IHS ESDU Contribution of fin to sideforce, yawing moment and rolling moment derivatives due to rate of yaw, (Y sub r) sub F, (N sub r) sub F, (L sub r) sub F. 82017

Description
ESDU 82017 provides a method for estimating the contribution of a fin to the sideforce, yawing moment and rolling moment derivatives due to rate of yaw 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 rate of yaw, (Y sub r) sub F, (N sub r) sub F, (L sub r) sub F. - 82017 - IHS ESDU
    IHS ESDU
Description
ESDU 82017 provides a method for estimating the contribution of a fin to the sideforce, yawing moment and rolling moment derivatives due to rate of yaw 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.

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Contribution of fin to sideforce, yawing moment and rolling moment derivatives due to rate of yaw, (Y sub r) sub F, (N sub r) sub F, (L sub r) sub F. - 82017 - IHS ESDU
IHS ESDU
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Contribution of fin to sideforce, yawing moment and rolling moment derivatives due to rate of yaw, (Y sub r) sub F, (N sub r) sub F, (L sub r) sub F.
82017
Contribution of fin to sideforce, yawing moment and rolling moment derivatives due to rate of yaw, (Y sub r) sub F, (N sub r) sub F, (L sub r) sub F. 82017
ESDU 82017 provides a method for estimating the contribution of a fin to the sideforce, yawing moment and rolling moment derivatives due to rate of yaw 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 82017 provides a method for estimating the contribution of a fin to the sideforce, yawing moment and rolling moment derivatives due to rate of yaw 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.

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Technical Specifications

  IHS ESDU
Product Category Standards and Technical Documents
Product Number 82017
Product Name Contribution of fin to sideforce, yawing moment and rolling moment derivatives due to rate of yaw, (Y sub r) sub F, (N sub r) sub F, (L sub r) sub F.
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