By J. Mattingly, H. von Ohain

This article offers an entire creation to gasoline turbine and rocket propulsion for aerospace and mechanical engineers. development at the very winning Elements of fuel Turbine Propulsion, textbook insurance has been extended to incorporate rocket propulsion and the cloth on fuel dynamics has been dramatically better. The textual content is split into 4 elements: simple options and fuel dynamics; research of rocket propulsion platforms; parametric (design element) and function (off-design) research of air respiring propulsion structures; and research and layout of significant fuel turbine engine elements (fans, compressors, generators, inlets, nozzles, major burners, and afterburners).

Design innovations 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 e-book, the e-book builds upon definitions and steadily develops the thermodynamics, gasoline dynamics, rocket engine research, and gasoline turbine engine ideas. The publication comprises over a hundred labored examples and various homework difficulties so ideas are utilized once they are brought. Over six hundred illustrations and photographs convey simple options, traits, and layout examples.

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

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

Example text

381 381 399 404 427 C h a p t e r 8. 5 E n g i n e Performance A n a l y s i s 437 .................. 381 Introduction . . . . . . . . . . . . . . . . . . Gas Generator . . . . . . . . . . . . . . . . . Turbojet Engine . . . . . . . . . . . . . . . . . Turbojet Engine with Afterbuming . . . . . . . . . . . Turbofan Engine---Separate Exhausts and Convergent Nozzles . . . . . . . . . . . . . . . Problems . .

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 ..................................

Ideal Turbofan with O p t i m u m Fan Pressure Ratio . . . . . . Ideal Pulse Detonation E n g i n e . . . . . . . . . . . . Problems ...................................... 261 262 264 264 266 266 278 291 302 325 332 341 344 Component Performance 355 ..................... Introduction . . . . . . . . . . . . . . . . . . Variation in G a s Properties . . . . . . . . . . . . . C o m p o n e n t Performance . . . . . . . .

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