메뉴 건너뛰기




Volumn 4, Issue , 2006, Pages 2694-2705

Comparison of noise reduction effect between AFC and conventional IBC by moving overlapped grid method

Author keywords

[No Author keywords available]

Indexed keywords

ACTIVE FLAP CONTROL (AFC); BLADE-VORTEX INTERACTION (BVI); EULER CODES; INDIVIDUAL BLADE CONTROL (IBC);

EID: 33845635153     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (9)

References (49)
  • 1
    • 4143129825 scopus 로고    scopus 로고
    • Flight path management and control methodology to reduce helicopter Blade-Vortex Interaction (BVI) noise
    • San Francisco, CA, Jan.
    • Gopalan, G., Schmitz, F. H., and Sim, B. W., Flight Path Management and Control Methodology to Reduce Helicopter Blade-Vortex Interaction (BVI) Noise, AHS Vertical Lift Aircraft Design Conference, San Francisco, CA, Jan., 2000.
    • (2000) AHS Vertical Lift Aircraft Design Conference
    • Gopalan, G.1    Schmitz, F.H.2    Sim, B.W.3
  • 2
    • 4143124366 scopus 로고    scopus 로고
    • Flight trajectory management to reduce helicopter Blade-Vortex Interaction (BVI) noise with head/Tailwind effects
    • The Hague, The Netherlands, Sep.
    • Schmitz, F. H., Gopalan, G., and Sim, B. W., Flight Trajectory Management to Reduce Helicopter Blade-Vortex Interaction (BVI) Noise with Head/Tailwind Effects, 26th ERF, No. 77, The Hague, The Netherlands, Sep., 2000.
    • (2000) 26th ERF , Issue.77
    • Schmitz, F.H.1    Gopalan, G.2    Sim, B.W.3
  • 3
    • 0020192497 scopus 로고
    • Full-scale measurements of blade-vortex interaction noise
    • Oct
    • Boxwell, D. A. and Schmitz, F. H., Full-Scale Measurements of Blade-Vortex Interaction Noise, Journal of the American Helicopter Society, Vol.27, (4), Oct, 1982, pp. 11-27.
    • (1982) Journal of the American Helicopter Society , vol.27 , Issue.4 , pp. 11-27
    • Boxwell, D.A.1    Schmitz, F.H.2
  • 4
    • 0022752380 scopus 로고
    • Wind-tunnel acoustic results of two rotor models with several designs
    • Martin, R. M. and Connor, A. B., Wind-Tunnel Acoustic Results of Two Rotor Models with Several Designs, NASA-TM 87698, 1986.
    • (1986) NASA-TM 87698
    • Martin, R.M.1    Connor, A.B.2
  • 6
    • 1242274992 scopus 로고
    • Progress towards quieter civil helicopters
    • Lowson, M. V., Progress Towards Quieter Civil Helicopters, 17th ERF, No. 59, 1991.
    • (1991) 17th ERF , Issue.59
    • Lowson, M.V.1
  • 7
    • 0031223475 scopus 로고    scopus 로고
    • Reduction of helicopter blade-vortex interaction noise by active rotor control technology
    • Yu, Y. H., Gmelin, B., Splettstößer, W., Philippe, J.J., Prieur, J., and Brooks, T., Reduction of Helicopter Blade-Vortex Interaction Noise by Active Rotor Control Technology, Prog. Aerospace Sci., Vol. 33, 1997, pp. 647-687.
    • (1997) Prog. Aerospace Sci. , vol.33 , pp. 647-687
    • Yu, Y.H.1    Gmelin, B.2    Splettstößer, W.3    Philippe, J.J.4    Prieur, J.5    Brooks, T.6
  • 8
    • 0029703804 scopus 로고    scopus 로고
    • Passive design for reduction of high-speed impulsive rotor noise
    • Washington DC, June
    • Baeder, J. D., Passive Design for Reduction of High-Speed Impulsive Rotor Noise, AHS 52nd Annual Forum, Washington DC, June 1996.
    • (1996) AHS 52nd Annual Forum
    • Baeder, J.D.1
  • 9
    • 84964238149 scopus 로고    scopus 로고
    • Effect of blade-tip shape on high-speed rotor noise
    • June
    • Aoyama, T., Aoki, M., Kondo, N., Saito, S., and Kawachi, K, Effect of Blade-Tip Shape on High-Speed Rotor Noise, AIAA Paper 96-2380, June 1996.
    • (1996) AIAA Paper , vol.96 , Issue.2380
    • Aoyama, T.1    Aoki, M.2    Kondo, N.3    Saito, S.4    Kawachi, K.5
  • 13
    • 33745521199 scopus 로고    scopus 로고
    • Closed loop IBC results from recent CH-53G flight tests
    • Arnold, U. T. P., Fürst, D., Closed Loop IBC Results from Recent CH-53G Flight Tests, 30th ERF, 2004.
    • (2004) 30th ERF
    • Arnold, U.T.P.1    Fürst, D.2
  • 14
    • 4143111255 scopus 로고    scopus 로고
    • Active tab, a new active technique for helicopter noise reduction
    • Kobiki, N., et al., Active Tab, a New Active Technique for Helicopter Noise Reduction, 29th ERF, 2003.
    • (2003) 29th ERF
    • Kobiki, N.1
  • 16
    • 4143135289 scopus 로고    scopus 로고
    • Numerical analysis of BVI noise reduction by active tab
    • Aoyama, T., Yang, C., Saito, S., Numerical Analysis of BVI Noise Reduction by Active Tab, 60th AHS Annual Forum. 2004.
    • (2004) 60th AHS Annual Forum
    • Aoyama, T.1    Yang, C.2    Saito, S.3
  • 18
    • 33644644291 scopus 로고    scopus 로고
    • Closed-loop control test of the NASA/Army/MIT active twist rotor for vibration reduction
    • Phoenix, AZ, May
    • Shin, S., Cesnik, C. E. S., Hall, S. R., Closed-loop Control Test of the NASA/Army/MIT Active Twist Rotor for Vibration Reduction, AHS 59th Annual Forum, Phoenix, AZ, May, 2003.
    • (2003) AHS 59th Annual Forum
    • Shin, S.1    Cesnik, C.E.S.2    Hall, S.R.3
  • 20
    • 33644669999 scopus 로고    scopus 로고
    • Acoustic aspects of active-twist rotor control
    • Montreal, Canada, June
    • Booth, E. R., Jr., Wilbur, M. L., Acoustic Aspects of Active-Twist Rotor Control, AHS 58th Annual Forum, Montreal, Canada, June, 2002.
    • (2002) AHS 58th Annual Forum
    • Booth Jr., E.R.1    Wilbur, M.L.2
  • 21
    • 33745529888 scopus 로고    scopus 로고
    • Vibration reduction in rotorcraft using actively controlled flaps - Their evolution and potential for improving rotorcraft technology
    • Friedmann, P. P., Vibration Reduction In Rotorcraft Using Actively Controlled Flaps - Their Evolution and Potential for Improving Rotorcraft Technology, 30th ERF, 2004.
    • (2004) 30th ERF
    • Friedmann, P.P.1
  • 22
    • 4143092566 scopus 로고    scopus 로고
    • Simultaneous vibration and noise reduction in rotorcraft using aeroelastic simulation
    • Liu, L., Patt, D., and Friedmann, P. P., Simultaneous Vibration and Noise Reduction in Rotorcraft Using Aeroelastic Simulation, 60th AHS Annual Forum, 2004.
    • (2004) 60th AHS Annual Forum
    • Liu, L.1    Patt, D.2    Friedmann, P.P.3
  • 23
    • 33745560506 scopus 로고    scopus 로고
    • Achieving simultaneous reduction of rotorcraft vibration and noise reduction using simulation
    • Patt, D., Liu, L., and Friedmann, P. P., Achieving Simultaneous Reduction of Rotorcraft Vibration and Noise Reduction Using Simulation, 30th ERF, 2004.
    • (2004) 30th ERF
    • Patt, D.1    Liu, L.2    Friedmann, P.P.3
  • 25
    • 33644664024 scopus 로고    scopus 로고
    • Active interrogation of helicopter rotor faults using trailing edge flap actuation
    • Washington, DC, May
    • Stevens, P. W., Smith, E. C., Active Interrogation of Helicopter Rotor Faults using Trailing Edge Flap Actuation, AHS 57th Annual Forum, Washington, DC, May, 2001.
    • (2001) AHS 57th Annual Forum
    • Stevens, P.W.1    Smith, E.C.2
  • 29
    • 33644690835 scopus 로고    scopus 로고
    • Main rotor active flaps: Numerical assessment of noise and vibration reduction
    • Leconte, P. and Kube, R., Main Rotor Active Flaps: Numerical Assessment of Noise and Vibration Reduction, 2nd DLR-ONERA Aerospace Symposium, 2000.
    • (2000) 2nd DLR-ONERA Aerospace Symposium
    • Leconte, P.1    Kube, R.2
  • 32
    • 84888829603 scopus 로고    scopus 로고
    • http://www.eurocopter.com
  • 33
    • 84888852710 scopus 로고    scopus 로고
    • http://www.boeing.com/news/releases/2004/q2/nr_040518t.html.
  • 34
    • 0011399568 scopus 로고    scopus 로고
    • Wind tunnel testing of a mach-scaled active rotor with trailing-edge FLAPS
    • Washington, DC, May
    • Koratkar, N. A., Spencer, M. G., Chopra, L, Wind Tunnel Testing of a Mach-Scaled Active Rotor with Trailing-Edge FLAPS, AHS 57th Annual Forum, Washington, DC, May, 2001.
    • (2001) AHS 57th Annual Forum
    • Koratkar, N.A.1    Spencer, M.G.2    Chopra, L.3
  • 35
    • 0034296455 scopus 로고    scopus 로고
    • Status of application of smart structures technology to rotorcraft systems
    • Chopra, I., Status of Application of Smart Structures Technology to Rotorcraft Systems, J. of AHS, Vol. 45, No. 4, pp. 228-252, 2000.
    • (2000) J. of AHS , vol.45 , Issue.4 , pp. 228-252
    • Chopra, I.1
  • 36
    • 0032184345 scopus 로고    scopus 로고
    • Rotors with trailing edge flaps: Analysis and comparison with experimental data
    • Milgram, J., Chopra, L, and Straub, F., Rotors with Trailing Edge Flaps: Analysis and Comparison with Experimental Data, J. of AHS, Vol. 43, (4), 1998, pp. 319-332.
    • (1998) J. of AHS , vol.43 , Issue.4 , pp. 319-332
    • Milgram, J.1    Chopra, L.2    Straub, F.3
  • 37
    • 0030247268 scopus 로고    scopus 로고
    • Unsteady aerodynamics of flapped airfoil in subsonic flow by indicial concepts
    • Sep.-Oct.
    • Hariharan, N, and Leishman, J. G., Unsteady Aerodynamics of Flapped Airfoil in Subsonic Flow by Indicial Concepts. J. of Aircraft, Vol. 33, (5), Sep.-Oct. 1996, pp. 855-868.
    • (1996) J. of Aircraft , vol.33 , Issue.5 , pp. 855-868
    • Hariharan, N.1    Leishman, J.G.2
  • 38
    • 0029344786 scopus 로고
    • Rotor free-wake modeling using a pseudo-implicit technique including comparisons with experimental data
    • Bagai, A., and Leishman, J. G., Rotor Free-Wake Modeling Using a Pseudo-Implicit Technique Including Comparisons with Experimental Data, J. of AHS, Vol. 40, (3), 1995.
    • (1995) J. of AHS , vol.40 , Issue.3
    • Bagai, A.1    Leishman, J.G.2
  • 39
    • 0031699301 scopus 로고    scopus 로고
    • Vibration reduction in rotorcraft using actively controlled trailing edge flaps and issues related to practical implementation
    • May
    • Myrtle, T. F. and Friedmann, P. P., Vibration Reduction in Rotorcraft Using Actively Controlled Trailing Edge Flaps and Issues Related to Practical Implementation, 54th AHS Forum, May, 1998.
    • (1998) 54th AHS Forum
    • Myrtle, T.F.1    Friedmann, P.P.2
  • 40
    • 84883522572 scopus 로고    scopus 로고
    • Numerical analysis of active flap for noise reduction using moving overlapped grid method
    • Grapevine, TX, June
    • Aoyama, T., Yang, C., Saito, S., Numerical Analysis of Active Flap for Noise Reduction Using Moving Overlapped Grid Method, AHS 61st Annual Forum, Grapevine, TX, June, 2005.
    • (2005) AHS 61st Annual Forum
    • Aoyama, T.1    Yang, C.2    Saito, S.3
  • 42
    • 33644694207 scopus 로고    scopus 로고
    • Numerical analysis of interaction noise between main rotor and tail rotor of helicopter
    • Yokohama, August
    • Yang, C., Aoyama, T, Saito, S., Numerical Analysis of Interaction Noise between Main Rotor and Tail Rotor of Helicopter, 24th ICAS, Yokohama, August, 2004.
    • (2004) 24th ICAS
    • Yang, C.1    Aoyama, T.2    Saito, S.3
  • 43
    • 0018705112 scopus 로고
    • Rotational noise of helicopter rotors
    • Nakamura, Y., and Azuma, A., "Rotational Noise of Helicopter Rotors," Vertica, vol. 3, No. 3/4, pp.293-316, 1979.
    • (1979) Vertica , vol.3 , Issue.3-4 , pp. 293-316
    • Nakamura, Y.1    Azuma, A.2
  • 44
    • 4143071350 scopus 로고
    • Unsteady calculation for flow-field of helicopter rotor with various tip shapes
    • Paper No.B03, Avignon, France, September
    • Aoyama, T., Kawachi, K., Saito, S., Unsteady Calculation for Flow-field of Helicopter Rotor with Various Tip Shapes, 18th European Rotorcraft Forum, Paper No.B03, Avignon, France, September 1992.
    • (1992) 18th European Rotorcraft Forum
    • Aoyama, T.1    Kawachi, K.2    Saito, S.3
  • 45
    • 0027552521 scopus 로고
    • Higher-order-accurate upwind schemes for solving the compressible Euler and Navier-Stokes equations
    • Yamamoto, S. and Daiguji, H., Higher-Order-Accurate Upwind Schemes for Solving the Compressible Euler and Navier-Stokes Equations, J. of Computers & Fluids, 22, pp.259-270, 1993.
    • (1993) J. of Computers & Fluids , vol.22 , pp. 259-270
    • Yamamoto, S.1    Daiguji, H.2
  • 46
    • 0002611610 scopus 로고    scopus 로고
    • Role of CFD in aeronautical engineering (No. 14) - AUSM type upwind schemes
    • Shima, E. and Jounouchi, T., Role of CFD in Aeronautical Engineering (No. 14) - AUSM type Upwind Schemes -, NAL SP-34, 1999, pp. 7-12.
    • (1999) NAL SP-34 , pp. 7-12
    • Shima, E.1    Jounouchi, T.2
  • 47
    • 0012319835 scopus 로고
    • Theory of noise generation from moving bodies with an application to helicopter rotors
    • Farassat, F., Theory of noise generation from moving bodies with an application to helicopter rotors, NASA TR R 451, 1975.
    • (1975) NASA TR , vol.R 451
    • Farassat, F.1
  • 48
    • 21244483683 scopus 로고    scopus 로고
    • Elementary study for the effect of HHC and active flap on blade vortex interaction
    • Dresden, Germany, September
    • Kobiki, N., Tsuchihashi, A., Murashige, A., Yamakawa, E., Elementary Study for the Effect of HHC and Active Flap on Blade Vortex Interaction, 23rd European Rotorcraft Forum, Dresden, Germany, September, 1997.
    • (1997) 23rd European Rotorcraft Forum
    • Kobiki, N.1    Tsuchihashi, A.2    Murashige, A.3    Yamakawa, E.4


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.