| 000 | 00698 a2200241 4500 | ||
|---|---|---|---|
| 001 | 284345 | ||
| 020 | _a | ||
| 041 | _aeng | ||
| 080 | _aLNASA TP 1176 : 1978 | ||
| 245 | _aDirect mneasurements and analysis of skin friction and cooling downstream of multiple flush-slot injection into a turbulent mach 6 boundary layer | ||
| 250 | _a | ||
| 260 | _aWashington, D.C. | ||
| 260 | _bNational Aeronautics & Space Administration | ||
| 260 | _c1978 | ||
| 300 | _a109 p. | ||
| 300 | _c | ||
| 856 | _uNASA | ||
| 490 | _aNASA TP 1176 : 1978 | ||
| 700 | _a | ||
| 650 | _a | ||
| 650 | _aSlot injection, Slot cooling, Mutiple flush slots, Skin-friction reduction, Boundary-layer profiles | ||
| 942 | _cPP | ||
| 942 | _2UDC | ||
| 999 |
_c243598 _d243598 |
||