2.2. PROTOCOLOS DE CAPA ENLACE PARA ALTA DISPONIBILIDAD
2.2.2. RAPID SPANNING TREE PROTOCOL (RSTP)
Due to the jump in velocity across the duct vortex wake (Figure 3.3) it was found necessary to adopt the procedure outlined in Section 5.5 to account for propulsor slipstream contraction.
These modifications together with the formulation of the ducted propulsor design method will now be detailed in the coming Chapters.
References
1) SilverleafjA. "Prospects for Unconventional Marine Propulsion Devices", 7th
Symposium on Naval Hydrodynamics, Office of Naval Research, Arlington Va., USA, August 1968
2) Borges,!. "Three Dimensional Inverse Design of Turbomachinery", Ph.D.
Thesis, Cambridge University Engineering Department, Cambridge, 1986
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Thesis, Cambridge University Engineering Department, Cambridge, 1988
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Engineering Systems", Cambridge Engine Technology Series, Cambridge University Press, 1991
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pp454-470, J. Mech. Eng. Sci., Vol. 11, No.5, 1969
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Flow in Turbomachinery Blade Passages", p82, ASME Journal of Engineering for Gas Turbines and Power, Vol. 104, April 1982
7) Wilkinson,D.H. "A Numerical Solution of the Analysis and Design Problems for
the Flow Past One or More Aerofoils", Aeronautical Research Council Reports and Memoranda (ARC R & M) No. 3545, London, April 1967
8) Novak,R.A., Haymann-Haber,G. "A Mixed-Flow Cascade Passage Design Procedure Based on a Power Series Expansion", p231, ASME Journal of Engineering for Gas Turbines and Power, Vol. 105, April 1983
9) Betz,A., Flugge-Lotz,I. "Design of Centrifugal Impeller Blades", NACA TM-
902,1939
10) Hawthome,W.R., Wang,C., Tan,C.S., McCune,J.E. "Theory of Blade Design for Large Deflections: Part I - Two-Dimensional Cascade", ASME Journal of Engineering for Gas Turbines and Power, Vol. 106, April 1984
11) Jennions,I.K., Stow,P. "A Quasi-Three-Dimensional Turbomachinery Blade Design System: Part I - Throughflow Analysis", p301, ASME Journal of Engineering for Gas Turbines and Power, Vol. 107, April 1985
12) Jennions,I.K., Stow,P. "A Quasi-Three-Dimensional Turbomachinery Blade Design System: Part II - Computerised System", p308, ASME Journal of Engineering for Gas Turbines and Power, Vol. 107, April 1985
13) Dang,T.Q. "A Fully Three-Dimensional Inverse Method for Turbomachinery Blading in Transonic Flows", ASME Paper 92-GT-209, 1992
14) Zhao,X., Sun,C., Wu,C. "A Simple Method for Solving Three-Dimensional Inverse Problems of Turbomachine Flow and the Annular Constraint Condition", p293, ASME Journal of Engineering for Gas Turbines and Power, Vol.107, April 1985
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16) Tan,C.S., Hawthorne,W.R., McCune,J.E., Wang,C. "Theory of Blade Design
for Large Deflections: Part II - Annular Cascades", ASME Journal of
Engineering for Gas Turbines and Power, Vol. 106, April 1984
17) Lamb,H. "Hydrodynamics", p248. Sixth Edition, Cambridge University Press, 1932
18) Hawthorne,W.R. "The Actuator Duct Representation of Turbomachinery Blade Rows", CUED/A - Turbo/TR 119, Cambridge University Engineering Department, Cambridge, 1983
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28) Dawes,W.N. "Application of Full Navier-Stokes Solvers to Turbomachinery Flow Problems", VKI Lecture Series 2: Numerical Techniques for Viscous Flow Calculations in Turbomachinery Blading, 1986
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30) Dixon,S.L. "Fluid Mechanics, Thermodynamics of Turbomachinery", p2. Third Edition, Pergamon Press, 1978
Rotor Blades Outlet V anes
Flow
(a) Single Stage Axial Flow Compressor or Pump
Rotor Blades
Outlet V anes Flow
(b) Mixed Flow Pump
Flow Direction
Outlet Diffuser
V aneless Diffuser
Volute
Impeller
Guide V anes Runner Blades
Flow Flow
Draught Tube
(c) Centrifugal Compressor or Pump
(d) Francis Turbine (Mixed Flow Type)
Guide V anes
Flow Flow
Draught Tube or Diffuser
(e) Kaplan Turbine
Nozzle Wheel Inlet Pipe F lo w - J e t (f) Pelton Wheel F i g u r e 3 . 1 : D i a g r a m m a t i c F o r m o f V a r i o u s T y p e s o f T u r b o m a c h i n e (as P r e s e n t e d b y D i x o n [30])
Mu I t i p I e BI ode Rows