Let me write this T by W max square into L by D square Z and rate of climb maximum, this is for jet, for a propeller it is np by W minus 0.8776 under root W by S rho CD naught 1 by L by D 3 by 2 and of course, here the Z equal to 1 plus under root 1 plus 3 L by D square into T by W max square something like this.
ನಾನು T by W max square into L by D square Z ಮತ್ತು ಗರಿಷ್ಠ rate of climbವನ್ನು ಬರೆಯುತ್ತೇನೆ, ಇದು ಜೆಟ್ ಗಾಗಿರುತ್ತದೆ, ಒಂದು ಪ್ರೊಪೆಲ್ಲರ್ಗೆ ಇದು np by W minus 0.8776 under root W by S rho CD naught 1 by L by D 3 by 2 ರಿಂದ ಮತ್ತು ಸಹಜವಾಗಿ, Z equal to 1 plus under root 1 plus 3 L by D square into T by W max square ಈ ರೀತಿಯದ್ದಾಗಿದೆ.