| 000 | 00690 a2200241 4500 | ||
|---|---|---|---|
| 001 | 284790 | ||
| 020 | _a | ||
| 041 | _aeng | ||
| 080 | _aLNASA CR 3069 : 1978 | ||
| 245 | _aFeasibility of combining linear theory and impact theory methods for the analysis and design of high speed configurations | ||
| 250 | _a | ||
| 260 | _aWashington, D.C. | ||
| 260 | _bNational Aeronautics & Space Administration | ||
| 260 | _c1978 | ||
| 300 | _a39 p. | ||
| 300 | _c | ||
| 856 | _uNASA | ||
| 490 | _aNASA CR 3069 : 1978 | ||
| 700 | _a | ||
| 650 | _a | ||
| 650 | _aAerodynamic characteristics, Aerodynamic predictions, Delta wings, Pressure distributions, High speed configurations | ||
| 942 | _cPP | ||
| 942 | _2UDC | ||
| 999 |
_c244105 _d244105 |
||