Aerodynamic forces and moments for a slender wing-body configuration are summarized from an investigation in the Langley National Transonic Facility (NTF). The results include both longitudinal and lateral-directional aerodynamic properties as well as slideslip derivatives. Results were selected to emphasize Reynolds number effects at a transonic speed although some lower speed results are also presented for context. The data indicate nominal Reynolds number effects on the longitudinal aerodynamic coefficients and more pronounced effects for the lateral-directional aerodynamic coefficients. The Reynolds number sensitivities for the lateral-directional coefficients were limited to high angles of attack.
Reynolds Number Effects on the Transonic Aerodynamics of a Slender Wing-Body Configuration
1989
18 pages
Report
Keine Angabe
Englisch
Nonlinear slender wing aerodynamics
AIAA | 1976
|Low-Reynolds-Number Effects on Delta-Wing Aerodynamics
Online Contents | 1998
|Low-Reynolds-Number Effects on Delta-Wing Aerodynamics
AIAA | 1998
|