| 000 | 00636 a2200241 4500 | ||
|---|---|---|---|
| 001 | 315339 | ||
| 020 | _a | ||
| 041 | _aeng | ||
| 080 | _aLNASA CR 3099 : 1979 | ||
| 245 | _aRotary balance data for a single-engine trainer design for an angle-of-attack range of 8 degree to 90 degree | ||
| 250 | _a | ||
| 260 | _aWashington, D.C. | ||
| 260 | _bNational Aeronautics and Space Administration | ||
| 260 | _c1980 | ||
| 300 | _a324 p. | ||
| 300 | _c | ||
| 856 | _u | ||
| 490 | _aNASA CR 3099 : 1979 | ||
| 700 | _a | ||
| 650 | _a | ||
| 650 | _aGeneral aviation, Spinning, Rotary balance, High angle-of-attack wind tunnel | ||
| 942 | _cPP | ||
| 942 | _2UDC | ||
| 999 |
_c263009 _d263009 |
||