000 00665 a2200265 4500
001 276408
020 _a
041 _aeng
080 _a043:629.136.2:533.6.01Abh
245 _aMeasurement of aerodynamic forces on hypersonic models in an impulse facility using an accelerometer balance (R)
250 _a
260 _aMumbai
260 _bIIT
260 _c2009
300 _a40 p.
300 _c30 cm
490 _a
100 _aAbhinav Kumar, K.S.N.
700 _aMenezes, V.
650 _aMenezes, V.
650 _aTheses and Dissertations
650 _aAerodynamic load , Hypersonic , Accelerometers , Shock tunnel
942 _cTD
942 _2UDC
999 _c205751
_d205751