عنوان

Propulsion and power :

شابک

3319759795

شابک

9783319759791

شابک اشتباه

3319759779

شابک اشتباه

9783319759777

عنوان اصلي

Propulsion and power :

نام عام مواد

[Book]

ساير اطلاعات عنواني

an exploration of gas turbine performance modeling /

نام نخستين پديدآور

Joachim Kurzke, Ian Halliwell.

محل نشرو پخش و غیره

Cham :

نام ناشر، پخش کننده و غيره

Springer,

تاریخ نشرو بخش و غیره

2018.

نام خاص و کميت اثر

1 online resource

متن يادداشت

Intro; Preface; Contents; About the Authors; Acknowledgements; Introduction; Simulation Tasks; 1 New Engine Design; 1.1 Nomenclature; 1.2 Generation of Shaft Power; 1.2.1 Ideal Thermodynamic Cycles; 1.2.1.1 Methods to Increase the Power Output; 1.2.1.2 Methods for Reducing Fuel Consumption; 1.2.2 The Efficiency of Shaft Power Generation; 1.2.2.1 Ideal Cycles; 1.2.2.2 Real Cycles; 1.2.2.3 Back to the Definition of Efficiency; 1.2.3 Combined Cycle; 1.2.3.1 The Heat Recovery Steam Generator (HRSG); 1.2.3.2 Steam Turbine; 1.2.3.3 Combined Cycle Output; 1.3 Aircraft Propulsion; 1.3.1 Turbojet.

متن يادداشت

1.3.1.1 Ideal Turbojet Cycle1.3.1.2 A Method to Increase Turbojet Thrust; 1.3.1.3 Effect of Flight Velocity; 1.3.2 More Definitions of Efficiency; 1.3.2.1 Real Turbojet Cycle; 1.3.2.2 Efficiency of the Turbojet with Reheat (Afterburner); 1.3.3 Turbofan; 1.4 Fundamental Design Decisions; 1.4.1 Turbofan: Mixed Flow or Separate Flow?; 1.4.1.1 Separate Flow Turbofan; 1.4.1.2 Mixed Flow Turbofan; 1.4.1.3 Comparison at Constant Propulsive Efficiency; 1.4.2 Dry or Reheated Turbofan?; 1.4.2.1 Reheated Turbofans for Supersonic Flight; 1.4.2.2 Dry Turbofans for Supersonic Flight.

متن يادداشت

1.4.3 Convergent or Convergent-Divergent Nozzle?1.4.4 Single or Two Stage High Pressure Turbine?; 1.4.4.1 Simple Cycle Study; 1.4.4.2 Realistic Optimization; 1.4.4.3 Engines with Single Stage Turbines; 1.4.4.4 Design with Prescribed Rotor Blade Metal Temperature; 1.4.4.5 Engines with Two-Stage Turbines; 1.4.4.6 Conclusion; 1.5 Conceptual Turbofan Design; 1.5.1 Flow Annulus; 1.5.1.1 Local Mach Numbers; 1.5.1.2 Hub/Tip Radius Ratio; 1.5.1.3 Relationships Between Components; 1.5.1.4 Spool Speed; 1.5.1.5 Core Size; 1.5.2 Direct Drive or with a Gearbox?

متن يادداشت

1.5.3 Conventional Turbofans with Bypass Ratios Between 6 and 141.5.3.1 Fan and Booster; 1.5.3.2 Bypass; 1.5.3.3 Low Pressure Turbine; 1.5.3.4 Effect of Spool Speed; 1.5.4 Turbofan with Gearbox; 1.5.5 Comparison; 1.5.5.1 Mechanics; 1.5.5.2 Aerodynamics; 1.5.6 The Fundamental Differences; 1.6 Mission Analysis; 1.6.1 General Requirements; 1.6.2 Single Point Design; 1.6.3 Multi-point Design; 1.6.3.1 Commercial Aircraft; 1.6.3.2 Fighter Aircraft; 1.6.4 High Speed Propulsion; 1.6.4.1 Point Performance; 1.6.4.2 Turbojet; 1.6.4.3 Turbojet with Reheat (Afterburner); 1.6.4.4 Turbofan with Reheat.

متن يادداشت

1.6.4.5 Ramjet1.6.4.6 Acceleration to High Mach Numbers; 1.7 References; 2 Engine Families; 2.1 Baseline Engine; 2.2 Derivative Engine; 2.2.1 Fan and Booster; 2.2.2 Core Compressor; 2.2.3 Combustor; 2.2.4 High Pressure Turbine; 2.2.5 Low Pressure Turbine; 2.3 Optimizing the Growth Engine; 2.3.1 Design Variables; 2.3.2 Design Constraints; 2.3.3 Figure of Merit; 2.3.4 Ranges for the Design Variables; 2.3.5 Starting Point; 2.3.6 Graphical User Interface; 2.4 Exploring the Design Space; 2.5#x83;References; 3 Modeling an Engine; 3.1 Sources of Data; 3.1.1 Magazines and Marketing Brochures.

بدون عنوان

0

بدون عنوان

8

بدون عنوان

8

بدون عنوان

8

بدون عنوان

8

متن يادداشت

The book is written for engineers and students who wish to address the preliminary design of gas turbine engines, as well as the associated performance calculations, in a practical manner. A basic knowledge of thermodynamics and turbomachinery is a prerequisite for understanding the concepts and ideas described. The book is also intended for teachers as a source of information for lecture materials and exercises for their students. It is extensively illustrated with examples and data from real engine cycles, all of which can be reproduced with GasTurb (TM). It discusses the practical application of thermodynamic, aerodynamic and mechanical principles. The authors describe the theoretical background of the simulation elements and the relevant correlations through which they are applied, however they refrain from detailed scientific derivations.

منبع سفارش / آدرس اشتراک

Springer

عنوان

Propulsion and power.

شماره استاندارد بين المللي کتاب و موسيقي

9783319759777

موضوع مستند نشده

Gas-turbines-- Performance.

موضوع مستند نشده

Gas-turbines-- Performance.

موضوع مستند نشده

TECHNOLOGY & ENGINEERING-- Mechanical.

موضوع مستند نشده

TEC-- 009070

موضوع مستند نشده

TGMF

موضوع مستند نشده

TGMF1

شماره

ويراست

شماره رده

مستند نام اشخاص تاييد نشده

Kurzke, Joachim.

مستند نام اشخاص تاييد نشده

Halliwell, Ian.

تاريخ عمليات

20200823110508.0

قواعد فهرست نويسي ( بخش توصيفي )

pn

نام الکترونيکي

نوع ماده

[Book]

تكميل شده

Y