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ESDU 82010 D [ Active ]

Contribution of fin to sideforce, yawing moment and rolling moment derivatives due to sideslip, (Yv)F, (Nv)F, (Lv)F, in the presence of body, wing and tailplane

standard by Engineering Sciences Data Unit , 02/01/2017

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Full Description

ESDU 82010 provides a method for estimating the contribution of a fin to the sideforce, yawing moment and rolling moment derivatives due to sideslip for aircraft at subsonic speeds. The data are applicable where there is a linear variation of lift coefficient with angle of attack and a linear variation of sideforce, yawing moment and rolling moment coefficients with angle of sideslip.

Discussions of the effects due to the presence of a dorsal fin and of rear-fuselage mounted jet-engine nacelles are included.

 

Product Details

Edition:
82#
Published:
02/01/2017
Number of Pages:
37
File Size:
1 file , 1 MB
Product Code(s):
4, 4
 

Document History

  1. ESDU 82010 D

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    Contribution of fin to sideforce, yawing moment and rolling moment derivatives due to sideslip, (Yv)F, (Nv)F, (Lv)F, in the presence of body, wing and tailplane

    • Most Recent

  2. ESDU 82010 C


    Contribution of fin to sideforce, yawing moment and rolling moment derivatives due to sideslip, (Y sub v) sub F, (N sub v) sub F, (L sub v) sub F, in the presence of body, wing and tailplane.

    • Historical Version