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Real-time computer data system for the 40- by 80-foot wind tunnel facility at Ames Research CenterThe background material and operational concepts of a computer-based system for an operating wind tunnel are described. An on-line real-time computer system was installed in a wind tunnel facility to gather static and dynamic data. The computer system monitored aerodynamic forces and moments of periodic and quasi-periodic functions, and displayed and plotted computed results in real time. The total system is comprised of several off-the-shelf, interconnected subsystems that are linked to a large data processing center. The system includes a central processor unit with 32,000 24-bit words of core memory, a number of standard peripherals, and several special processors; namely, a dynamic analysis subsystem, a 256-channel PCM-data subsystem and ground station, a 60-channel high-speed data acquisition subsystem, a communication link, and static force and pressure subsystems. The role of the test engineer as a vital link in the system is also described.
Document ID
19750014265
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Cambra, J. M.
(NASA Ames Research Center Moffett Field, CA, United States)
Tolari, G. P.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 3, 2013
Publication Date
May 1, 1975
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NASA-TN-D-7970
A-5751
Accession Number
75N22337
Funding Number(s)
PROJECT: RTOP 021-06-16-05-00
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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