| Record ID | marc_university_of_toronto/uoft.marc:3708391099:962 |
| Source | University of Toronto |
| Download Link | /show-records/marc_university_of_toronto/uoft.marc:3708391099:962?format=raw |
LEADER: 00962nam 22002172 4500
008 000000s1991 ||| | |1|| ||||| d
088 $aAIAA-91-1707
088 $aA91-42560
090 $a54367$bAERO
100 1 $aMinucci, Marco A. S.
245 13 $aAn investigation of hypersonic shock tunnel testing at an equilibrium interface condition of 4,100K: theory and experiment /$cMarco A. S. Minucci and Henry T. Nagamatsu.
260 $aWashington, D. C :$bAmerican Institute of Aeronautics and Astronautics,$c1991.
300 $a17 p. :$bill.
504 $aIncludes bibliographical references: p. 11-12.
580 $aSource: AIAA 22nd Fluid Dynamics, Plasma Dynamics & Lasers Conference, June 24-26, 1991/Honolulu, Hawaii
650 7 $aHypersonic flow$2nasat
650 7 $aHypersonic shock tubes$2nasat
700 1 $aNagamatsu, Henry T.
710 20 $aAIAA
948 $a01/09/2001$b01/09/2001
949 $a54367$wLC$c1$i34444022827000$lSTACKS$mAEROSPACE$rY$sY$tBOOK$u28/1/2001