High-Speed Wind Tunnel Tests of a Full-Scale Proprotor on the Tiltrotor Test Rig

Acree, C W, Jr ; Sheikman, A L ; Norman, Thomas R

关键词: HYPERSONIC WIND TUNNELS;    TRANSONIC WIND TUNNELS;    WIND TUNNEL TESTS;    AERODYNAMICS;    CLIMBING FLIGHT;    HOVERING;    ROTORS;    TILT ROTOR AIRCRAFT;    VIBRATION TESTS;   

RP-ID  :  ARC-E-DAA-TN67822

学科分类：航空航天科学

美国|英语

来源: NASA Technical Reports Server

【 摘 要 】

The Tiltrotor Test Rig (TTR) is a NASA project, joint with the U.S. Army and Air Force, to develop a new, large scale proprotor test system for the National Full-Scale Aerodynamics Complex (NFAC). 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. This is the highest airspeed ever achieved by a full-scale proprotor in any wind tunnel. 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 paper summarizes the results of the test, including examples of the most significant data.