ESDU 71018
Approximate wave drag of rectangular planform fairings at zero incidence in supersonic flow.
Abstract:
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.Indexed under:
- Double-Wedge Section Wings
- Double-Wedge Sections
- Parabolic-Arc Section Fairings
- Parabolic-Arc Section Wings
- Ramp Fairings
- Rectangular Wings
- Wave Drag
Details:
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