched elastomeric film. Decreasing the inner pressure of the sample produces axial grooves, whose depth can be accurately varied, on demand. First, we characterize the relation between groove depth and pneumatic loading through a combination of precision mechanical experiments and finite element simulations. Second, wind tunnel tests are used to measure the aerodynamic drag coefficient (as a function of Reynolds number) of the grooved samples, with different levels of periodicity and groove depths. We focus specifically on the drag crisis and systematically measure the associated minimum drag coefficient and the critical Reynolds number at which it occurs. The results are in agreement with the classic literature of rough cylinders, albeit with an unprecedented level of precision and resolution in varying topography using a single sample. Finally, we leverage the morphable nature of our system to dynamically reduce drag for varying aerodynamic loading conditions. We demonstrate that actively controlling the groove depth yields a drag coefficient that decreases monotonically with Reynolds number and is significantly lower than the fixed sample counterparts. These findings open the possibility for the drag reduction of grooved cylinders to be operated over a wide range of flow conditions. | en_US |
dc.description.sponsorship | National Science Foundation (U.S.) (CAREER CMMI-1351449) | en_US |
dc.publisher | American Physical Society | en_US |
dc.relation.isversionof | http://dx.doi.org/10.1103/PhysRevFluids.2.123903 | en_US |
dc.rights | Article is made available in accordance with the publisher's policy and may be subject to US copyright law. Please refer to the publisher's site for terms of use. | en_US |
dc.source | American Physical Society | en_US |
dc.title | Active aerodynamic drag reduction on morphable cylinders | en_US |
dc.type | Article | en_US |
dc.identifier.citation | Guttag, M. and P. M. Reis. "Active aerodynamic drag reduction on morphable cylinders." Physical Review Fluids 2, 12 (December 2017): 123903 © 2017 American Physical Society | en_US |
dc.contributor.department | Massachusetts Institute of Technology. Department of Civil and Environmental Engineering | en_US |
dc.contributor.department | Massachusetts Institute of Technology. Department of Mechanical Engineering | en_US |
dc.contributor.mitauthor | Guttag, Mark Andrew | |
dc.contributor.mitauthor | Reis, Pedro Miguel | |
dc.relation.journal | Physical Review Fluids | en_US |
dc.eprint.version | Final published version | en_US |
dc.type.uri | http://purl.org/eprint/type/JournalArticle | en_US |
eprint.status | http://purl.org/eprint/status/PeerReviewed | en_US |
dc.date.updated | 2018-02-07T20:55:52Z | |
dc.language.rfc3066 | en | |
dc.rights.holder | American Physical Society | |
dspace.orderedauthors | Guttag, M.; Reis, P. M. | en_US |
dspace.embargo.terms | N | en_US |
dc.identifier.orcid | https://orcid.org/0000-0002-0703-4989 | |
dc.identifier.orcid | https://orcid.org/0000-0003-3984-828X | |
mit.license | PUBLISHER_POLICY | en_US |