| 000 | 00650nam a2200181 4500 | ||
|---|---|---|---|
| 003 | OSt | ||
| 005 | 20211014100907.0 | ||
| 008 | 211014b xxu||||| |||| 00| 0 eng d | ||
| 040 | _cIIT Kanpur | ||
| 041 | _aeng | ||
| 100 | _aMatthews, Clarence W. | ||
| 245 |
_aA numerical analysis of the use of perforated walls to control shock location and moment in an internal compression supersonic inlet [NASA TR R-317] _cMatthews, Clarence W. |
||
| 260 |
_aWashington, D. C. _bNational Aeronautics and Space Administration _c1969 |
||
| 300 | _a52p | ||
| 440 | _aNational Aeronautics and Space Administration | ||
| 650 | _aSupersonic inlet | ||
| 942 | _cREF | ||
| 999 |
_c564926 _d564926 |
||