000 00397pam a2200133a 44500
082 _aNASA
_bTN D-7549 -
100 _aMiller,Max J
245 1 _aESTIMATION OF DEVIATION ANGLE FOR AXIAL-FLOW COMPRESSOR BLADE SECTIONS USING INVISCID-FLOW SOLUTIONS
260 _a
_bNasa, Washington, D.C.
_c1974
300 _a41
500 _aBound With Nasa Tn D-7541-50
964 _gCIRC
997 _aTR8390 C
999 _c394080
_d394080