<DOC>
<DOCNO>
31
</DOCNO>
<TITLE>
thermal buckling of supersonic wing panels .
</TITLE>
<AUTHOR>
hoff,n.j.
</AUTHOR>
<BIBLIO>
j. ae. scs. 23, 1956, 1019.
</BIBLIO>
<TEXT>
  the temperature and thermal stress distributions are analyzed
in multicellular supersonic wing structures .  a buckling criterion
is established for the panels of cover plates subjected to thermal
stresses .
</TEXT>
</DOC>
