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Wind tunnel apparatus for translational oscillation experimentsA full-model translational oscillation apparatus has been developed for the wind-tunnel determination, in a wide speed range, of all three moment derivatives due to translational acceleration. The apparatus can be employed, in principle, for both vertical and horizontal oscillation experiments and can be used, therefore, to obtain moment derivatives due to alpha or beta, respectively. This information can be obtained directly if the model can be oscillated in the translational mode only, or indirectly - by utilizing some complementary information from angular oscillation experiments - if the model is allowed to also perform a small angular oscillation. The apparatus employs modern, fully digital instrumentation and an extensive use of auto and cross correlation techniques is made in the data reduction procedure
Document ID
19800039757
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Orlik-Ruckemann, K. J.
(National Aeronautical Establishment Ottawa Ontario, Canada)
Hanff, E. S.
(National Aeronautical Establishment Ottawa Ontario, Canada)
Anstey, C. R.
(National Aeronautical Establishment Ottawa, Canada)
Date Acquired
August 10, 2013
Publication Date
January 1, 1980
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
AIAA PAPER 80-0046
Report Number: AIAA PAPER 80-0046
Meeting Information
Meeting: Aerospace Sciences Meeting
Location: Pasadena, CA
Start Date: January 14, 1980
End Date: January 16, 1980
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
80A23927
Funding Number(s)
CONTRACT_GRANT: NASW-3079
Distribution Limits
Public
Copyright
Other

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