| 000 | 00592 a2200157 4500 | ||
|---|---|---|---|
| 005 | 20221220151107.0 | ||
| 100 | _aGrafton, Sue B. | ||
| 245 | 1 |
_aNASA TN [D-6090] _bDYNAMIC STABILITY DERIVATIVES OF A TWIN-JET FIGHTER MODEL FOR ANGLES OF ATTACK FROM -10(DEGREE) TO 110(DEGREE) _cSue B. Grafton and Charles E. Libbey |
|
| 260 |
_bNasa, Washington, D.C. _c1971 |
||
| 300 | _a36 | ||
| 440 | _aNASA Technical Note | ||
| 500 | _aNASA Technical Note D-6090-99 Bounded Volumes Accession No. 101225; Contents: TR9515-22 | ||
| 650 | _aAerodynamics | ||
| 700 | _a Libbey, Charles E. | ||
| 942 | _cTR | ||
| 999 |
_c394863 _d394863 |
||