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Volumn , Issue , 2004, Pages 9549-9563

A study of rotorcraft noise prediction in maneuvering flight

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC NOISE; COMPUTER SIMULATION; HELICOPTERS; MANEUVERABILITY; PROBLEM SOLVING; ROTORS; WIND TUNNELS;

EID: 2942709843     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-850     Document Type: Conference Paper
Times cited : (14)

References (13)
  • 3
    • 0019681684 scopus 로고
    • Theoretical prediction of dynamic inflow derivatives
    • Pitt, D. M., and Peters, D. A., "Theoretical Prediction of Dynamic Inflow Derivatives," Vertica, Vol. 5, No. 1, 1981, pp. 21-34.
    • (1981) Vertica , vol.5 , Issue.1 , pp. 21-34
    • Pitt, D.M.1    Peters, D.A.2
  • 4
    • 0021076378 scopus 로고
    • The prediction of helicopter discrete frequency noise
    • Farassat, F. and Succi, G. P., "The Prediction of Helicopter Discrete Frequency Noise," Vertica, Vol. 7, No. 4, 1983, pp. 309-320.
    • (1983) Vertica , vol.7 , Issue.4 , pp. 309-320
    • Farassat, F.1    Succi, G.P.2
  • 5
    • 0014667963 scopus 로고
    • Sound generation by turbulence and surface in arbitrary motion
    • London, Series A, May
    • Ffowcs Williams, J. E. and Hawkings, D. L., "Sound Generation by Turbulence and Surface in Arbitrary Motion", Philosophical Transactions of the Royal Society, London, Series A, Vol. 264, No 1151, May 1969, pp. 321-342.
    • (1969) Philosophical Transactions of the Royal Society , vol.264 , Issue.1151 , pp. 321-342
    • Ffowcs Williams, J.E.1    Hawkings, D.L.2
  • 12
    • 0027634991 scopus 로고
    • Blade-vortex interaction data obtained from a pressure-instrumented model UH-60a rotor at the DNW
    • July
    • Lorber, P. F., "Blade-Vortex Interaction Data Obtained From a Pressure-Instrumented Model UH-60A Rotor at the DNW," Journal of the American Helicopter Society, Vol. 38, No. 3, July 1993, pp. 2634.
    • (1993) Journal of the American Helicopter Society , vol.38 , Issue.3 , pp. 2634
    • Lorber, P.F.1
  • 13
    • 2342635049 scopus 로고    scopus 로고
    • Flight-path management/control methodology to reduce helicopter blade-vortex interaction noise
    • March-April
    • Schmilz, F. H., Gopalan, G., and Sim, B. W., "Flight-Path Management/Control Methodology to Reduce Helicopter Blade-Vortex Interaction Noise," Journal of Aircraft, Vol. 39., No. 2, March-April 2002, pp. 193205.
    • (2002) Journal of Aircraft , vol.39 , Issue.2 , pp. 193-205
    • Schmilz, F.H.1    Gopalan, G.2    Sim, B.W.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.