| 000 | 00690 a2200289 4500 | ||
|---|---|---|---|
| 001 | 36662 | ||
| 020 | _a0 | ||
| 041 | _aeng | ||
| 080 | _a533.692 Raj | ||
| 245 | _aAnalysis of wings with leading edge and/or trailing edge segmented (spanwise) flaps using planar horse shoe vortex-lattic method | ||
| 250 | _a | ||
| 260 | _aBangalore | ||
| 260 | _bNational Aeronautical Lab., | ||
| 260 | _c1985 | ||
| 300 | _avarious p. | ||
| 300 | _c27.5 cm | ||
| 490 | _a | ||
| 100 | _aRajeshwari, B. | ||
| 700 | _aDutt, H.N.V | ||
| 700 | _a | ||
| 650 | _a | ||
| 650 | _aLeading edges (Aerodynamics) | ||
| 650 | _aVortex-motion | ||
| 650 | _aAirplanes-Wings | ||
| 942 | _cBK | ||
| 942 | _2UDC | ||
| 999 |
_c116754 _d116754 |
||