Abstract A formalized decision-making process is presented to choose an arrangement of bypass engine turbocompressor supports at the draft design stage. The elements of the theory of graphs and mathematical logic are used in the process of formalization.
Choice of support arrangement in designing two-support rotors of gas turbine engines
Russian Aeronautics (Iz VUZ) ; 53 , 1 ; 51-56
2010-03-01
6 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Choice of support arrangement in designing two-support rotors of gas turbine engines
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