| 000 | 01449nam a22004817a 4500 | ||
|---|---|---|---|
| 001 | NM000560 | ||
| 003 | AR-HaUTN | ||
| 007 | ta | ||
| 008 | 58020s[196 ||||||||||||||000 | spa|| | ||
| 005 | 20240930172040.0 | ||
| 020 | _a048661980x | ||
| 040 | _aAR-HaUTN | ||
| 100 |
_aMilneThomson, L. M. _95818 |
||
| 245 |
_aTheoretical aerodynamics _cL. M. MilneThomson |
||
| 250 | _a4th. ed. | ||
| 260 |
_aNew York _bDover |
||
| 300 |
_axviii, 420 p. _bgráficos |
||
| 500 | _aSímbolos, referencias bibliográficas y alfabeto griego, en páginas preliminares | ||
| 500 | _aEjemplos, al final de cada capítulo | ||
| 500 | _aIndice alfabético, al final del libro | ||
| 505 | _tPreliminary notions | ||
| 505 | _tBernoulli's theorem | ||
| 505 | _tTwodimensional motion | ||
| 505 | _tRectilinear vortices | ||
| 505 | _tThe circular cylinder as an aerofoil | ||
| 505 | _tJoukowski's transformation | ||
| 505 | _tTheory of twodimensional aerofoils | ||
| 505 | _tThin aerofoils | ||
| 505 | _tInduced velocity | ||
| 505 | _tAerofoil of finite aspecto ratio | ||
| 505 | _tThe lifting line theory | ||
| 505 | _tLifting surface theory | ||
| 505 | _tPropellers | ||
| 505 | _tWind tunnel corrections | ||
| 505 | _tSubsonic flow | ||
| 505 | _tSupersonic flow | ||
| 505 | _tSupersonic sweptback and delta wings | ||
| 505 | _tSimple flight problems | ||
| 505 | _tMoments | ||
| 505 | _tStability | ||
| 505 | _tVectors | ||
| 942 | _cBK | ||
| 999 |
_c560 _d560 |
||