<DOC>
<DOCNO>
358
</DOCNO>
<TITLE>
on the model of the free shock separation, turbulent
boundary layer .
</TITLE>
<AUTHOR>
mager,a.
</AUTHOR>
<BIBLIO>
j. ae. scs. 1956, 181.
</BIBLIO>
<TEXT>
  by free shock-separated boundary layers, one means that type of separation
where the flow downstream of the separation region is free to
adjust to any direction that may result from the shock-boundary-layer
interaction process .  a detailed model of the free shock-separated turbulent
boundary layer is postulated, and the pressure rise following
from this model is estimated and compared with experiments .  the results
are applied to the prediction of separation in an overexpanded
nozzle .
</TEXT>
</DOC>
