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Volumn , Issue , 2001, Pages

Unsteady blade response: The BVI model vs. The gust model

Author keywords

[No Author keywords available]

Indexed keywords

BLADE THICKNESS; BLADE-VORTEX INTERACTION; BOUNDARY ELEMENT ANALYSIS; FLOW DISTURBANCES; MODEL-BASED OPC; RAPID DISTORTION THEORY; SECTION THICKNESS; VORTEX CONVECTION;

EID: 84896839518     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (16)

References (19)
  • 1
    • 0031121652 scopus 로고    scopus 로고
    • Effects of Surface Blowing/Suction On The Aerodynamics of Helicopter Rotor Blade-vortex Interactions (BVI)-A Numerical Simulation
    • April
    • Rassan, A. A., Straub, F. K., and Charles, B. D., "Effects of Surface Blowing/Suction On The Aerodynamics of Helicopter Rotor Blade-vortex Interactions (BVI)-A Numerical Simulation," J. of the American Helicopter Society, Vol. 42, No. 2, April 1997, pp. 182-194.
    • (1997) J. of the American Helicopter Society , vol.42 , Issue.2 , pp. 182-194
    • Rassan, A.A.1    Straub, F.K.2    Charles, B.D.3
  • 2
    • 0031186715 scopus 로고    scopus 로고
    • Parallel Blade-vortex Interactions: An Experimental Study and Comparison with Computations
    • July
    • Kitaplioglu, C., Caradonna, F., and Burley, C. L., "Parallel Blade-vortex Interactions: An Experimental Study and Comparison with Computations," J. of the American Helicopter Society, Vol. 42, No. 3, July 1997, pp. 272-281.
    • (1997) J. of the American Helicopter Society , vol.42 , Issue.3 , pp. 272-281
    • Kitaplioglu, C.1    Caradonna, F.2    Burley, C.L.3
  • 7
    • 0032265227 scopus 로고    scopus 로고
    • Direct Computations of Unsteady Flows About Thin Airfoils
    • Grace, S. M., Hariharan, S. I., and Atassi, H. M., "Direct Computations of Unsteady Flows About Thin Airfoils," Journal of Computational Acoustics, Vol. 6, No. 3, 1998, pp. 337-355.
    • (1998) Journal of Computational Acoustics , vol.6 , Issue.3 , pp. 337-355
    • Grace, S.M.1    Hariharan, S.I.2    Atassi, H.M.3
  • 8
    • 0000812311 scopus 로고    scopus 로고
    • Radiated Noise from Airfoils in Realistic Mean Flows
    • June
    • Lockard, D. P. and Morris, P. J., "Radiated Noise from Airfoils in Realistic Mean Flows," AIAA Journal, Vol. 36, No. 6, June 1998, pp. 907-914.
    • (1998) AIAA Journal , vol.36 , Issue.6 , pp. 907-914
    • Lockard, D.P.1    Morris, P.J.2
  • 9
    • 0020098679 scopus 로고
    • Effect of Thickness on Airfoil Surface Noise
    • March
    • Olsen, W. and Wagner, J., "Effect of Thickness on Airfoil Surface Noise," AIAA J., Vol. 20, No. 3, March 1982, pp. 437-439.
    • (1982) AIAA J , vol.20 , Issue.3 , pp. 437-439
    • Olsen, W.1    Wagner, J.2
  • 10
    • 84896811359 scopus 로고    scopus 로고
    • private communication with DTMB research scientist
    • Minniti, R., 2000, private communication with DTMB research scientist.
    • (2000)
    • Minniti, R.1
  • 12
    • 0031555839 scopus 로고    scopus 로고
    • A Unified Boundary Integral Methodology for Aerodynamics and Aeroacoustics of Rotors
    • Gennaretti, M., Luceri, L., and Morino, L., "A Unified Boundary Integral Methodology for Aerodynamics and Aeroacoustics of Rotors," J. Sound and Vib., Vol. 200, No. 4, 1997, pp. 467-89.
    • (1997) J. Sound and Vib , vol.200 , Issue.4 , pp. 467-489
    • Gennaretti, M.1    Luceri, L.2    Morino, L.3
  • 13
    • 85025190709 scopus 로고
    • Boundary Integral Equations In Aerodynamics
    • Morino, L., "Boundary Integral Equations In Aerodynamics," Appl. Mech. Rev., Vol. 46, No. 8, 1993, pp. 445-66.
    • (1993) Appl. Mech. Rev , vol.46 , Issue.8 , pp. 445-466
    • Morino, L.1
  • 15
    • 84977142687 scopus 로고    scopus 로고
    • Free-Wake Analysis for Calculating the Aeroacoustics of a Wing-Flap Configuration
    • Reno, NV, Jan 10-13 2000, Paper no. AIAA 2000-0607
    • Wood, T. H. and Grace, S. M., "Free-Wake Analysis for Calculating the Aeroacoustics of a Wing-Flap Configuration," Proceedings of the 38th AIAA Aerospace Sciences Meeting, Reno, NV, Jan 10-13 2000, pp. 162-173, Paper no. AIAA 2000-0607.
    • Proceedings of the 38th AIAA Aerospace Sciences Meeting , pp. 162-173
    • Wood, T.H.1    Grace, S.M.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.