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 |