ESDU 11007 describes an alternative procedure for implementing viscous effects using a method to add a frozen boundary layer to the wing surface in the form of a displacement thickness with corrections for sweep. The method is subsonic with compressibility corrections and has been enhanced to give an improved calculation of sectional viscous drag. The addition of this item enables the FP method to be used as a rapid assessment tool to provide initial aerodynamic qualities of wings as part of the design process.
Produits p\xe9troliers et lubrifiants - D\xe9termination des caract\xe9ristiques antirouille des graisses lubrifiantes
| IHS ESDU | Accuris | |
|---|---|---|
| Product Category | Standards and Technical Documents | Standards and Technical Documents |
| Product Number | 11007 | 11007 |
| Product Name | Full-potential method for three-dimensional wings and wing-body combinations Part 6: Full-potential with frozen boundary layer | Produits p\xe9troliers et lubrifiants - D\xe9termination des caract\xe9ristiques antirouille des graisses lubrifiantes |
