| 000 | 00578 a2200241 4500 | ||
|---|---|---|---|
| 001 | 265470 | ||
| 020 | _a | ||
| 041 | _aeng | ||
| 080 | _aLNASA TM 4032 : 1988 | ||
| 245 | _aModifications to the Langley 8-foot transonic pressure tunnel for the laminar flow control experiment | ||
| 250 | _a | ||
| 260 | _aWashington, D.C. | ||
| 260 | _bNational Aeronautics and Space Admin | ||
| 260 | _c1988 | ||
| 300 | _a121 p. | ||
| 300 | _c | ||
| 856 | _u | ||
| 490 | _aNASA TM 4032 : 1988 | ||
| 700 | _a | ||
| 650 | _a | ||
| 650 | _aLaminar flow control, Wind tunnels | ||
| 942 | _cPP | ||
| 942 | _2UDC | ||
| 999 |
_c218257 _d218257 |
||