The influence of multiple high pressure, supersonic, radial or tangential jets, that are injected from the circumference of the base plane of an axisymmetric body, on its longitudinal aerodynamic coefficients in transonic flow is studied experimentally. The interaction of the jets with the body flow field increases the pressures on the forebody, thus altering its lift and static stability characteristics. It is shown that, within the range of parameters studied. This interaction has a stabilizing effect on the body. The contribution to lift and stability is significant at small angles of attack and decreases nonlinearly at higher angles when the crossflow mechanism becomes dominant.
Interaction of multiple supersonic jets with a transonic flow field
AIAA Fluid and Plasma Dyn. Conf. ; 1983 ; Danvers, MA, United States
1983-05-01
Report
Keine Angabe
Englisch
Near-Field Flow of Supersonic Swirling Jets
Online Contents | 1995
|Near-field flow of supersonic swirling jets
AIAA | 1995
|