Upgrades at the NASA Langley Research Center National Transonic Facility
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Several projects have been completed or are nearing completion at the NASA Langley Research Center (LaRC) National Transonic Facility (NTF). The addition of a Model Flow-Control/Propulsion Simulation test capability to the NTF provides a unique, transonic, high-Reynolds number test capability that is well suited for research in propulsion airframe integration studies, circulation control high-lift concepts, powered lift, and cruise separation flow control. A 1992 vintage Facility Automation System (FAS) that performs the control functions for tunnel pressure, temperature, Mach number, model position, safety interlock and supervisory controls was replaced using current, commercially available components. This FAS upgrade also involved a design study for the replacement of the facility Mach measurement system and the development of a software-based simulation model of NTF processes and control systems. The FAS upgrades were validated by a post upgrade verification wind tunnel test. The data acquisition system (DAS) upgrade project involves the design, purchase, build, integration, installation and verification of a new DAS by replacing several early 1990’s vintage computer systems with state of the art hardware/software. This paper provides an update on the progress made in these efforts. See reference 1.
[1] Owen W. Bissett,et al. Selected Major Modifications To The National Transonic Facility , 2009 .
[2] William E. Milholen,et al. NASA High-Reynolds Number Circulation Control Research - Overview of CFD and Planned Experiments , 2010 .
[3] B. L. Berrier,et al. Operating Characteristics of the Multiple Critical Venturi System and Secondary Calibration Nozzles Used for Weight-Flow Measurements in the Langley 16-Foot Transonic Tunnel , 1985 .