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pro vyhledávání: '"Marpu, Ritu"'
Autor:
Marpu, Ritu Priyanka
Helicopters in forward flight experience complex aerodynamic phenomena to various degrees. In low speed level flight, the vortex wake remains close to the rotor disk and interacts with the rotor blades to give rise to blade vortex interaction phenome
Externí odkaz:
http://hdl.handle.net/1853/47661
Autor:
Marpu, Ritu, Sankar, Lakshmi
A subset of the US-Army/NASA wind tunnel tests of a full-scale UH-60A Black-Hawk rotor system have been modeled using a Hybrid Navier-Stokes - Free Wake methodology, loosely coupled to a multi-body dynamics analysis. Results for rotor performance, ae
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::368b817dd248716ce3b196eebcc20c49
Autor:
Marpu, Ritu, Sankar, Lakshmi
A Hybrid Navier-Stokes Free-Wake Computational Fluid Dynamics (CFD) methodology, coupled with a multi-body dynamics analysis code, has been applied to study the aeromechanical loads developed over the UH-60A rotor experiencing a severe diving turn ma
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::2d4fa9c8a41f31f6afe0318694ab18b4
A Hybrid Navier-Stokes Free-Wake Computational Fluid Dynamics (CFD) methodology, coupled with a multibody dynamics analysis code, has been applied to the UH-60A rotor to study the loads developed during selected revolutions of a severe diving turn ma
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d6b896ff70875fb7207d3e7924e0f640
A Hybrid Navier-Stokes Free-Wake Computational Fluid Dynamics (CFD) methodology, coupled with a multi-body dynamics analysis code, has been applied to the UH-60A rotor to study the loads developed during selected revolutions of a severe diving turn m
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::750361fafc0cece73432758d882eaae4
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