In this example the metastable titanium Ti-5Al-5Mo-5V-3Cr (Ti-5553) (wt.%) alloy has been developed recently to replace the alloy Ti-10V-2Fe-3Al (Ti-1023) in some of the structural components of the aircraft. The microstructure, texture and mechanical properties of the alloy Ti-5553 and similar Mo equivalent (8.15).
For more details about Mo equivalent calcuation, you can see the paper:
Weiss ,I. & Semiatin, S.L. (1998). Thermomechanical processing of beta titanium alloys–An overview. Materials Science and Engineering: A,243(1),46–65.
Weiss, I., & Semiatin, S. L. (1998). Thermomechanical processing of beta titanium alloys—an overview. Materials Science and Engineering: A, 243(1-2), 46–65. doi:10.1016/s0921-5093(97)00783-1
Ti-5Al-5Mo-5V-3Cr and similar Mo equivalent alloys: First principles calculations and experimental investigations you please go through this research paper