Abstract: This paper describes a methodology and a fully tested and calibrated mathematical model for the treatment of endwall effects in axial compressor aerodynamic calculations. Additional losses and deviations caused by the ...

Abstract: This paper describes a new universal algebraic model for the estimation of flow deflection and losses in axial compressor inlet guide vane devices. The model deals with nominal flow and faroffdesign operating conditions ...

Abstract: In the published paper, the expressions listed under (51) were miswritten. The correct version is (51)–for a rotor:–for a stator:(w2/w1)T<Ctc(WRmin)T/1.3(w2/w1)A<(WRmin)A(w2/w1)H<(WRmin)H/1.3(w2/w1)T<(WRmin)T ...

Abstract: The approach applied in various research papers that model compressor shock losses is valid only for certain types of airfoil cascades operating in a narrow range of working conditions. Lately, more general shock loss ...

Abstract: Abstract. Next-generation aircraft with boundary layer ingesting (BLI) engines can reduce fuel consumption but pose challenges for fan and compressor operation due to inlet distortion. To optimize the design of such engines, ...

Abstract: As a consequence of the increasing share of volatile renewable energy sources such as wind and solar in present-day electrical grid systems, time variations of the power demand for fossil fuel plants can become more sudden. ...