Work

Structural Testing of Full-Scale Flap-Bending/Twist Composite Coupled Blades

Year: 2025

Type: conference-paper

Source: Vertical Flight Society Annual Forum and Technology Display

DOI: 10.4050/f-0081-2025-0138

Authors: Sikorsky, a Lockheed Martin Co., Tyler Sinotte, Sikorsky, a Lockheed Martin Co., Daniel Schuster

Language: English

Topic: Aeroelasticity and Vibration Control

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

OpenAlex ID: W4411858567

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