| 000 | 00651 a2200241 4500 | ||
|---|---|---|---|
| 001 | 311657 | ||
| 020 | _a | ||
| 041 | _aeng | ||
| 080 | _aLNASA TN D 8205 : 1976 | ||
| 245 | _aEffect of angleplying and matrix enhancement on impact-resistant boron / aluminum composites | ||
| 250 | _a | ||
| 260 | _aWashington, D.C. | ||
| 260 | _bNational Aeronautics and Space Administration (NASA) | ||
| 260 | _c1976 | ||
| 300 | _a30 p. | ||
| 300 | _c | ||
| 856 | _uNASA | ||
| 490 | _aNASA TN D 8205 : 1976 | ||
| 700 | _a | ||
| 650 | _a | ||
| 650 | _aComposite materials, Metal matrix composites, Compressor blades, Aluminum, Charpy impact test | ||
| 942 | _cPP | ||
| 942 | _2UDC | ||
| 999 |
_c260149 _d260149 |
||