<DOC>
<DOCNO>
598
</DOCNO>
<TITLE>
new test techniques for a hypervelocity wind tunnel .
</TITLE>
<AUTHOR>
stalmach, c.j. and cooksey, j.m.
</AUTHOR>
<BIBLIO>
aerospace engineering. vol. 21. march 1962 .
</BIBLIO>
<TEXT>
the measurement of rocket exhaust effects on vehicle stability and the
measurement of aerodynamic damping were made in an arc-discharge type of
 hypervelocity wind tunnel . sample data are given to indicate the
quality of data obtainable in this tunnel, and samples of self-luminous
and shadowgraph photographs are also presented .
</TEXT>
</DOC>
