Title:
Conceptual Level Optimization of a Fan Stage Under Distortion Considering Aero-structural Constraints

dc.contributor.author Pokhrel, Manish
dc.contributor.author Sarojini, Darshan
dc.contributor.author Mavris, Dimitri N.
dc.contributor.corporatename Georgia Institute of Technology. Aerospace Systems Design Laboratory en_US
dc.contributor.corporatename American Institute of Aeronautics and Astronautics
dc.contributor.corporatename Georgia Institute of Technology. Aerospace Systems Design Laboratory
dc.date.accessioned 2020-06-17T14:42:08Z
dc.date.available 2020-06-17T14:42:08Z
dc.date.issued 2020-06
dc.description Presented at AIAA Aviation 2020 Forum en_US
dc.description.abstract Rotor blades experience unsteady forces and aerodynamic losses when operating in a distorted inflow. The structural analysis of rotors under these conditions, therefore, is of prime importance during the early design phase. In a companion paper, an extension to the multi-meanline method for conceptual fan stage design in a non-axisymmetric flow field has been presented. Here, the authors present a computationally efficient design framework that links the aerodynamic design and structural analysis of the rotor. Rotor structural analysis comprises of computing dynamic stresses, the excitation frequencies, and resonance margins at various modes of vibration. A design space encapsulating fan stage design variables, aerodynamic performance, and rotor structural constraints is explored and optimized for maximum fan stage efficiency subject to aerodynamic and mechanical constraints. en_US
dc.identifier.citation Pokhrel, Manish, Darshan Sarojini, and Dimitri Mavris. "Conceptual Level Optimization of a Fan Stage Under Distortion Considering Aero-structural Constraints." AIAA AVIATION 2020 FORUM. 2020. DOI: https://doi.org/10.2514/6.2020-3115 en_US
dc.identifier.doi 10.2514/6.2020-3115 en_US
dc.identifier.uri http://hdl.handle.net/1853/62943
dc.language.iso en_US en_US
dc.publisher Georgia Institute of Technology en_US
dc.publisher Georgia Institute of Technology
dc.publisher.original American Institute of Aeronautics and Astronautics (AIAA)
dc.relation.ispartofseries ASDL; en_US
dc.subject Rotor blades en_US
dc.subject Structural analysis en_US
dc.subject Structural constraints en_US
dc.title Conceptual Level Optimization of a Fan Stage Under Distortion Considering Aero-structural Constraints en_US
dc.type Text
dc.type.genre Paper
dspace.entity.type Publication
local.contributor.author Mavris, Dimitri N.
local.contributor.corporatename Daniel Guggenheim School of Aerospace Engineering
local.contributor.corporatename Aerospace Systems Design Laboratory (ASDL)
local.contributor.corporatename College of Engineering
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relation.isOrgUnitOfPublication a8736075-ffb0-4c28-aa40-2160181ead8c
relation.isOrgUnitOfPublication 7c022d60-21d5-497c-b552-95e489a06569
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