Elements of Propulsion: Gas Turbines and Rockets (Aiaa by J. Mattingly, H. von Ohain

By J. Mattingly, H. von Ohain

This article offers a whole advent to gasoline turbine and rocket propulsion for aerospace and mechanical engineers. construction at the very winning Elements of gasoline Turbine Propulsion, textbook insurance has been improved to incorporate rocket propulsion and the cloth on gasoline dynamics has been dramatically more advantageous. The textual content is split into 4 elements: easy suggestions and gasoline dynamics; research of rocket propulsion structures; parametric (design element) and function (off-design) research of air respiring propulsion platforms; and research and layout of significant fuel turbine engine parts (fans, compressors, generators, inlets, nozzles, major burners, and afterburners).

Design recommendations are brought early (aircraft and rocket functionality in an introductory bankruptcy) and built-in all through. Written with wide scholar enter at the layout of the booklet, the e-book builds upon definitions and progressively develops the thermodynamics, gasoline dynamics, rocket engine research, and gasoline turbine engine rules. The booklet includes over a hundred labored examples and diverse homework difficulties so ideas are utilized when they are brought. Over six hundred illustrations and images express simple techniques, developments, and layout examples.

Eight computing device courses accompany the textual content, which enable for speedy calculation of developments, “what if” questions, conceptual layout, homework difficulties, and homework verification. The software program runs within the home windows working procedure on PC-compatible structures.

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Extra info for Elements of Propulsion: Gas Turbines and Rockets (Aiaa Education Series)

Example text

437 447 464 486 C h a p t e r 9. 6 Turbomachinery 537 Introduction . . . . . . . . . . . . . . . . . . Euler's Turbomachinery Equations . . . . . . . . . . . Axial-Flow Compressor Analysis . . . . . . . . . . . Centrifugal-Flow Compressor Analysis . . . . . . . . . Axial-Flow Turbine Analysis . . . . . . . . . . . . . Centrifugal-Flow Turbine Analysis . . . . . . . . . . . Problems . . . .

A s s u m p t i o n s o f Ideal Cycle Analysis . . . . . . . . . . Ideal R a m j e t . . . . . . . . . . . . . . . . . . Ideal Turbojet . . . . . . . . . . . . . . . . . . Ideal Turbojet with Afterburner . . . . . . . . . . . . Ideal Turbofan . . . . . . . . . . . . . . . . . Ideal Turbofan with O p t i m u m B y p a s s Ratio . . . . . . . . Ideal Turbofan with O p t i m u m Fan Pressure Ratio . . . . . . Ideal Pulse Detonation E n g i n e .

Chapter 1. 6 Chapter 2. 11 Introduction . . . . . . . . . . . . . . . . ix xv li Iv lvii 1 Propulsion . . . . . . . . . . . . . . . . . . . Units and Dimensions .............................. Operational E n v e l o p e s a n d Standard A t m o s p h e r e . . . . . . . Airbreathing E n g i n e s . . . . . . . . . . . . . . . . Aircraft Performance . . . . . . . . . . . . . . . . Rocket Engines ..................................

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