000 00268pam a2200109a 44500
082 _aNASA
_bCR-1738 -
100 _aS A Powers
245 1 _aFlow fields over sharp edged delta wings with attached shock
260 _a
_b
_c
700 _aE R Beeman
997 _aTR8657 C
999 _c406122
_d406122