Plasma Fairings for Quieting Aircraft Landing Gear Noise

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNX13CL22P
Agency Tracking Number: 125455
Amount: $124,999.00
Phase: Phase I
Program: SBIR
Awards Year: 2013
Solicitation Year: 2012
Solicitation Topic Code: A3.02
Solicitation Number: N/A
Small Business Information
MO, Chesterfield, MO, 63006-6971
DUNS: 126752018
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Chris Nelson
 Principal Investigator
 (425) 778-7853
Business Contact
 Alan Cain
Title: President
Phone: (314) 373-3311
Research Institution
A major component of airframe noise for commercial transport aircraft is the deployed landing gear. The noise from the gear originates due to complex, unsteady bluff body flow separation from gear components and the subsequent multiple interactions of unsteady wakes with downstream undercarriage elements. The object of this SBIR effort is to develop and advance a novel 'plasma fairing' technology for quieting landing gear noise. The concept deals with the use of single dielectric barrier discharge (SDBD) plasma actuators to reduce noise associated with bluff body separation around the gear. SDBD plasma actuators will be employed either in the form of spanwise-orientated actuators or plasma streamwise vortex generators (PSVGs) to suppress surface pressure fluctuations, and consequently flow-induced noise, on a representative landing gear model. Our Phase I effort will involve a combination of numerical and experimental studies to be conducted at Innovative Technology Applications Company, LLC and the University of Notre Dame, respectively, in order to advance the design and optimization of 'plasma fairings' from a simple geometry (tandem circular cylinder) to a more complex/realistic landing gear geometry (e.g., the Gulfstream G550 nose gear). A combination of DES numerical simulations and wind tunnel experiments is expected to provide a clear demonstration of the plasma fairing performance for noise reduction, while providing a clear path forward for Phase II.

* Information listed above is at the time of submission. *

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