000 | 03024mc a2200433a 44500 | ||
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001 | NM003146 | ||
003 | AR-HaUTN | ||
005 | 20240912182212.0 | ||
007 | ta | ||
008 | 22120sc.20 ||||||||||||||000 | seng|d | ||
020 | _a1563475383 | ||
040 |
_aAR-HaUTN _cAR-HaUTN |
||
080 | _a629.73.03=111 MAT | ||
100 |
_aMattingly, Jack D. _93029 |
||
245 |
_aAircraft engine design / _cJack D. Mattingly , William H. Heiser, David T. Pratt |
||
250 | _a2nd ed. | ||
260 |
_aReston _bAmerican Institute of Aeronautics and Astronautics _cc. 2002 |
||
300 |
_axxvii, 687 p. _bgráficos, tablas |
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490 | _aAIAA Education Series | ||
500 | _aApéndices, índice alfabético y títulos de la Serie, al final del libro. | ||
505 | _u<a href="https://biblio-intra.frh.utn.edu.ar/opac-tmpl/bootstrap/indices/3146.pdf" target="_blank">Indice Alfabético </a> | ||
505 | _tThe design process : Introduction. Designing Is Different. The Need. Our Approach. The Wheel Exists. Charting the course. Units. The atmosphere. Compressible flow relationships. Looking ahead. Example request for proposal. Mission terminology. References | ||
505 | _tConstraint analysis : Concept. Design tools. Preliminary estimates for constraint analysis Example constraint analysis. References | ||
505 | _tMission analysis : Concept. Design tolos. Aircraft weight and fuel consumtion data .Example misión analysis. References | ||
505 | _tEngine selection : parametric cycle analysis : Concept. Design tolos. Finding promising solutions. Example engine selection: Parametric cycle analysis. References | ||
505 | _tEngine selection : performance cycle analysis : Concept. . Design tolos. Component behavior. Example engine selection: performance cycle analysis. Reference | ||
505 | _tSizing the engine : installed performance : Concept. Design tolos. AEDsys software implementation of installation losses. example tnstalled performance and final engine sizing. AAF Engine performance. Reference | ||
505 | _tEngine component design : global and interface quantities : Concept. Design tolos. Engine systems design. Example engine global and interface quantities. Reference. | ||
505 | _tEngine component design : rotating turbomachinery : Concept. Design tolos. Example AAF engine component desidn: rotating. Turbomachinery. References | ||
505 | _tEngine component design : combustion systems : Concept. Design tools--Main burner. Design tools--Afterburners. Example engine component design: combustión systems. References | ||
505 | _tEngine component design : inlets and exhaust nozzles : Concept. Inlets. exhaust nozzles. Example engine component design: inlet and exhaust nozzle. Reference | ||
650 | 2 | 7 |
_aAVIONES _2Tesauro SPINES _94038 |
650 | 1 | 7 |
_aMOTORES DE AVIACIÓN _2Tesauro SPINES _94608 |
650 | 2 | 7 |
_aTECNOLOGÍA AERONAÚTICA _2Tesauro SPINES _94323 |
700 |
_aHeiser, William H. _93030 |
||
700 |
_aPratt, David T. _93031 |
||
800 |
_aPrzemieniecki, John. S. _93032 |
||
942 |
_cBK _2udc |
||
999 |
_c3146 _d3146 |