| 000 | 00631 a2200241 4500 | ||
|---|---|---|---|
| 001 | 311283 | ||
| 020 | _a | ||
| 041 | _aeng | ||
| 080 | _aLNASA CR 2610 : 1976 | ||
| 245 | _aTransonic pressure measurements and comparison of theory to experiment for an arrow-wing configuration : Summary report | ||
| 250 | _a | ||
| 260 | _aWashington, D.C. | ||
| 260 | _bNASA | ||
| 260 | _c1976 | ||
| 300 | _a489 p. | ||
| 300 | _c | ||
| 856 | _uNASA | ||
| 490 | _aNASA CR 2610 : 1976 | ||
| 700 | _a | ||
| 650 | _a | ||
| 650 | _aAeroelasticity, Experimental pressure distributions, Aerodynamic theory, Arrow wing configuration | ||
| 942 | _cPP | ||
| 942 | _2UDC | ||
| 999 |
_c259690 _d259690 |
||