| 000 | 00661 a2200241 4500 | ||
|---|---|---|---|
| 001 | 265474 | ||
| 020 | _a | ||
| 041 | _aeng | ||
| 080 | _aLNASA TP 2588 : 1987 | ||
| 245 | _aComparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds | ||
| 250 | _a | ||
| 260 | _aWashington, D.C. | ||
| 260 | _bNational Aeronautics and Space Admin | ||
| 260 | _c1987 | ||
| 300 | _a124 p. | ||
| 300 | _c | ||
| 856 | _u | ||
| 490 | _aNASA TP 2588 : 1987 | ||
| 700 | _a | ||
| 650 | _a | ||
| 650 | _aNozzle-afterbody flow interactions, Reynolds number effects, Wind tunnel and flight comparison | ||
| 942 | _cPP | ||
| 942 | _2UDC | ||
| 999 |
_c218270 _d218269 |
||