| 000 | 00673pam a2200193a 44500 | ||
|---|---|---|---|
| 005 | 20200623122906.0 | ||
| 008 | 200623b xxu||||| |||| 00| 0 eng d | ||
| 040 | _cIIT Kanpur | ||
| 041 | _aeng | ||
| 100 | _aBennett, Floyd V. | ||
| 245 | 1 |
_aComparison of experimental and theoretical static aeroelastic loads and deflections of a thin 45 deg delta wing in supersonic flow [NASA TN D-974] _cFloyd V. Bennett |
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| 260 |
_bNasa, Washington, D.C. _c1961 |
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| 300 | _a41p | ||
| 440 | _aNational Aeronautics and Spce Administratio (NASA) | ||
| 500 | _aBound With Nasa Tn D-971-973,975-980 | ||
| 505 | _aTechnical Note D-974 | ||
| 650 | _aAeroelastic | ||
| 942 | _cREF | ||
| 999 |
_c399182 _d399182 |
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