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Wind Tunnel Performance Tests of a Full-Scale Proprotor on the Tiltrotor Test Rig The Tiltrotor Test Rig (TTR) is a new, large-scale proprotor test system for the National Full-Scale Aerodynamics Complex (NFAC). The TTR was jointly developed by NASA, the U. S. Army and the U. S. Air Force. The first wind-tunnel entry was completed in November 2018 with a modern, 26-ft diameter proprotor. The primary purpose was to complete the development of the TTR, including systems integration with the NFAC. The TTR and rotor were tested up to 273 knots in axial flow, which is the highest airspeed ever achieved by a full-scale proprotor in any wind tunnel. The entry constitutes the first full-scale wind-tunnel test of a gimballed, coning-flexure rotor. Extensive conversion-mode data were also acquired, and hover/climb conditions were explored. Additional testing included aerodynamic tares, motor tests, thermal tests, modal vibration tests, and other checkout activities. This report summarizes the results of the test, including examples of the most significant data.
Document ID
20210021871
Acquisition Source
Ames Research Center
Document Type
Technical Memorandum (TM)
Authors
C W Acree, Jr.
(Ames Research Center Mountain View, California, United States)
A L Sheikman
(Ames Research Center Mountain View, California, United States)
T R Norman
(Ames Research Center Mountain View, California, United States)
Date Acquired
September 21, 2021
Publication Date
December 30, 2022
Subject Category
Aeronautics (General)
Report/Patent Number
NASA/TM-20210021871
Funding Number(s)
WBS: 664817
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Technical Review
NASA Peer Committee
Keywords
Tiltrotor Test Rig
TTR
Wind Tunnel
Performance
Full-Scale Proprotor
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