| 000 | 00658 a2200241 4500 | ||
|---|---|---|---|
| 001 | 279333 | ||
| 020 | _a | ||
| 041 | _aeng | ||
| 080 | _aLNASA CR 3567 : 1983 | ||
| 245 | _aAnalysis of unswept and swept wing chordwise pressure data from an oscillating naca 0012 airfoil experiment : vol. - I : technical report | ||
| 250 | _a | ||
| 260 | _aWashington, D.C. | ||
| 260 | _bNASA | ||
| 260 | _c1983 | ||
| 300 | _a104 p. | ||
| 300 | _c | ||
| 856 | _u | ||
| 490 | _aNASA CR 3567 : 1983 | ||
| 700 | _a | ||
| 650 | _a | ||
| 650 | _aAerodynamic testing, Airfoil aerodynamics, Dynamic stall, Oscillating NACA 0012 airfoil, Pitching oscillations | ||
| 942 | _cPP | ||
| 942 | _2UDC | ||
| 999 |
_c238224 _d238224 |
||