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Volumn 10, Issue 1, 2001, Pages 77-85

Blade-vortex interaction noise reduction with active twist smart rotor technology

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC VARIABLES CONTROL; AERODYNAMICS; COMPUTATIONAL FLUID DYNAMICS; INTELLIGENT MATERIALS; NOISE ABATEMENT;

EID: 0035249993     PISSN: 09641726     EISSN: None     Source Type: Journal    
DOI: 10.1088/0964-1726/10/1/307     Document Type: Article
Times cited : (34)

References (42)
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    • Surendriah, M.1
  • 20
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    • Induced strain actuation of composite beams and rotor blades with embedded piezoceramics
    • Chen P C and Chopra I 1996 Induced strain actuation of composite beams and rotor blades with embedded piezoceramics Smart Struct. Mater. 5 35-48
    • (1996) Smart Struct. Mater. , vol.5 , pp. 35-48
    • Chen, P.C.1    Chopra, I.2
  • 21
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    • Hover test of a smart rotor with induced strain actuation of blade twist
    • Chen P C and Chopra I 1997 Hover test of a smart rotor with induced strain actuation of blade twist AIAA J. 35 6-16
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    • Chen, P.C.1    Chopra, I.2
  • 22
    • 0031130312 scopus 로고    scopus 로고
    • Wind tunnel test of a smart rotor with induced strain actuation of blade twist
    • Chen P C and Chopra I 1997 Wind tunnel test of a smart rotor with induced strain actuation of blade twist J. Intell. Mater. Syst. Struct. 8 414-25
    • (1997) J. Intell. Mater. Syst. Struct. , vol.8 , pp. 414-425
    • Chen, P.C.1    Chopra, I.2
  • 26
  • 32
    • 0021600203 scopus 로고
    • Practical computation of unsteady lift
    • Beddoes T S 1984 Practical computation of unsteady lift Vertica 8 55-71
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    • Beddoes, T.S.1
  • 33
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    • Modeling of subsonic unsteady aerodynamics for rotary wing applications
    • Leishman J G 1990 Modeling of subsonic unsteady aerodynamics for rotary wing applications J. Am. Helicopter Soc. 35 29-38
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    • Leishman, J.G.1
  • 36
    • 0343425446 scopus 로고
    • Determination of indicial lift and moment of a 2-D pitching airfoil at subsonic mach numbers for oscillatory coefficients with numerical calculations for a mach number of 0.7
    • Mazelsky B 1952 Determination of indicial lift and moment of a 2-D pitching airfoil at subsonic mach numbers for oscillatory coefficients with numerical calculations for a mach number of 0.7 NACA TN 2613
    • (1952) NACA TN 2613
    • Mazelsky, B.1
  • 37
    • 0027593903 scopus 로고
    • Indicial lift approximations for two-dimensional subsonic flow as obtained by oscillatory measurements
    • Leishman J G 1993 Indicial lift approximations for two-dimensional subsonic flow as obtained by oscillatory measurements AIAA J. Aircraft 30 340-51
    • (1993) AIAA J. Aircraft , vol.30 , pp. 340-351
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  • 38
    • 0030737188 scopus 로고    scopus 로고
    • Indicial aerodynamics in compressible flow - Direct calculations
    • Parameswaran V and Baeder J D 1997 Indicial aerodynamics in compressible flow - direct calculations AIAA J. Aircraft 34 131-3
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    • Parameswaran, V.1    Baeder, J.D.2
  • 40
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    • Unsteady lift of a flapped airfoil by indicial concepts
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  • 42
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    • Theory of noise generation from moving bodies with an application to helicopter rotors
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.