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.
F-15 wind-tunnel/flight correlations
1982-06-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
X-29A for NTF wind-tunnel/flight correlations
NTRS | 1982
|Numerical Correlations Between Flight and Plasma Wind-Tunnel Tests
Online Contents | 1997
|