IHS ESDU Approximate wave drag of rectangular planform fairings at zero incidence in supersonic flow. 71018

Description
ESDU 71018 provides a simple method of estimating the wave drag due to rectangular planform fairings at zero incidence in supersonic flow. The data, which were derived using linearised supersonic flow theory, apply to fairings with constant streamwise section of "two- or three-slope" or parabolic profile.
Description
ESDU 71018 provides a simple method of estimating the wave drag due to rectangular planform fairings at zero incidence in supersonic flow. The data, which were derived using linearised supersonic flow theory, apply to fairings with constant streamwise section of "two- or three-slope" or parabolic profile.

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Approximate wave drag of rectangular planform fairings at zero incidence in supersonic flow. - 71018 - IHS ESDU
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Approximate wave drag of rectangular planform fairings at zero incidence in supersonic flow.
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Approximate wave drag of rectangular planform fairings at zero incidence in supersonic flow. 71018
ESDU 71018 provides a simple method of estimating the wave drag due to rectangular planform fairings at zero incidence in supersonic flow. The data, which were derived using linearised supersonic flow theory, apply to fairings with constant streamwise section of "two- or three-slope" or parabolic profile.

ESDU 71018 provides a simple method of estimating the wave drag due to rectangular planform fairings at zero incidence in supersonic flow. The data, which were derived using linearised supersonic flow theory, apply to fairings with constant streamwise section of "two- or three-slope" or parabolic profile.

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Technical Specifications

  IHS ESDU
Product Category Standards and Technical Documents
Product Number 71018
Product Name Approximate wave drag of rectangular planform fairings at zero incidence in supersonic flow.
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