Ravikumar, C and Balakrishnan, N and Holla, VS (1987) A Microprocessor Based System for Wind Tunnel Measurements. In: ICIASF '87 RECORD: Proceedings of the 12th International Congress on Instrumentation in Aerospace Simulation Facilities, June 22-25, 1987, Williamsburg, VA, pp. 54-68.
A 16- bit microprocessor based system has been designed and developed for automatic flow field pressure survey and force measurements in the low speed wind tunnel at the Indian Institute of Science. The instrumentation sub systems that are required for the above measurements under the processor control, the system processor or unit, interfaces to standard peripherals, future expansion provisions and communication channel to other computer systems have all been developed in- house. Software has been designed to provide a powerful friendly and reconfigurable integrated integrated instrumentation. The software also ensures POAL time data acquision. On-line 'pre-processing and storage of the data on a floppy. Software has also been developed on an inexpensive PC for the data presentation in color graphics. The design, development and implementation details, of the system have been presented in this paper.
|Item Type:||Conference Paper|
|Additional Information:||©1987 IEEE. Personal use of this material is permitted. However, permission to reprint/republish this material for advertising or promotional purposes or for creating new collective works for resale or redistribution to servers or lists, or to reuse any copyrighted component of this work in other works must be obtained from the IEEE.|
|Keywords:||Wind tunnel measurements;Component strain gauge balance|
|Department/Centre:||Division of Mechanical Sciences > Aerospace Engineering (Formerly, Aeronautical Engineering)|
|Date Deposited:||25 Aug 2008|
|Last Modified:||19 Sep 2010 04:14|
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