A survey is presented of inviscid theoretical methods that are useful in the study of lift-generated vortices. Concepts derived using these invisicid theories are cited which have helped to guide research directed at alleviating the velocities and rolling moments imposed on aircraft entering these wakes.
Inviscid modeling of aircraft trailing vortices
01.01.1977
Aufsatz (Konferenz)
Keine Angabe
Englisch
Inviscid to turbulent transition of trailing vortices
AIAA | 1975
|Inviscid to turbulent transition of trailing vortices
NTRS | 1975
|Merging of Aircraft Trailing Vortices
AIAA | 1977
|Merging of aircraft trailing vortices
AIAA | 1977
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