| 000 | 00696 a2200241 4500 | ||
|---|---|---|---|
| 001 | 279750 | ||
| 020 | _a | ||
| 041 | _aeng | ||
| 080 | _aLNASA CR 3642 : 1983 | ||
| 245 | _aAeroelastic loads prediction for an arrow wing : Task III - evaluation of the boeing three - dimensional leading-edge vortex code | ||
| 250 | _a | ||
| 260 | _aWashington, D.C. | ||
| 260 | _bNational Aeronautics and Space Administration | ||
| 260 | _c1983 | ||
| 300 | _a218 p. | ||
| 300 | _c | ||
| 856 | _u | ||
| 490 | _aNASA CR 3642 : 1983 | ||
| 700 | _a | ||
| 650 | _a | ||
| 650 | _aAeroelasticity, Experimental pressure distributions, Aerodynamic theory, Arrow-wing configuration, Wind tunnel test | ||
| 942 | _cPP | ||
| 942 | _2UDC | ||
| 999 |
_c239064 _d239064 |
||