The problem of design parameters selection of the turbine engine is the most important task at the preliminary design stage of the multi-purpose aircraft. A special feature of the multi-purpose aircraft mission is a sudd...
Ryszard Szczepanik (2013). ANALYSIS OF 1ST STAGE COMPRESSOR
ROTOR BLADE STRESS AND VIBRATION AMPLITUDES
IN ONE-PASS JET ENGINE. Journal of KONES, 20(4),
441-450. https://europub.co.uk/articles/-A-71115
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