Development of automated test sequence for mach 3.5 propulsion test facility

Srinivas, J and Prateesh Kumar, P and Sathiyamoorthy, K and Venu, G (2013) Development of automated test sequence for mach 3.5 propulsion test facility. In: International Symposium on Air Breathing Engines (ISABE-2013-1306), 9-13 Sep. 2013, Busan, Korea.

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Abstract

Data acquisition and control software plays a pivotal role in operating advanced test facilities. Development of automated test sequence (ATS) for the operation and control of Semi-Free Jet Test Facility (SFJTF) is presented. This paper explains the hardware used to realize the ATS, discrete (on / off) and continuous (PID) control logics developed to operate the facility in a fully automated mode, safety interlocks used and value added features like on-line monitoring of critical facility parameters, manual override etc,. Typical test results of Mach number, total temperature and total pressure are presented for the test runs conducted with the developed ATS.

Item Type: Conference or Workshop Item (Paper)
Additional Information: Copyright to this article belongs to M/s. American Institute of Aeronautics and Astronautics Inc.
Uncontrolled Keywords: Automated test sequence;Propulsion test facility;Pressure transmitters
Subjects: AERONAUTICS > Aeronautics (General)
AERONAUTICS > Aerodynamics
AERONAUTICS > Aircraft Propulsion and Power
Depositing User: Ms. Alphones Mary
Date Deposited: 01 Jul 2014 04:16
Last Modified: 01 Jul 2014 04:16
URI: http://nal-ir.nal.res.in/id/eprint/11989

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