| 000 | 00613 a2200277 4500 | ||
|---|---|---|---|
| 001 | 55600 | ||
| 020 | _a0 | ||
| 041 | _aeng | ||
| 080 | _a533.693 Gad | ||
| 245 | _aDevelopment of a device for controlling the leading edge vortices on a delta wing | ||
| 250 | _a | ||
| 260 | _a | ||
| 260 | _bKent : Flow Research, 1986 | ||
| 260 | _c1986 | ||
| 300 | _a82 p. | ||
| 300 | _c27 cm | ||
| 490 | _a | ||
| 100 | _aGad-el-Hak, Mohamed | ||
| 700 | _a | ||
| 650 | _a | ||
| 650 | _aVortex-motion | ||
| 650 | _aAirplanes-Wings, Triangular | ||
| 650 | _aLeading edges (Aerodynamics) | ||
| 942 | _cBK | ||
| 942 | _2UDC | ||
| 999 |
_c104420 _d104420 |
||