The objective is to develop efficient numerical techniques for the study of aeroelastic response of a propfan in an unsteady transonic flow. A three dimensional unsteady Euler solver is being modified to address this problem.
Numerical simulation of unsteady rotational flow over propfan configurations
AIAA 28th Aerospace Sciences Meeting and Exhibit ; 1990 ; Reno, NV, United States
01.11.1989
Aufsatz (Konferenz)
Keine Angabe
Englisch