| 000 | 00904cam a2200265 4500 | ||
|---|---|---|---|
| 001 | sa 68019765 | ||
| 003 | DLC | ||
| 005 | 20260227112719.0 | ||
| 008 | 720710s1969 ii b 00010 eng | ||
| 010 | _asa 68019765 //r82 | ||
| 025 | _aPL480:I-F-E-275 | ||
| 050 | 0 |
_aTL504 _b.B35 TN-20 _aTL574.P7 |
|
| 082 |
_a629.13/008 s _a629.134/32 |
||
| 100 | 1 | 0 | _aRamamoorthy, P. |
| 245 | 1 | 0 |
_aSpline approximation as applied to aeronautical problems, _cby P. Ramamoorthy & C. L. Narayana. |
| 260 | 0 |
_aBangalore, _bNational Aeronautical Laboratory, _c1969. |
|
| 300 |
_ai, 5 p. _c29 cm. |
||
| 490 | 1 | _aNAL Technical note, TN-20 | |
| 504 | _aBibliography: p. 5. | ||
| 650 | 0 |
_aAirplanes _xWings _xTesting. |
|
| 650 | 0 | _aSpline theory. | |
| 650 | 0 | _aPressure. | |
| 700 | 1 | 0 |
_aNarayana, C. L., _ejoint author. |
| 810 | 1 |
_aBangalore, India (City). _bNational Aeronautical Laboratory. _tNAL Technical note, _vTN-20. |
|
| 999 |
_c89060 _d89060 |
||