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Fourth Edition A. M. Y. Razak Professor of Turbomachinery Institute of Aerospace Propulsion University of Manchester McGraw-Hill Education New York • Chicago • San Francisco • Athens • London • Madrid • Mexico City Milan • New Delhi • Singapore • Sydney • Toronto Copyright © 2026 by McGraw-Hill Education All rights reserved. No part of this publication may be reproduced or distributed in any form or by any means, or stored in a database or retrieval system, without the prior written consent of McGraw-Hill Education, including, but not limited to, network or other electronic storage or transmission, or broadcast for distance learning.
6.1 Fan Types – Propeller, Tube-Axial, Vane-Axial 6.2 Fan Laws and System Curves 6.3 Noise Generation and Control Part 3: Turbines Chapter 7: Axial Flow Turbines 7.1 Impulse vs. Reaction Stages 7.2 Velocity Triangles for Power Extraction 7.3 Blade Cooling – Film, Transpiration, and Impingement 7.4 Loss Correlations – Soderberg, Ainley & Mathieson, Kacker-Okapuu Turbines Compressors And Fans Fourth Edition
Stage pressure ratio ( \pi_s = 1.3 ), number of stages ( n = \frac\ln 15\ln 1.3 = \frac2.7080.262 \approx 10.3 ), so 10 stages (final ratio slightly adjusted).
5.1 Impeller and Diffuser Flow 5.2 Slip Factor and Incidence 5.3 Vaneless and Vaned Diffusers 5.4 Performance Maps and Choke Printed in the United States of America Fourth Edition A
12.1 Additively Manufactured Blades 12.2 Supercritical COâ‚‚ Turbomachinery 12.3 Hydrogen Fuel Effects
: A compressor stage has ( U = 250\ \textm/s ), axial velocity ( C_x = 180\ \textm/s ), inlet absolute flow angle ( \alpha_1 = 15^\circ ), outlet absolute angle ( \alpha_2 = 45^\circ ). Find specific work. Reaction Stages 7
10.1 Campbell Diagram 10.2 Critical Speeds and Damping 10.3 High-Cycle Fatigue