• DocumentCode
    1719898
  • Title

    An embedded wireless data acquisition system for wind tunnel model applications

  • Author

    Adcock, Edward ; Bartlett, James ; Culliton, William ; Jordan, Thomas ; Mau, Johnny ; Bare, E. Ann ; Florance, Jennifer ; Kahng, Seun

  • Author_Institution
    NASA Langley Res. Center, Hampton, VA, USA
  • fYear
    2001
  • fDate
    8/1/2001 12:00:00 AM
  • Firstpage
    327
  • Lastpage
    336
  • Abstract
    An in-model data acquisition system has been developed that can accept inputs from various sensors and transfer the data wirelessly to an access point outside a wind tunnel´s test section. This system was developed as a potential alternative to the current state of wind tunnel data collection, which requires the use of long lengths of cable carrying low-level sensor signals that are extremely susceptible to induced noise. Irk addition, present methods of retrieving data require that multiple cables be routed across the balance, creating alternate load paths. With the advent of wireless data transfer, not only are these two items addressed, but also the reduction of external cables to the model will reduce wind tunnel model installation time as well as the cost of operation. This paper will describe the results of two separate wind tunnel tests, conducted at NASA Langley´s Transonic Dynamics Tunnel and the 16-foot Transonic Tunnel, in which this new embedded system was used to collect data from typical aerodynamic measurements. The recorded results from these wind tunnel experiments include data from pressure, model attitude, temperature, and force balance transducers
  • Keywords
    aerospace simulation; data acquisition; embedded systems; radiotelemetry; wind tunnels; MEMS sensors; aerodynamic measurements; embedded electronics; embedded wireless data acquisition; external cables reduction; force balance transducers; in-model data acquisition system; model attitude; plug and play/test concept; pressure transducers; smart wing test; temperature transducers; transonic dynamics tunnel; wind tunnel model applications; wireless telemetry; Aerodynamics; Communication cables; Costs; Data acquisition; Embedded system; Information retrieval; NASA; Sensor systems; System testing; Wireless sensor networks;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Instrumentation in Aerospace Simulation Facilities, 2001. 19th International Congress on ICIASF 2001
  • Conference_Location
    Cleveland, OH
  • Print_ISBN
    0-7803-7022-8
  • Type

    conf

  • DOI
    10.1109/ICIASF.2001.960267
  • Filename
    960267