Unsteady, vortex-dominated flowfields are presently studied by using the conical Euler equations as an efficient first step toward investigation of the full three-dimensional problem, under the assumption that the supersonic flow about a delta wing is conical and therefore allows the three-dimensional problem to be reduced to a two-dimensional one. Attention is given to the case of a delta wing undergoing wing-rock motion. The code developed has also been modified to allow treatment of the 'free-to-roll' case.
Conical Euler simulation of wing rock for a delta wing planform
Journal of Aircraft ; 28
1991-01-01
Sonstige
Keine Angabe
Englisch
Hingeless flow control over a delta wing planform
AIAA | 2000
|Hingeless Flow Control over a Delta-Wing Planform
AIAA | 2002
|Hingeless Flow Control Over A Delta Wing Planform
British Library Conference Proceedings | 2000
|