000 | 01543nam a22004217a 4500 | ||
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001 | NM002660 | ||
003 | AR-HaUTN | ||
007 | ta | ||
008 | 61120s2001 ||||||||||||||000 | spa|| | ||
005 | 20240930172236.0 | ||
020 | _a9780521662192 | ||
040 | _aAR-HaUTN | ||
100 |
_aKatz, Joseph _97432 |
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245 |
_aLowspeed aerodynamics _cJoseph Katz , Allen Plotkin |
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250 | _a2nd ed. | ||
260 |
_aCambridge _bCambridge University Press |
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300 |
_axvi, 613 p. _bgráficos |
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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 | _tSmalldisturbance 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 | _tThe laminar boundary layer | ||
505 | _tEnhancement of the potential flow model | ||
653 | _aINGENIERIA AERONAUTICA | ||
653 | _aPROYECTO Y DISENO AERODINAMICO | ||
700 |
_aPlotkin, Allen _97433 |
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942 | _cBK | ||
999 |
_c2660 _d2660 |