Experimental results are analyzed to develop an understanding of the n
ow physics causing fiat spin of axisymmetric bodies, which is a key to
the development of the capability for the prediction of the nat spin
of advanced aircraft. The flow phenomenon sustaining the flat spin mot
ion is the now separation asymmetry due to the moving wall effect at l
ocally critical flow conditions on the body, which is made possible by
the presence of three-dimensional now effects. Body roughness and mic
roasymmetry play important roles in extending the range of ambient now
conditions at which nat spin can develop.