Under-wing installation effects on jet noise at sideline

4th AIAA/CEAS Aeroacoustics Conference

Volumn , Issue , 1998, Pages

  Mead, Craig J ^a   Strange, Paul J R ^b  

^a DEFENCE SCIENCE AND TECHNOLOGY LABORATORY   (United Kingdom)

^b ROLLS ROYCE PLC   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC NOISE; ACOUSTIC NOISE MEASUREMENT; ACOUSTIC WAVE TRANSMISSION; AEROACOUSTICS; ARCHITECTURAL ACOUSTICS; ENGINES; EXHAUST SYSTEMS (ENGINE); TURBOFAN ENGINES;

HIGHER FREQUENCIES; INSTALLATION EFFECTS; LOWER FREQUENCIES; RECTANGULAR PLATES; SIMULATED FLIGHT; SOUND TRANSMISSION; STATIC CONDITIONS; TEST PROGRAMME;

FIGHTER AIRCRAFT;

EID: 84896815306     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-2207     Document Type: Conference Paper

References (13)

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11. Head R W and Fisher M J, ‘Jet/surface interaction noise:-Analysis offarfield low frequency augmentations of jet noise due to the presence of a shield’, AIAA-76-502, July 1976.
12. Cargill A M, ‘Flight evaluation of an acoustic exhaust shield’, Unpublished internal memo (IMR 00327), Rolls-Royce pic., 1977.
13. Reddy N N and Tanna H K, ‘Installation effects on jet noise inflight’, AIAA-80-1044, June 1980.