Aeromechanical Design of Damped High Pressure Turbine Blades Subject to Low Engine Order Forcing
Symposium, Evaluation, control and prevention of high cycle fatigue in gas turbine engines for land, sea and air vehicles ; 2005 ; Granada, Spain
Evaluation, control and prevention of high cycle fatigue in gas turbine engines for land, sea and air vehicles ; 121 ; Paper 29
01.01.2005
Paper 29
Held on CD-ROM
Aufsatz (Konferenz)
Englisch
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Aeromechanical stability of rotorcraft with advanced geometry blades
Tema Archiv | 1993
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