| 000 | 00870pam a2200229a 44500 | ||
|---|---|---|---|
| 003 | OSt | ||
| 040 | _cIIT Kanpur | ||
| 041 | _aeng | ||
| 110 | _aWashington. National Aeronautics and Space Administration (NASA) | ||
| 245 | 1 |
_aNASA Technical Note [NASA TN D-4679]: Calibration of 30 degree included-angle cone for determining local flow conditions in mach number range of 1.51 to 3.51 _cWalter A. Vahl and Robert L. Weirich |
|
| 260 |
_bNASA _c1968 _aWashington |
||
| 300 | _a39p | ||
| 440 | _aNational Aeronautics and Space Administration | ||
| 440 | _aNASA Technical Note | ||
| 500 | _aBound together NASA TN D-4671 to 4680 | ||
| 500 | _aBound vol. Acc. No. 86062 contains Acc. No. TR10091 to TR10099 | ||
| 650 | _aAeronautics | ||
| 650 | _aAircraft -- SST model -- flow field | ||
| 700 | _aVahl, Walter A. | ||
| 700 | _aWeirich, Robert L. | ||
| 942 | _cBK | ||
| 999 |
_c393169 _d393169 |
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