Sensitivity of the FAA Integrated Noise Model to input parameters

Applied Acoustics

Volumn 66, Issue 3, 2005, Pages 263-276

  Clemente, J ^a   Gaja, E ^b   Clemente, G ^b   Reig, A ^b  

^a GARCÍA BBM Acústica ^*  (Spain)

^b UNIVERSITAT POLITÈCNICA DE VALÈNCIA   (Spain)

Author keywords

Aircraft noise; Integrated noise model; Noise modelling; Sensitivity analysis

Indexed keywords

AIRCRAFT; AIRPORTS; COMPUTATIONAL METHODS; COMPUTER SIMULATION; FLIGHT DYNAMICS; SENSITIVITY ANALYSIS;

CIVIL AIRPORTS; NOISE CONTOURS; SEGMENTATION TECHNIQUE;

ACOUSTIC NOISE;

EID: 10644232873     PISSN: 0003682X     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.apacoust.2004.08.002     Document Type: Article

References (7)

1. Hullah P, Cavadini L. Aircraft noise modelling validation through the use of full 4-D flight trajectories including thrust calculation. In: Fourth FAA/Eurocontrol R&D Conference.
2. European Civil Aviation Conference. Report on Standard Method of Computing Noise Contours around Civil Airports, doc. 29.
3. Society of Automotive Engineers, A21 Committee. Procedure for the Calculation of Aircraft Noise in the Vicinity of Airports, SAE-AIR-1845.
4. Federal Aviation Administration. Integrated Noise Model 5.1 Technical Manual.
5. Clemente FJ. Uncertainties in Aircraft Noise Modelling. Institute of Sound and Vibration Research, Southampton, United Kingdom, 2003.
6. EUROCONTROL Experimental Centre. Error Sensitivity Analysis of the Integrated Noise Model, doc, EEC/ENV/2002/006, 2002.
7. Singer BA, Lockard DP, Brentner KS. Computational aeroacoustic analysis of slat trailing-edge flow.