IHS ESDU Estimation of rolling moment derivative due to sideslip for complete aircraft at subsonic speeds. 81032

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ESDU 81032 illustrates the estimation of the rolling moment derivative due to sideslip for complete aircraft at subsonic speeds. It shows how to combine the ESDU methods for predicting the contributions of the separate parts of the aircraft. It covers cruise, landing and take-off configurations and is applicable where there is a linear variation of lift coefficient with angle of attack and of rolling moment coefficient with angle of sideslip.
Description
ESDU 81032 illustrates the estimation of the rolling moment derivative due to sideslip for complete aircraft at subsonic speeds. It shows how to combine the ESDU methods for predicting the contributions of the separate parts of the aircraft. It covers cruise, landing and take-off configurations and is applicable where there is a linear variation of lift coefficient with angle of attack and of rolling moment coefficient with angle of sideslip.

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Estimation of rolling moment derivative due to sideslip for complete aircraft at subsonic speeds. - 81032 - IHS ESDU
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Estimation of rolling moment derivative due to sideslip for complete aircraft at subsonic speeds.
81032
Estimation of rolling moment derivative due to sideslip for complete aircraft at subsonic speeds. 81032
ESDU 81032 illustrates the estimation of the rolling moment derivative due to sideslip for complete aircraft at subsonic speeds. It shows how to combine the ESDU methods for predicting the contributions of the separate parts of the aircraft. It covers cruise, landing and take-off configurations and is applicable where there is a linear variation of lift coefficient with angle of attack and of rolling moment coefficient with angle of sideslip.

ESDU 81032 illustrates the estimation of the rolling moment derivative due to sideslip for complete aircraft at subsonic speeds. It shows how to combine the ESDU methods for predicting the contributions of the separate parts of the aircraft. It covers cruise, landing and take-off configurations and is applicable where there is a linear variation of lift coefficient with angle of attack and of rolling moment coefficient with angle of sideslip.

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Technical Specifications

  IHS ESDU
Product Category Standards and Technical Documents
Product Number 81032
Product Name Estimation of rolling moment derivative due to sideslip for complete aircraft at subsonic speeds.
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