1. Cost/benefit of advanced materials technologies for future aircraft turbine engines;Stephens,1980
2. Performance of two-layer thermal barrier systems on directionally solidified Ni-Al-Mo and comparative effects of alloy thermal expansion on system life;Stecura;NASA Tech. Memo. 81604,1980
3. Two-layer thermal barrier coating for turbine airfoils—furnace and burner rig results;Stecura;NASA Tech. Memo. X-3425,1976
4. Durability of zirconium thermal barrier ceramic coatings on air-cooled turbine blades in cyclic jet engine operations;Liebert;NASA Tech. Memo. X-3410,1976
5. Thermal barrier coatings: burner rig hot corrosion test results;Hodge;NASA Tech. Memo. 79005,1978