This fourth 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: 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 (HCF) Science and Technology Program 2000 Annual Report
2000
219 pages
Report
Keine Angabe
Englisch
Nonferrous Metals & Alloys , Jet & Gas Turbine Engines , Aircraft engines , Gas turbines , Fatigue(Mechanics) , Stresses , Vibration , Shock waves , Damping , Passive systems , High strength alloys , Fan blades , Airfoils , Laser beams , Propulsion systems , Surface properties , Instrumentation , Paints , Traveling waves , Water impingement , Damage tolerance , High cycle fatigue , Aeromechanical characterization , Component analysis , Forced response , Lsp(Laser shock peening) , Surface treatments , Turbine engines , Nsms(Noninterference stress measurement system) , Ihptet(Integrated high performance turbine engine technology) , Xtc-76/2 engine , Xtc-66 engineWuafrlapplto04