NASA/AHS Rotorcraft Noise Reduction program - Accomplishments at Sikorsky Aircraft
Helicopter external noise technology development since the initiation of the highly successful NASA/AHS Rotorcraft Noise Reduction program in 1983 is discussed. The effect of various blade tip shapes on two 9.4-ft diameter rotor systems investigated in NASA-Langley's 14 x 22 ft wind tunnel was...
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Veröffentlicht in: | Vertiflite 1989-01, Vol.35, p.68-73 |
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1. Verfasser: | |
Format: | Magazinearticle |
Sprache: | eng |
Online-Zugang: | Volltext |
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Zusammenfassung: | Helicopter external noise technology development since the initiation of the highly successful NASA/AHS Rotorcraft Noise Reduction program in 1983 is discussed. The effect of various blade tip shapes on two 9.4-ft diameter rotor systems investigated in NASA-Langley's 14 x 22 ft wind tunnel was determined. A noise reduction potential of up to 5 dB in BVI noise levels was demonstrated. Tail rotor noise characteristics, with and without empennage interaction effects, were also studied. (K.K.) |
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ISSN: | 0042-4455 |