| 000 | 00845pam 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-3029]: Semiempirical method for predicting effects of incident-reflecting shocks on the turbulent boundary layer _cS. Z. Pinckney |
|
| 260 |
_bNASA _c1965 _aWashington |
||
| 300 | _a99p | ||
| 440 | _aNational Aeronautics and Space Administration | ||
| 440 | _aNASA Technical Note | ||
| 500 | _aBound together NASA TN D-3021 to 3030 | ||
| 500 | _aBound vol. Acc. No. 64302 contains Acc. No. TR10442 to TR10450 | ||
| 650 | _aAircraft | ||
| 650 | _aHypersonic airbreathing propulsion systems | ||
| 650 | _aTurbulent boundary layer | ||
| 700 | _aPinckney, S. Z. | ||
| 942 | _cBK | ||
| 999 |
_c395357 _d395357 |
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