Engineers Manual  was used. ... Three input fields in the program were created to allow the user to account for: (1) drag reduction; (2) system weight increase; (3) SFC increase. As the ... In the Boeing report  the total drag for the baseline 757 -200 at 37000ft at Mach 0.80 for a lift coefficient of 0.50, was given as 0.03079.
|Title||:||Aerodynamic Drag Reduction Technologies|
|Publisher||:||Springer Science & Business Media - 2013-06-29|