000
00268pam a2200109a 44500
082
_a
NASA
_b
CR-1738 -
100
_a
S A Powers
245
1
_a
Flow fields over sharp edged delta wings with attached shock
260
_a
_b
_c
700
_a
E R Beeman
997
_a
TR8657 C
999
_c
406122
_d
406122