Validation of a prediction model for aerodynamic noise from aircraft landing gear

8th AIAA/CEAS Aeroacoustics Conference and Exhibit

Volumn , Issue , 2002, Pages

  Smith, M G ^a   Chow, L C ^b  

^a UNIVERSITY OF SOUTHAMPTON   (United Kingdom)

^b AIRBUS OPERATIONS LTD   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC NOISE; DEVELOPMENT AND TESTING; ENGINEERING TOOLS; FULL SCALE TESTS; NUMBER OF FACTORS; PREDICTION MODEL; REDUCTION POTENTIAL; SEMI-EMPIRICAL;

AEROACOUSTICS; AERODYNAMICS; AIRFRAMES; ENGINES; LANDING GEAR (AIRCRAFT); NOISE ABATEMENT; STRUCTURAL FRAMES; WIND TUNNELS;

ACOUSTIC NOISE;

EID: 84896689701     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)

1. Souliez, F.J., Long, L.N., Morris, P.J., Sharma, A. Landing Gear Aerodynamic Noise Prediction using Unstructured Grids, AIAA 2002-0799
2. Smith, M.G., Chow, L.C., Prediction Method for Aerodyanmic Noise from Aircraft Landing Gears, AIAA 98-2228
3. Chow, L.C., Mau, K., Remy, H. Landing Gears and High Lift Devices Airframe Noise Research, AIAA 2002-2408
4. Dobrzynski, W., Chow, L.C., Guion, P., Shiells, D. Research into Landing gears Airframe Noise Reduction. AIAA 2002-2409
5. Dobrzynski, W. and Buckholz, H. Full Scale Noise Testing on Airbus Landing Gears in the German Dutch Wind Tunnel, AIAA-97-1597, May 1997.
6. Amiet, R.K. Correction of Open Jet Wind Tunnel Measurements for Shear Layer Refraction, AIAA Paper No. 75-532, March 1975.
7. Curle, N. The influence of Solid Boundaries upon Aerodynamic Sound. Proc. Royal Soc., Vol. A231, pp.505-514, 1955.
8. Dowling, A.P. and Ffowcs Williams, J.E. Sound and Sources of Sound, Ellis Horwood, 1983