Wajid Hasan1 and C. P. Singh2
Abdul Razaq*, Muhammad Jamal Khan*, Tahir Sarwar* and Mohammad Jamal Khan**
Aamir Saleem1, Arshad Mahmood Malik2*, Najam Ul Hassan1 and Imtiaz A. Qamar3
Tajwali Khan1*, Ihtzaz Qamar1, Feroz Shah2, Kareem Akhtar2, Rehman Akhtar3
engine based on heat and mass transfer. Effect of the fuel droplet curvature on vapor pressure is incorporated in the
model. The model is applied on a small-scale combustion chamber of bi-propellant liquid rocket engine where fuel
concentration away from droplet is not zero. A code is generated a...
Muhammad Irfan*, Saeed Gul*, Mohammad Younas*
Asad Naeem Shah1,2, GE Yun-shan1, HE Chao1,3