F-0079-2023-18007: Surrogate-model based Optimization Framework for the Structural Design of Helicopter Rotor Blades subject to Dynamics and Failure Criteria - Technical Paper

Event: Vertical Flight Society 79th Annual Forum and Technology Display

Authors

 German Aerospace Center (DLR)

Franziska Becker

 German Aerospace Center (DLR)

Abstract

Content: ABSTRACT

Meta Tags

Topics: Propellers and rotors
Optimization
Failure analysis

Affiliated or Co-Author: German Aerospace Center (DLR)

Details

DOI: https://doi.org/10.4050/F-0079-2023-18007

Citation: Majeti, R. and Becker, F., "Surrogate-model based Optimization Framework for the Structural Design of Helicopter Rotor Blades subject to Dynamics and Failure Criteria," Vertical Flight Society 79th Annual Forum and Technology Display, West Palm Beach, Florida, May 16, 2023, https://doi.org/10.4050/F-0079-2023-18007.

Additional Details

Publisher: The Vertical Flight Society

Published: 5/16/2023

Product Code: F-0079-2023-18007

Content Type: Technical Paper

Language: English