245mi - architettura navale · 2020. 12. 23. · 245mi - architettura navale a.a. 2020/21 propeller...

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245MI - Architettura Navale A.A. 2020/21 Propeller geometry Docente: Prof. Mitja Morgut Università degli Studi di Trieste Dipartimento di Ingegneria e Architettura Via A. Valerio 10, 34127 Trieste Edificio C5 - Stanza C5_2.44 mail: [email protected]

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  • 245MI - Architettura NavaleA.A. 2020/21

    Propeller geometry

    Docente: Prof. Mitja MorgutUniversità degli Studi di TriesteDipartimento di Ingegneria e ArchitetturaVia A. Valerio 10, 34127 TriesteEdificio C5 - Stanza C5_2.44mail: [email protected]

  • Geometry Airfoil Scale effects

    Frames of reference

    Architettura Navale, A.A. 2020/21

    Global reference frame Local reference frame

  • Geometry Airfoil Scale effects

    Propeller reference lines

    Architettura Navale, A.A. 2020/21

  • Geometry Airfoil Scale effects

    Cylindrical sections

    Architettura Navale, A.A. 2020/21

  • Geometry Airfoil Scale effects

    Pitch

    Architettura Navale, A.A. 2020/21

    Definition of helix Definition of pitch angle

  • Geometry Airfoil Scale effects

    Pitch lines

    Architettura Navale, A.A. 2020/21

  • Geometry Airfoil Scale effects

    Mean pitch

    Architettura Navale, A.A. 2020/21

  • Geometry Airfoil Scale effects

    Skew

    Architettura Navale, A.A. 2020/21

  • Geometry Airfoil Scale effects

    Total rake (and the expanded view)

    Architettura Navale, A.A. 2020/21

  • Geometry Airfoil Scale effects

    Propeller outlines and area

    Architettura Navale, A.A. 2020/21

    Approximation: AD ≈ AE

  • Geometry Airfoil Scale effects

    Example

    Architettura Navale, A.A. 2020/21

  • Geometry Airfoil Scale effects

    Example

    Architettura Navale, A.A. 2020/21

  • Geometry Airfoil Scale effects

    Airfoil

    Architettura Navale, A.A. 2020/21

    CL =L

    0.5ρAV 2

    CD =D

    0.5ρAV 2

    A = chord× span

  • Geometry Airfoil Scale effects

    Propeller scale effects - 1978 ITTC performance prediction method

    Architettura Navale, A.A. 2020/21

    ReM(0.75R) =V0.75R c

    νM

    V =√

    V 2A + (0.75πnD)2

    KTS = KTM −∆KTKQS = KQM −∆KQ

    ∆KT =−0.3∆CD(

    P

    D

    )(cZ

    D

    )∆KQ = 0.25∆CD

    (cZ

    D

    )∆CD =∆CDM −∆CDS

    ∆CDM = 2(1+ 2t

    c

    )[0.044

    (ReM(0.75R))1/6− 5

    (ReM(0.75R))2/3

    ]

    ∆CDS = 2(1+ 2t

    c

    )[1.89+1.62log10

    (c

    Kp

    )]−2.5

    GeometryFrames of reference

    AirfoilScale effects