Interior noise ground tests conducted on a DC-9 aircraft test section are described. The objectives were to study ground test and analysis techniques for evaluating the effectiveness of interior noise control treatments for advanced turboprop aircraft, and to study the sensitivity of the ground test results to changes in various test conditions. Noise and vibration measurements were conducted under simulated advanced turboprop excitation, for two interior noise control treatment configurations. These ground measurement results were compared with results of earlier UHB (Ultra High Bypass) Demonstrator flight sts with comparable interior treatment configurations. The Demonstrator is an MD-80 test aircraft with the left JT8D engine replaced with a prototype UHB advanced turboprop engine.
Comparison ofdvanced turboprop interior noise control ground and flight test data
01.01.1992
Aufsatz (Konferenz)
Keine Angabe
Englisch
Comparison of Advanced Turboprop Interior Noise Control Ground and Flight Test Data
British Library Conference Proceedings | 1992
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