ESDU 66031
Introductory sheet on subcritical lift-dependent drag of wings.
Abstract:
ESDU 66031 discusses the various contributions to the drag of a lifting wing of moderate to high aspect ratio in subcritical viscous flow, considering both a cambered and twisted wing and a plane symmetrical section wing. A method of analysis is discussed for the case of plane symmetrical section wings; it uses ESDU 74035 to determine the drag due to trailing vortices and applies a correction for lift dependent drag due to boundary layer developed in ESDU 66032.Indexed under:
Details:
| Data Item ESDU 66031 | |
|---|---|
| Format: |
|
| Status: |
|
| Previous Releases: |
|
| ISBN: |
|
The Data Item document you have requested is available only to subscribers or purchasers.
- Subscribers login here.
- If you are not an ESDU subscriber you can
- find out how to subscribe, or
- purchase this Data Item from the Standards Store.