000 00416pam a2200133a 44500
082 _aNASA
_bTND-6031 -
100 _aBarnwell,Richard W.
245 1 _aA TIME DEPENDENT METHOD FOR CALCULATING SUPERSONIC BLUNT-BODY FLOW FIELDS WITH SHARP CORNERS AND EMBEDDED SHOCK WAVES
260 _a
_bNasa, Washington, D.C.
_c1970
300 _a65
500 _aBound With Nasa Tnd-6030
964 _gCIRC
997 _aTR8319 C
999 _c394688
_d394688