URI(s)
Identifies LC/NAF RWO
Exact Matching Concepts from Other Schemes
Sources
- found: Aerodynamic characteristics of several 6-percent-thick airfoils at angles of attack from 0° to 20° at high subsonic speeds, 1955:title page (Bernard N. Daley)
Instance Of
Scheme Membership(s)
Collection Membership(s)
Change Notes
- 2022-01-21: new
- 2022-01-22: revised
Alternate Formats