000 00604nam a2200193Ia 4500
919 _a200176
082 _a629.134 52
_bP18 (THESIS)
100 _aMedhi, Biswajit
_d
245 _aDesign and development of non-intrusive optical probes for quantitative analysis of flow fields in hypersonic shock tunnels
_cby Biswajit Medhi
260 _aBengaluru
_bIndian Institute of Science
_c2018
300 _axxiii, 142p.;
_e
500 _aDepartment of Instrumentation and Applied Physics, IISc, PhD THESIS
653 _aaerophysical research; ICMAR theoretical mechanics; applied mechanics;
700 _aVasu, R. M.
950 _cMarch 2018
999 _c199576
_d199576