| 000 | 00594 a2200241 4500 | ||
|---|---|---|---|
| 001 | 282238 | ||
| 020 | _a | ||
| 041 | _aeng | ||
| 080 | _aLNASA TP 2269 : 1983 | ||
| 245 | _aWing planform effects at supersonic speeds for an advanced fighter configuration | ||
| 250 | _a | ||
| 260 | _aWashington, D.C. | ||
| 260 | _bNational Aeronautics & Space Administration | ||
| 260 | _c1984 | ||
| 300 | _a115 p. | ||
| 300 | _c | ||
| 856 | _u | ||
| 490 | _aNASA TP 2269 : 1983 | ||
| 700 | _a | ||
| 650 | _a | ||
| 650 | _aSupersonic aerodyn, Planform study, Cranked wings, Internal flow | ||
| 942 | _cPP | ||
| 942 | _2UDC | ||
| 999 |
_c242134 _d242134 |
||