<DOC>
<DOCNO>
430
</DOCNO>
<TITLE>
calibration of the flow in the mach 4 working section
of the 4ft . x 3ft . high supersonic speed wind tunnel
at rae bedford .
</TITLE>
<AUTHOR>
andrews,d.r. and brown,c.s.
</AUTHOR>
<BIBLIO>
rae tn.aero.2820, 1962.
</BIBLIO>
<TEXT>
  mach number and flow angle distributions in the working section of
the mach 4 nozzle of the 4 ft x 3 ft high-supersonic-speed wind tunnel
are presented for a range of total pressure and humidity .
</TEXT>
</DOC>
