Aerodynamics of Turbines and Compressors. (HSA-1), Volume 1

Volume X of the __High Speed Aerodynamics and Jet Propulsion__ series. Contents include: Theory of Two-Dimensional Flow through Cascades; Three-Dimensional Flow in Turbomachines; Experimental Techniques; Flow in Cascades; The Axial Compressor Stage; The Supersonic Compressor; Aerodynamic Design of Axial Flow Turbines; The Radial Turbine; The Centrifugal Compressor; Intermittent Flow Effects. Originally published in 1964. The **Princeton Legacy Library** uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905. Foreword Preface Contents Section A. Introduction Section B. Theory of Two-Dimensional Flow Through Cascades Section C. Three-Dimensional Flow in Turbomachines Section D. Experimental Techniques Section E. Flow in Cascades Section F. The Axial Compressor Stage Section G. The Supersonic Compressor Section H. Aerodynamic Design of Axial Flow Turbines Section I. The Radial Turbine Section J. The Centrifugal Compressor Section K. Blading Interaction Effects in Turbines Index