| 000 | 01513nam a22004097a 4500 | ||
|---|---|---|---|
| 001 | NM002659 | ||
| 003 | AR-HaUTN | ||
| 007 | ta | ||
| 008 | 61120sc. 1 ||||||||||||||000 | spa|| | ||
| 005 | 20240930172236.0 | ||
| 020 | _a007054466 | ||
| 040 | _aAR-HaUTN | ||
| 100 |
_aKatz, Joseph _97430 |
||
| 245 |
_aLowspeed aerodynamics _bfrom wing theory to panel methods _cJoseph Katz , Allen Plotkin |
||
| 250 | _a[1st] ed. | ||
| 260 |
_aNew York _bMcGrawHill |
||
| 300 |
_axv, 632 _bgráficos |
||
| 500 | _aApéndices e índice alfabético, al final del libro | ||
| 505 | _tIntroduction and background | ||
| 505 | _tFundamentals of inviscid, incompressible flow | ||
| 505 | _tGeneral solutions of the incompressible, potential flow equations | ||
| 505 | _tSmall disturbance flow over threedimensional wings : formulation of the problem | ||
| 505 | _tSmall disturbance flow over twodimensional airfoils | ||
| 505 | _tExact solutions with complex variables | ||
| 505 | _tPerturbation methods | ||
| 505 | _tThreedimensional smalldisturbance solutions | ||
| 505 | _tNumerical (panel) methods | ||
| 505 | _tSingularity elements and influence coefficients | ||
| 505 | _tTwodimensional numerical solutions | ||
| 505 | _tThreedimensional numerical solutions | ||
| 505 | _tUnsteady incompressible potential flow | ||
| 505 | _tEnhancement of the potential flow model | ||
| 653 | _aINGENIERIA AERONAUTICA | ||
| 653 | _aPROYECTO Y DISENO AERODINAMICO | ||
| 700 |
_aPlotkin, Allen _97431 |
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| 942 | _cBK | ||
| 999 |
_c2659 _d2659 |
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