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http://dx.doi.org/10.5139/JKSAS.2012.40.6.536

Design of Instrumented Pod for Flight Aeroacoustic Environment  

Jun, Oo-Chul (국방과학연구소 7본부 2부)
Kim, Sang-Yong (국방과학연구소)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.40, no.6, 2012 , pp. 536-541 More about this Journal
Abstract
An instrumented pod has been developed to measure the aeroacoustic environment as well as the conventional data such as load, vibration, and aerodynamic heating of fighters during flight tests, confirming to the recently developed external pod design for fighters. This study presents the development of the measurement system in detail, being the first indigenous effort in its kind. The pod was designed to meet the requirements of the MIL-HDBK-1763 and MIL-STD-810 Method 515, which are the base to determine the locations and range of sensors. The Endevco 8510B-2 was selected as the sensor to withstand the harsh environment during the flight tests. In order to assess the integrity of the fabricated pod design, a ground run-up test of a KF-16 has been conducted with the pod installed at Station 5. The test results show that the system works well but the sound level exceeds the predetermined sensor range. The sensor range has been readjusted for flight test performed later.
Keywords
Aeroacoustic Test; Instrumented Pod; Aircraft-Store Compatibility;
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