000 00410pam a2200145a 44500
082 _aNAS
_bTN D-7520 -
100 _aAlbers,James A
245 1 _aBOUNDARY-LAYER ANALYSIS OF SUBSONIC INLET DIFFUSER GEOMETRIES FOR ENGINE NACELLES
260 _a
_bNasa, Washington, D.C.
_c1974
300 _a29
500 _aBound With Nasa Tn D-7512-20
700 _aFelderman,John
964 _gCIRC
997 _aTR8699 C
999 _c394662
_d394662