| 000 | 00715nam a22001937a 4500 | ||
|---|---|---|---|
| 005 | 20200218131412.0 | ||
| 008 | 200218b xxu||||| |||| 00| 0 eng d | ||
| 040 | _cIIT Kanpur | ||
| 041 | _aeng | ||
| 100 | _aChauvin, Leo T. and Buglia James J. | ||
| 245 |
_aNeasurement of aerodynamics heat transfer to a deflected trailing edge flap on a delta fin in free flight at Mach numbers from 1.5 to 2.6 [NASA Tn D-250] _cLeo T. Chauvin and James J. Buglia |
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| 260 |
_aWashington, D. C. _bNASA _cJune 1960 |
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| 300 | _a18p | ||
| 440 | _aNational Aeronautics and Space Administration (NASA) | ||
| 505 | _aTechnical note D-250 | ||
| 650 | _aAerodynamic heat transfer | ||
| 700 | _aBuglia James J. | ||
| 942 | _cREF | ||
| 999 |
_c561379 _d561379 |
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