![ESDU AERO F.02.01.07:1993 ESDU AERO F.02.01.07:1993](https://cdn.pdfstandards.shop/wp-content/uploads/woocommerce-placeholder-300x300.png)
ESDU AERO F.02.01.07:1993
$62.40
Conversion factor for profile drag increment for part-span flaps
Published By | Publication Date | Number of Pages |
ESDU | 1993-02-01 | 3 |
ESDU Aero F.02.01.07 gives curves that provide factors to correct the profile drag increment due to deflection of a full-span flap to give the increment for a part-span flap with arbitrary spanwise position. The curves are a function of taper ratio and apply to straight-tapered wings. They may be used with the full-span increments from ESDU 74010 for split flaps, from ESDU 87024 for plane flaps, and from ESDU 08013 for single-slotted flaps.