Download e-book for iPad: Elements of Propulsion: Gas Turbines and Rockets (Aiaa by J. Mattingly, H. von Ohain

By J. Mattingly, H. von Ohain

ISBN-10: 1563477793

ISBN-13: 9781563477799

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

Design ideas are brought early (aircraft and rocket functionality in an introductory bankruptcy) and built-in all through. Written with huge scholar enter at the layout of the e-book, the e-book builds upon definitions and progressively develops the thermodynamics, gasoline dynamics, rocket engine research, and fuel turbine engine rules. The ebook comprises over a hundred labored examples and various homework difficulties so suggestions are utilized when they are brought. Over six hundred illustrations and photographs convey simple suggestions, developments, and layout examples.

Eight desktop courses accompany the textual content, which permit for quick calculation of traits, “what if” questions, conceptual layout, homework difficulties, and homework verification. The software program runs within the home windows working process on PC-compatible platforms.

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

Example text

Variation in G a s Properties . . . . . . . . . . . . . C o m p o n e n t Performance . . . . . . . . . . . . . . Inlet a n d Diffuser Pressure Recovery . . . . . . . . . . C o m p r e s s o r and Turbine Efficiencies . . . . . . . . . . B u r n e r Efficiency a n d Pressure L o s s . . . . . . . . . . E x h a u s t Nozzle L o s s . . . . . . . . . . . . . . . M e c h a n i c a l Efficiency o f Power Shaft .

As previously stated, the new turbojets employing a dual-rotor configuration or controlled variable-stator blades were capable of substantially higher pressure ratios than the fixed-geometry, single-spool engines of the 1940s. Engine cycle analysis showed that the high power-per-unit mass flow rate needed for the advanced engines required higher turbine inlet temperatures. This requirement led to continuous major research efforts to achieve high-efficiency combustion with low pollution, to increase the effectiveness of turbine blade-cooling methods, and to improve the temperature capabilities of materials.

Preface . . . . . . . . . . . . . . . . . . . . . . . . Acknowledgments . . . . . . . . . . . . . . . . . . . . Nomenclature . . . . . . . . . . . . . . . . . . . . . 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 .

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

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