Modal Test and Analysis of the NASA Tiltrotor Test Rig

Russell, Carl R ; Acree, Cecil W

关键词: TILT ROTOR AIRCRAFT;    WIND TUNNELS;    AERODYNAMICS;    FREQUENCY RESPONSE;    HAMMERS;    SHAKING;    VIBRATION MODE;    SHAKERS;   

RP-ID  :  ARC-E-DAA-TN50736

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 being developed at the NASA Ames Research Center for testing full-scaleproprotors in the National Full-scale Aerodynamics Complex (NFAC) wind tunnel. The TTR is currentlyundergoing checkout testing to ensure its proper functionality. Part of the checkout process is a groundvibration test, or shake test, to characterize the modal characteristics of the test rig once it is installed in the wind tunnel. This paper presents a summary of the shake test procedure and an overview of the test results. The results include frequency response functions for a number of different test configurations as well as visualizations of the major mode shapes. Excitation methods included random and swept sine shaking as well as hammer impacts. At the conclusion of this paper, some recommendations are given for future shake tests.