2832869

ESDU 74010 A [ Active ]

Low-speed drag coefficient increment at zero lift due to full-span split flaps.

standard by Engineering Sciences Data Unit , 11/01/1974

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Full Description

ESDU 74010 gives curves of drag increment at zero lift as a function of wing thickness/chord ratio and flap deflection for various flap chord/wing chord ratios between 0.1 and 0.4. The curves are based on a correlation of experimental data from 10 sources, and are accurate to within 10 per cent for rectangular wings and within 20 per cent for straight-tapered swept and unswept wings. To correct the data for application to part-span flaps, ESDU Aero F.02.01.07 is used.

 

Product Details

Edition:
74
Published:
11/01/1974
Number of Pages:
12
File Size:
1 file , 320 KB
Product Code(s):
3, 3