| 000 | 00717 a2200241 4500 | ||
|---|---|---|---|
| 001 | 275355 | ||
| 020 | _a | ||
| 041 | _aeng | ||
| 080 | _aLNASA CR 4019 : 1986 | ||
| 245 | _aSimulated flight acoustic investigation of treated ejector effectiveness on advanced mechanical suppressors for high velocity jet noise reduction | ||
| 250 | _a | ||
| 260 | _aWashington, D.C. | ||
| 260 | _bNational Aeronautics and Space Adminstration | ||
| 260 | _c1986 | ||
| 300 | _a413 p. | ||
| 300 | _c | ||
| 856 | _u | ||
| 490 | _aNASA CR 4019 : 1986 | ||
| 700 | _a | ||
| 650 | _a | ||
| 650 | _aSupersonic jet noise reduction, Mechanically suppressed ejector, Shock cell noise, Variable cycle engine, Treated ejector | ||
| 942 | _cPP | ||
| 942 | _2UDC | ||
| 999 |
_c232748 _d232748 |
||