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http://dx.doi.org/10.5139/JKSAS.2013.41.1.10

Effective Perceived Noise Level Prediction for a Propeller driven UAV by using Wind Tunnel Test Data  

Ryi, Jae-Ha (Department of Aerospace Engineering, Chungnam National University)
Rhee, Wook (DAEWOO Shipbuilding and Marine Engineering CO., LTD.)
Choi, Jong-Soo (Department of Aerospace Engineering, Chungnam National University)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.41, no.1, 2013 , pp. 10-16 More about this Journal
Abstract
This paper discussed a procedure for noise certification of Aircraft and predicting the full scale over-flight noise of propeller from acoustic wind tunnel measurement of small scale propeller. Noise Certification Procedures is established from International Civil Aviation Organization(ICAO). The data manipulations are then discussed in extrapolation to simulation flight distance and flight simulation. One of the most important point of flight simulation is adjustments for differences between wind tunnel test conditions and flight test conditions. To simulated the noise level estimation procedure for noise data post-process, simulate procedures from data of the wind tunnel noise measurement and the flight noise measurement by using a 7kg degree UAV. This study confirmed an effectively noise estimation procedures by wind tunnel noise test and flight noise test.
Keywords
ICAO; Propeller Noise; Flight Noise Test; EPNL; Wind Tunnel Test; Environmental Noise;
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