| 000 | 00665 a2200265 4500 | ||
|---|---|---|---|
| 001 | 15521 | ||
| 020 | _a0 | ||
| 041 | _aeng | ||
| 080 | _a621.454:533.6.07 Vad | ||
| 245 | _aFlow field calculation in supersonic mixed-compression aircraft inlets at angle of attack using the three-dimensional method of characteristics with discrete shock wave fitting | ||
| 250 | _a | ||
| 260 | _an.p. | ||
| 260 | _bPurdue University, | ||
| 260 | _c1977 | ||
| 300 | _axiv,243 p. | ||
| 300 | _c22 cm | ||
| 490 | _a | ||
| 100 | _aVadyak, Joseph | ||
| 700 | _a | ||
| 650 | _a | ||
| 650 | _aAerodynamics, Supersonic | ||
| 650 | _aShock waves | ||
| 942 | _cBK | ||
| 942 | _2UDC | ||
| 999 |
_c17731 _d17731 |
||