APA (7th ed.) Citation

Bashir, M., Khan, S. A., & Rajendran, P. (2015). Combined effect of nozzle pressure ratio and screech prone supersonic mach number in a suddenly expanded flow.

Chicago Style (17th ed.) Citation

Bashir, Musavir, Sher Afghan Khan, and Parvathy Rajendran. Combined Effect of Nozzle Pressure Ratio and Screech Prone Supersonic Mach Number in a Suddenly Expanded Flow. 2015.

MLA (8th ed.) Citation

Bashir, Musavir, et al. Combined Effect of Nozzle Pressure Ratio and Screech Prone Supersonic Mach Number in a Suddenly Expanded Flow. 2015.