The Resource Aircraft Propulsion Systems Technology and Design
Aircraft Propulsion Systems Technology and Design
Resource Information
The item Aircraft Propulsion Systems Technology and Design represents a specific, individual, material embodiment of a distinct intellectual or artistic creation found in Missouri University of Science & Technology Library.This item is available to borrow from 1 library branch.
Resource Information
The item Aircraft Propulsion Systems Technology and Design represents a specific, individual, material embodiment of a distinct intellectual or artistic creation found in Missouri University of Science & Technology Library.
This item is available to borrow from 1 library branch.
- Language
- eng
- Extent
- 1 online resource (535 pages)
- Contents
-
- ""Cover""; ""Title""; ""Copyright""; ""Foreword""; ""Table of Contents""; ""Chapter 1. Design and Development of Aircraft Propulsion Systems""; ""1.1 Introduction""; ""1.2 Engine Design Objectives""; ""1.3 Effect of Thermodynamic Variables on Engine Performance""; ""1.4 Development of Thrust""; ""1.5 Off-Design Performance of Gas Turbine Propulsion Engines""; ""1.6 Losses in Available Energy""; ""1.7 Interrelations Among Aerodynamic Components""; ""1.8 Interaction with Other Specialties""; ""1.9 Advanced Flow Calculations""; ""1.10 Biography of a Typical Engine""
- ""Chapter 2. Turbopropulsion Combustion Technology""""2.1 Introduction""; ""2.2 Combustion System Description/Definitions""; ""2.3 Component Considerations""; ""2.4 Design Tools""; ""2.5 Future Requirements""; ""2.6 Conclusions""; ""Chapter 3. Engine/Airframe Performance Matching""; ""3.1 Introduction""; ""3.2 Mission Analysis""; ""3.3 Optimization of Engine/Airplane Match""; ""3.4 Sensitivity and Influence Coefficients""; ""3.5 Computer Simulation of Gas Turbine Engines""; ""Chapter 4. Inlets and Inlet/Engine Integration""; ""4.1 Introduction""
- ""4.2 Elements of a Successful Inlet/Engine Integration Program""""4.3 Definition of Subsonic Inlet/Engine Operational Requirements""; ""4.4 Definition of Supersonic Inlet/Engine Operational Requirements""; ""4.5 Engine Impact on Inlet Design""; ""4.6 Inlet Impact on Engine Design""; ""4.7 Validation of Inlet/Engine System""; ""Chapter 5. Variable Convergent-Divergent Exhaust Nozzle Aerodynamics""; ""5.1 Introduction""; ""5.2 Nozzle Concept""; ""5.3 Performance Predictions""; ""5.4 Aerodynamic Load Predictions""; ""Chapter 6. Engine Operability""; ""6.1 Introduction""; ""6.2 Definitions""
- ""6.3 Stability Assessment""""6.4 Aerodynamic Interface Plane""; ""6.5 Total Pressure Distortion""; ""6.6 Total Temperature Distortion""; ""6.7 Planar Waves""; ""6.8 Recoverability""; ""6.9 Analytical Techniques""; ""6.10 Summary""; ""Chapter 7. Aeroelasticity and Unsteady Aerodynamics""; ""7.1 Introduction""; ""7.2 Overview of Turbomachinery Flutter""; ""7.3 Brief Survey of Turbomachinery Flutter Regimes""; ""7.4 Elementary Considerations of Aircraft Wing Flutter""; ""7.5 Fundamental Differences Between Turbomachinery Flutter and Wing Flutter""
- ""7.6 Fundamental of Unsteady Aerodynamic Theory for Isolated Airfoils""""7.7 Unsteady Aerodynamic Theory for Cascaded Airfoils""; ""7.8 Dynamic Stall-Empiricism and Experiment""; ""7.9 Coupled Blade-Disk-Shroud Stability Theory""; ""Subject Index""; ""A""; ""B""; ""C""; ""D""; ""E""; ""F""; ""G""; ""H""; ""I""; ""K""; ""L""; ""M""; ""N""; ""O""; ""P""; ""R""; ""S""; ""T""; ""U""; ""V""; ""W""
- Isbn
- 9781600860218
- Label
- Aircraft Propulsion Systems Technology and Design
- Title
- Aircraft Propulsion Systems Technology and Design
- Language
- eng
- Cataloging source
- EBLCP
- http://library.link/vocab/creatorName
- Oates, Gordon C
- Dewey number
- 629.134/353
- Index
- no index present
- LC call number
- TL709 -- A44 1989eb
- Literary form
- non fiction
- Nature of contents
- dictionaries
- http://library.link/vocab/subjectName
-
- Aircraft gas-turbines
- Aircraft gas-turbines
- Label
- Aircraft Propulsion Systems Technology and Design
- Carrier category
- online resource
- Carrier category code
-
- cr
- Carrier MARC source
- rdacarrier
- Content category
- text
- Content type code
-
- txt
- Content type MARC source
- rdacontent
- Contents
-
- ""Cover""; ""Title""; ""Copyright""; ""Foreword""; ""Table of Contents""; ""Chapter 1. Design and Development of Aircraft Propulsion Systems""; ""1.1 Introduction""; ""1.2 Engine Design Objectives""; ""1.3 Effect of Thermodynamic Variables on Engine Performance""; ""1.4 Development of Thrust""; ""1.5 Off-Design Performance of Gas Turbine Propulsion Engines""; ""1.6 Losses in Available Energy""; ""1.7 Interrelations Among Aerodynamic Components""; ""1.8 Interaction with Other Specialties""; ""1.9 Advanced Flow Calculations""; ""1.10 Biography of a Typical Engine""
- ""Chapter 2. Turbopropulsion Combustion Technology""""2.1 Introduction""; ""2.2 Combustion System Description/Definitions""; ""2.3 Component Considerations""; ""2.4 Design Tools""; ""2.5 Future Requirements""; ""2.6 Conclusions""; ""Chapter 3. Engine/Airframe Performance Matching""; ""3.1 Introduction""; ""3.2 Mission Analysis""; ""3.3 Optimization of Engine/Airplane Match""; ""3.4 Sensitivity and Influence Coefficients""; ""3.5 Computer Simulation of Gas Turbine Engines""; ""Chapter 4. Inlets and Inlet/Engine Integration""; ""4.1 Introduction""
- ""4.2 Elements of a Successful Inlet/Engine Integration Program""""4.3 Definition of Subsonic Inlet/Engine Operational Requirements""; ""4.4 Definition of Supersonic Inlet/Engine Operational Requirements""; ""4.5 Engine Impact on Inlet Design""; ""4.6 Inlet Impact on Engine Design""; ""4.7 Validation of Inlet/Engine System""; ""Chapter 5. Variable Convergent-Divergent Exhaust Nozzle Aerodynamics""; ""5.1 Introduction""; ""5.2 Nozzle Concept""; ""5.3 Performance Predictions""; ""5.4 Aerodynamic Load Predictions""; ""Chapter 6. Engine Operability""; ""6.1 Introduction""; ""6.2 Definitions""
- ""6.3 Stability Assessment""""6.4 Aerodynamic Interface Plane""; ""6.5 Total Pressure Distortion""; ""6.6 Total Temperature Distortion""; ""6.7 Planar Waves""; ""6.8 Recoverability""; ""6.9 Analytical Techniques""; ""6.10 Summary""; ""Chapter 7. Aeroelasticity and Unsteady Aerodynamics""; ""7.1 Introduction""; ""7.2 Overview of Turbomachinery Flutter""; ""7.3 Brief Survey of Turbomachinery Flutter Regimes""; ""7.4 Elementary Considerations of Aircraft Wing Flutter""; ""7.5 Fundamental Differences Between Turbomachinery Flutter and Wing Flutter""
- ""7.6 Fundamental of Unsteady Aerodynamic Theory for Isolated Airfoils""""7.7 Unsteady Aerodynamic Theory for Cascaded Airfoils""; ""7.8 Dynamic Stall-Empiricism and Experiment""; ""7.9 Coupled Blade-Disk-Shroud Stability Theory""; ""Subject Index""; ""A""; ""B""; ""C""; ""D""; ""E""; ""F""; ""G""; ""H""; ""I""; ""K""; ""L""; ""M""; ""N""; ""O""; ""P""; ""R""; ""S""; ""T""; ""U""; ""V""; ""W""
- Control code
- 922978802
- Dimensions
- unknown
- Extent
- 1 online resource (535 pages)
- Form of item
- online
- Isbn
- 9781600860218
- Media category
- computer
- Media MARC source
- rdamedia
- Media type code
-
- c
- Specific material designation
- remote
- System control number
- (OCoLC)922978802
- Label
- Aircraft Propulsion Systems Technology and Design
- Carrier category
- online resource
- Carrier category code
-
- cr
- Carrier MARC source
- rdacarrier
- Content category
- text
- Content type code
-
- txt
- Content type MARC source
- rdacontent
- Contents
-
- ""Cover""; ""Title""; ""Copyright""; ""Foreword""; ""Table of Contents""; ""Chapter 1. Design and Development of Aircraft Propulsion Systems""; ""1.1 Introduction""; ""1.2 Engine Design Objectives""; ""1.3 Effect of Thermodynamic Variables on Engine Performance""; ""1.4 Development of Thrust""; ""1.5 Off-Design Performance of Gas Turbine Propulsion Engines""; ""1.6 Losses in Available Energy""; ""1.7 Interrelations Among Aerodynamic Components""; ""1.8 Interaction with Other Specialties""; ""1.9 Advanced Flow Calculations""; ""1.10 Biography of a Typical Engine""
- ""Chapter 2. Turbopropulsion Combustion Technology""""2.1 Introduction""; ""2.2 Combustion System Description/Definitions""; ""2.3 Component Considerations""; ""2.4 Design Tools""; ""2.5 Future Requirements""; ""2.6 Conclusions""; ""Chapter 3. Engine/Airframe Performance Matching""; ""3.1 Introduction""; ""3.2 Mission Analysis""; ""3.3 Optimization of Engine/Airplane Match""; ""3.4 Sensitivity and Influence Coefficients""; ""3.5 Computer Simulation of Gas Turbine Engines""; ""Chapter 4. Inlets and Inlet/Engine Integration""; ""4.1 Introduction""
- ""4.2 Elements of a Successful Inlet/Engine Integration Program""""4.3 Definition of Subsonic Inlet/Engine Operational Requirements""; ""4.4 Definition of Supersonic Inlet/Engine Operational Requirements""; ""4.5 Engine Impact on Inlet Design""; ""4.6 Inlet Impact on Engine Design""; ""4.7 Validation of Inlet/Engine System""; ""Chapter 5. Variable Convergent-Divergent Exhaust Nozzle Aerodynamics""; ""5.1 Introduction""; ""5.2 Nozzle Concept""; ""5.3 Performance Predictions""; ""5.4 Aerodynamic Load Predictions""; ""Chapter 6. Engine Operability""; ""6.1 Introduction""; ""6.2 Definitions""
- ""6.3 Stability Assessment""""6.4 Aerodynamic Interface Plane""; ""6.5 Total Pressure Distortion""; ""6.6 Total Temperature Distortion""; ""6.7 Planar Waves""; ""6.8 Recoverability""; ""6.9 Analytical Techniques""; ""6.10 Summary""; ""Chapter 7. Aeroelasticity and Unsteady Aerodynamics""; ""7.1 Introduction""; ""7.2 Overview of Turbomachinery Flutter""; ""7.3 Brief Survey of Turbomachinery Flutter Regimes""; ""7.4 Elementary Considerations of Aircraft Wing Flutter""; ""7.5 Fundamental Differences Between Turbomachinery Flutter and Wing Flutter""
- ""7.6 Fundamental of Unsteady Aerodynamic Theory for Isolated Airfoils""""7.7 Unsteady Aerodynamic Theory for Cascaded Airfoils""; ""7.8 Dynamic Stall-Empiricism and Experiment""; ""7.9 Coupled Blade-Disk-Shroud Stability Theory""; ""Subject Index""; ""A""; ""B""; ""C""; ""D""; ""E""; ""F""; ""G""; ""H""; ""I""; ""K""; ""L""; ""M""; ""N""; ""O""; ""P""; ""R""; ""S""; ""T""; ""U""; ""V""; ""W""
- Control code
- 922978802
- Dimensions
- unknown
- Extent
- 1 online resource (535 pages)
- Form of item
- online
- Isbn
- 9781600860218
- Media category
- computer
- Media MARC source
- rdamedia
- Media type code
-
- c
- Specific material designation
- remote
- System control number
- (OCoLC)922978802
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<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.library.mst.edu/portal/Aircraft-Propulsion-Systems-Technology-and/bGTy1xAF-bU/" typeof="Book http://bibfra.me/vocab/lite/Item"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.library.mst.edu/portal/Aircraft-Propulsion-Systems-Technology-and/bGTy1xAF-bU/">Aircraft Propulsion Systems Technology and Design</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.library.mst.edu/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.library.mst.edu/">Missouri University of Science & Technology Library</a></span></span></span></span></div>
