Aerodynamic Drag Reduction Technologies

Aerodynamic Drag Reduction Technologies

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Engineers Manual [8] 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 [9] 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
Author:Peter Thiede
Publisher:Springer Science & Business Media - 2013-06-29


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