000 00725 a2200217 4500
005 20250515230912.0
264 0 _c20121002
008 201210s 0 0 eng d
022 _a1559-128X
024 7 _a10.1364/AO.30.000770
_2doi
040 _aNLM
_beng
_cNLM
100 1 _aYan, D P
245 0 0 _aNew method of asymmetric flow field measurement in hypersonic shock tunnel.
_h[electronic resource]
260 _bApplied optics
_cMar 1991
300 _a770-4 p.
_bdigital
500 _aPublication Type: Journal Article
700 1 _aHe, A Z
700 1 _aNi, X W
773 0 _tApplied optics
_gvol. 30
_gno. 7
_gp. 770-4
856 4 0 _uhttps://doi.org/10.1364/AO.30.000770
_zAvailable from publisher's website
999 _c19929714
_d19929714