Unknown
Publication Date:
2011-08-18
Description:
F-15 correlation data for longitudinal control and inlet-ramp effectiveness, and horizontal-tail setting for trim are presented. The Reynolds number effect on airfoil laminar bubble burst is included.
Keywords:
AERODYNAMICS
Type:
NASA. Langley Research Center Wind-Tunnel(Flight Correlation, 1981; p 109-115
Format:
text
|
Location |
Call Number |
Expected |
Availability |