| 000 | 00838cam a22002411 4500 | ||
|---|---|---|---|
| 001 | 2176006 | ||
| 005 | 20130515014121.0 | ||
| 008 | 710301s1968 nyua 000 0 eng | ||
| 010 | _a 68022781 | ||
| 040 |
_aDLC _cDLC _dkpuc |
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| 050 | 0 | 0 |
_aTL671.6 _b.T45 |
| 082 | 0 | 0 | _a629.134/1 |
| 100 | 1 |
_aTeichmann, Frederick K. _q(Frederick Kurt), _d1905- _910403 |
|
| 245 | 1 | 0 |
_aFundamentals of aircraft structural analysis _c[by] Frederick K. Teichmann. |
| 260 |
_aNew York, _bHayden Book Co. _c[1968] |
||
| 300 |
_av, 132 p. _billus. _c24 cm. |
||
| 490 | 0 | _aHayden series in aeronautical technology | |
| 650 | 0 |
_aAirplanes _xDesign and construction. _910404 |
|
| 650 | 0 |
_aStrains and stresses. _91096 |
|
| 740 | _aAircraft structural analysis. | ||
| 906 |
_a7 _bcbc _corignew _du _eocip _f19 _gy-gencatlg |
||
| 942 |
_2lcc _cBK _hTL671.6 |
||
| 999 |
_c13796 _d13796 |
||