Record ID | harvard_bibliographic_metadata/ab.bib.10.20150123.full.mrc:133497478:1209 |
Source | harvard_bibliographic_metadata |
Download Link | /show-records/harvard_bibliographic_metadata/ab.bib.10.20150123.full.mrc:133497478:1209?format=raw |
LEADER: 01209cam a2200289 a 4500
001 010197786-7
005 20070820195725.0
008 001024s1958 maua b 000 0 eng d
035 0 $aocm45220705
040 $aCAI$cCAI$dOCLCQ
090 $aTL571.5$b.P69 1958
100 1 $aPowers, William E.
245 12 $aA shock tube investigation of heat transfer in the wake of a hemisphere-cylinder, with application to hypersonic flight /$cWilliam E. Powers, Kenneth F. Stetson and Mac C. Adams.
260 $a[Everett, Mass.] :$bAvco Manufacturing Corp., Avco Research Laboratory,$c[1958]
300 $a36, [3] p. :$bill. ;$c28 cm.
490 1 $aResearch report (Avco Research Laboratory) ;$v30
500 $a"... sponsored by the Ballistic Missile Division, Air Research and Development Command, United States Air Force under Contract AF 04(645)-18."
500 $a"August 1958."
504 $aIncludes bibliographical references (p. [39]).
650 0 $aAerodynamics, Hypersonic.
650 0 $aHeat$xTransmission.
650 0 $aShock tubes.
700 1 $aStetson, Kenneth F.
700 1 $aAdams, Mac C.
830 0 $aResearch report (Avco-Everett Research Laboratory) ;$v30.
988 $a20061228
906 $0OCLC