IHS ESDU 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. 82010

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.
  • 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. - 82010 - IHS ESDU
    IHS ESDU
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.

Suppliers

Company
Product
Description
Supplier Links
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. - 82010 - IHS ESDU
IHS ESDU
London, United Kingdom
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.
82010
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. 82010
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.

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.

Buy Now

Technical Specifications

  IHS ESDU
Product Category Standards and Technical Documents
Product Number 82010
Product Name 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.
Unlock Full Specs
to access all available technical data

Similar Products