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OverviewVolume XI of the High Speed Aerodynamics and Jet Propulsion series. Edited by W.R. Hawthorne and W.T. Olson. This is a comprehensive presentation of basic problems involved in the design of aircraft gas turbines, including sections covering requirements and processes, experimental techniques, fuel injection, flame stabilization, mixing processes, fuels, combustion chamber development, materials for gas turbine applications, turbine blade vibration, and performance. Originally published in 1960. 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. Full Product DetailsAuthor: William R. Hawthorne , Walter T. OlsonPublisher: Princeton University Press Imprint: Princeton University Press Volume: 2038 Dimensions: Width: 15.20cm , Height: 3.00cm , Length: 23.50cm Weight: 0.794kg ISBN: 9780691626154ISBN 10: 0691626154 Pages: 582 Publication Date: 08 December 2015 Audience: College/higher education , Professional and scholarly , Tertiary & Higher Education , Professional & Vocational Format: Paperback Publisher's Status: Active Availability: Manufactured on demand ![]() We will order this item for you from a manufactured on demand supplier. Language: English Table of Contents*Frontmatter, pg. i*Foreword, pg. v*Preface, pg. vii*Preface to Volume XI, pg. viii*Contents, pg. ix*Section A. General Considerations, pg. 3*Part Two. Combustion Chamber Design, pg. 7*Section B. Requirements and Processes, pg. 9*Section C. Experimental Techniques, pg. 44*Section D. Fuel Injection, pg. 92*Section E. Flame Stabilization, pg. 119*Section F. Mixing Processes, pg. 166*Section G. Fuels for Aircraft Gas Turbine Engines, pg. 245*Section H. Combustion Chamber Development, pg. 289*Section I. Mechanics of Materials for Gas Turbine Applications, pg. 353*Section J. Flutter Problems in Gas Turbines, pg. 425*Section K. Performance, pg. 463*Index, pg. 553ReviewsAuthor InformationTab Content 6Author Website:Countries AvailableAll regions |