A potential-flow based panel method was used to compute the aerodynamic loads along a three-dimensional flight path. Comparisons were made with rotary rig tests of an airplane performing a coning motion and found to compare well with the main components of the aerodynamic forces. The effect of the sting-type wind tunnel mounting of the model on the measured loads was briefly investigated, and the possible benefits of using this method combined with wind tunnel experiments were highlighted.
Numerical simulation of aircraft rotary aerodynamics
Numerische Simulation der Flugzeug-Rotationsaerodynamik
AIAA-Papers ; Jan ; 1-6
1988
6 Seiten, 13 Bilder, 16 Quellen
Aufsatz (Konferenz)
Englisch
Numerical simulation of aircraft rotary aerodynamics
AIAA | 1988
|Numerical simulation of aircraft rotary aerodynamics
NTRS | 1989
|Numerical simulation of aircraft rotary aerodynamics
NTRS | 1988
|Numerical simulation of aircraft rotary aerodynamics
AIAA | 1989
|