NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
Shake test results of the MDHC test stand in the 40- by 80-foot wind tunnelA shake test was conducted to determine the modal properties of the MDHC (McDonnell Douglas Helicopter Company) test stand installed in the 40- by 80- Foot Wind Tunnel at Ames Research Center. The shake test was conducted for three wind-tunnel balance configurations with and without balance dampers, and with the snubber engagement to lock the balance frame. A hydraulic shaker was used to apply random excitation at the rotor hub in the longitudinal and lateral directions. A GenRad 2515 computer-aided test system computed the frequency response functions at the rotor hub and support struts. From these response functions, the modal properties, including the natural frequency, damping ratio, and mode shape were calculated. The critical modes with low damping ratios are identified as the test-stand second longitudinal mode for the dampers-off configuration, the test-stand yaw mode for the dampers-on configuration, and the test stand first longitudinal mode for the balance-frame locked configuration.
Document ID
19940022093
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Lau, Benton H.
(NASA Ames Research Center Moffett Field, CA, United States)
Peterson, Randall
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1994
Subject Category
Aeronautics (General)
Report/Patent Number
NAS 1.15:108801
NASA-TM-108801
A-94029
Report Number: NAS 1.15:108801
Report Number: NASA-TM-108801
Report Number: A-94029
Accession Number
94N26596
Funding Number(s)
PROJECT: RTOP 505-59-36
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available