NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Ground Vibration Testing of the TiltRotor Aeroelastic Stability TestbedThis report is a summary of the ground vibration testing of the TiltRotor Aeroelastic Stability Testbed (TRAST). The U.S. Army has developed this new tiltrotor model system to validate whirl flutter stability analysis, a critical instability mechanism in this type of aircraft. As such, component-level vibration testing is critical to creating and validating analytical models. This report includes experimental vibration testing results from component level to the full model system. In addition, experimentally measured stiffness values are reported for key components of the model.
Document ID
20240004747
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Andrew R Kreshock
(United States Army Research Laboratory Adelphi, Maryland, United States)
Robert P Thornburgh
(United States Army Research Laboratory Adelphi, Maryland, United States)
Date Acquired
April 17, 2024
Publication Date
November 1, 2024
Subject Category
Aircraft Design, Testing and Performance
Research and Support Facilities (Air)
Report/Patent Number
NASA/TM-20240004747
Funding Number(s)
INTERAGENCY: 27678
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
wind tunnel testing
whirl flutter
No Preview Available