7 . Ma [1+k_1 xal ) (para a record The following equations explains the change in Mach number as a result of compressible fluid flow under adiabatic conditions in a constant area duct +] M dMa = 1 - Ma 2 Prove that the above differential form can be converted to following equation after integration using suitable integration limits. Lmax 1 - Mar +1, (y + 1)M2 4f + In D yM 2y 2(1+12) Where Lmax" is the maximum length to reach at chocked condition. 7 . Ma [1+k_1 xal ) (para a record The following equations explains the change in Mach number as a result of compressible fluid flow under adiabatic conditions in a constant area duct +] M dMa = 1 - Ma 2 Prove that the above differential form can be converted to following equation after integration using suitable integration limits. Lmax 1 - Mar +1, (y + 1)M2 4f + In D yM 2y 2(1+12) Where Lmax" is the maximum length to reach at chocked condition