TY - MUSIC AU - Mattingly, Jack D. AU - Heiser, William H. AU - Pratt, David T. TI - Aircraft engine design / T2 - AIAA Education Series SN - 1563475383 PY - 2002/// CY - Reston PB - American Institute of Aeronautics and Astronautics KW - AVIONES KW - Tesauro SPINES KW - MOTORES DE AVIACIÓN KW - TECNOLOGÍA AERONAÚTICA N1 - Apéndices, índice alfabético y títulos de la Serie, al final del libro. ; Indice Alfabético ; The 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; Constraint analysis : Concept. Design tools. Preliminary estimates for constraint analysis Example constraint analysis. References ; Mission analysis : Concept. Design tolos. Aircraft weight and fuel consumtion data .Example misión analysis. References; Engine selection : parametric cycle analysis : Concept. Design tolos. Finding promising solutions. Example engine selection: Parametric cycle analysis. References; Engine selection : performance cycle analysis : Concept. . Design tolos. Component behavior. Example engine selection: performance cycle analysis. Reference; Sizing the engine : installed performance : Concept. Design tolos. AEDsys software implementation of installation losses. example tnstalled performance and final engine sizing. AAF Engine performance. Reference; Engine component design : global and interface quantities : Concept. Design tolos. Engine systems design. Example engine global and interface quantities. Reference; Engine component design : rotating turbomachinery : Concept. Design tolos. Example AAF engine component desidn: rotating. Turbomachinery. References; Engine component design : combustion systems : Concept. Design tools--Main burner. Design tools--Afterburners. Example engine component design: combustión systems. References; Engine component design : inlets and exhaust nozzles : Concept. Inlets. exhaust nozzles. Example engine component design: inlet and exhaust nozzle. Reference ER -