This third annual report of the National Turbine Engine High Cycle Fatigue (HCF) Program is a brief review of work completed, work in progress, and technical accomplishments. This program is a coordinated effort with participation by the Air Force, the Navy, and NASA. The technical efforts are organized under eight Action Teams including: Materials Damage Tolerance Research, Forced Response Prediction, Component Analysis, Instrumentation, Passive Damping Technology, Component Surface Treatments, Aeromechanical Characterization, and Engine Demonstration. Daniel E. Thomson, AFRL/PRTC, Wright-Patterson AFB, is the Program Manager.
High Cycle Fatigue Science and Technology Program 1999 Annual Report
2000
154 pages
Report
Keine Angabe
Englisch
Aeronautics , Jet & Gas Turbine Engines , Nonferrous Metals & Alloys , Materials Degradation & Fouling , Aircraft engines , Gas turbines , Fatigue(Mechanics) , Stresses , Vibration , Passive systems , Shock waves , Damping , High strength alloys , Fan blades , Airfoils , Laser beams , Propulsion systems , Surface properties , Instrumentation , Traveling waves , Water impingement , Damage tolerance , High cycle fatigue , Nsms(Noninterference stress measurement system) , Forced response , Ihptet(Integrated high performance turbine engine technology) , XTC-76/2 engine , XTC-66 engines , Aeromechanics , Surface treatments , Lsp(Laser shock peening) , AFRL(Air Force Research Laboratory) , PRTC(Propulsion Directorate Turbine Engine Division Components Branch)
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