Volume 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.
Edited by:
William R. Hawthorne,
Walter T. Olson
Imprint: Princeton University Press
Country of Publication: United States
Volume: 2038
Dimensions:
Height: 235mm,
Width: 152mm,
Spine: 30mm
Weight: 794g
ISBN: 9780691626154
ISBN 10: 0691626154
Series: Princeton Legacy Library
Pages: 582
Publication Date: 15 February 2016
Audience:
College/higher education
,
Professional and scholarly
,
Primary
,
Undergraduate
Format: Paperback
Publisher's Status: Active
*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. 553
