000 00369pam a2200109a 44500
082 _aTR
_bTMX-3148
100 _aHugh A. Klassen
245 1 _aEffect of inducer inlet and diffuser throat areas on performance of a low pressure ratio sweptback centrifugal compressor
260 _a
_b
_c
650 _aUs National Aeronautics And Space Administration
997 _aTR2749 C
999 _c404802
_d404802