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Elements of Gas Turbine Propulsion w/ IBM 3.5' Disk [Hardback]

  • Formāts: Hardback, 960 pages, height x width x depth: 239x175x59 mm, weight: 1633 g, Illustrations
  • Izdošanas datums: 30-Nov-1995
  • Izdevniecība: McGraw-Hill Professional
  • ISBN-10: 0079121969
  • ISBN-13: 9780079121967
Citas grāmatas par šo tēmu:
  • Formāts: Hardback, 960 pages, height x width x depth: 239x175x59 mm, weight: 1633 g, Illustrations
  • Izdošanas datums: 30-Nov-1995
  • Izdevniecība: McGraw-Hill Professional
  • ISBN-10: 0079121969
  • ISBN-13: 9780079121967
Citas grāmatas par šo tēmu:
This text provides an introduction to the fundamentals of gas turbine engines and jet propulsion for aerospace or mechanical engineers. The book contains sufficient material for two sequential courses i propulsion (advanced fluid dynamics) an introductory course in jet propulsion and a gas turbine engine components course. The text is divided into four parts introduction to aircraft propulsion; basic concepts and one-dimensional/gas dynamics; analysis and performance of air breathing propulsion systems; and analysis and design of gas turbine engine components.
1 Introduction2 Thermodynamics Review3 Compressible Flow4 Aircraft Gas Turbine Engine5 Parametric Cycle Analysis of Ideal Engines6 Component Performance7 Parametric Cycle Analysis of Real Engines8 Engine Performance Analysis9 Turbomachinery10 Inlets, Nozzles and Combustion SystemsAppendixesA U.S. Standard Atmosphere, 1976B Gas Turbine Engine DataC Rocket Engine DataD Air and (CH2)n Properties at Low PressureE Compressible Flow FunctionsF Normal Shock FunctionsG Two-Dimensional Oblique Flow FunctionsH Rayleigh Line Flow FunctionsI Fanno Line Flow FunctionsJ Turbomachinery Stresses and MaterialsK About the Software
Jack D Mattingly received his B.S and M.S in Mechanical Engineering From the University of Notre Dame, and his Ph.D in Aeronautics and Astronautics at the University of Washington. While Studying for his doctorate under Gordon C.Oates, he pioneered research in the mixing ofconnaular swirling flows and develop a major new test facility. During his 28 years of experience in analysis and design of propulsion and thermodynamic system, he has developed aerothermodynamic cycle analysis models and created engineering software for air-breathing propulsion system. Dr. Mattingly has more than 23 years of experience in Engineering Education,Previously as a senior member of the Department of Aeronautics at the United States Air Force Academy, where he established a top undergraduate propulsion program. He retired from active duty with the U.S Air Force in 1989 and joined the faculty of Seattle University.