| 000 | 00433pam a2200145a 44500 | ||
|---|---|---|---|
| 082 |
_aNASA _bCR-2124 - |
||
| 100 | _aMiner,E W | ||
| 245 | 1 | _aA FINITE-DIFFERENCE METHOD FOR PREDICTING SUPERSONIC TURBULENT BOUNDARY-LAYER FLOW WITH TANGENTIAL SLOT INJECTION | |
| 260 |
_a _bNasa, Washington, D.C. _c1972 |
||
| 300 | _aXII,68 | ||
| 500 | _aBound With Nasa Cr-2121-29 | ||
| 700 | _aLewis,C H | ||
| 964 | _gCIRC | ||
| 997 | _aTR7975 C | ||
| 999 |
_c393367 _d393367 |
||