NATIONAL AERONAUTICS AND SPACE ADMINISTRATION CLEVELAND OH GLENN RESEARCH CENTER, Zhu, Dongming, Fox, Dennis S., Miller, Robert A., Ghosn, Louis J., Kalluri, Sreeramesh, NATIONAL AERONAUTICS AND SPACE ADMINISTRATION CLEVELAND OH GLENN RESEARCH CENTER, Zhu, Dongming, Fox, Dennis S., Miller, Robert A., Ghosn, Louis J., and Kalluri, Sreeramesh
The development of advanced high performance constant-volume-combustion-cycle engines (CVCCE) requires robust design of the engine components that are capable of enduring harsh combustion environments under high frequency thermal and mechanical fatigue conditions. In this study, a simulated engine test rig has been established to evaluate thermal fatigue behavior of a candidate engine combustor material, Haynes 188, under superimposed CO2 laser surface impulsive thermal loads (30 to 100 Hz) in conjunction with the mechanical fatigue loads (10 Hz). The mechanical high cycle fatigue (HCF) testing of some laser pre-exposed specimens has also been conducted under a frequency of 100 Hz to determine the laser surface damage effect. The test results have indicated that material surface oxidation and creep-enhanced fatigue is an important mechanism for the surface crack initiation under the simulated CVCCE engine conditions., Presented at the International Conference on Metallurgical Coatings and Thin Films sponsored by the AVS Science and Technology Society, Advanced Surface Engineering Division, San Diego, California on April 19-23, 2004. Grant no. WBS-22-708-03-04.