Exergy analysis and design optimization for aerospace vehicles and systems:
Gespeichert in:
| Format: | Buch |
|---|---|
| Sprache: | English |
| Veröffentlicht: |
Reston, Va
American Inst. of Aeronautics & Astronautics
2011
|
| Schriftenreihe: | Progress in astronautics and aeronautics
238 |
| Schlagworte: | |
| Online-Zugang: | Inhaltsverzeichnis |
| Beschreibung: | XXIV, 632 S. graph. Darst. |
| ISBN: | 9781600868399 |
Internformat
MARC
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Datensatz im Suchindex
| _version_ | 1804153237535719424 |
|---|---|
| adam_text | Titel: Exergy analysis and design optimization for aerospace vehicles and systems
Autor: Camberos, José A.
Jahr: 2011
TABLE OF CONTENTS
Preface ..............................................xv
Acknowledgments ....................................xvii
Nomenclature .........................................xxi
Chapter 1 Introduction ................................ 1
David J. Moorhouse, and Jose A. Camberos, U.S. Air Force Research Laboratory,
Wright-Patterson AF8, Ohio
References.................................................. 7
Suggested Reading........................................... 8
Chapter 2 Fundamentals of Exergy Analysis ................. 9
Jose A. Camberos, U.S. Air Force Research Laboratory, Wright-Patterson AFB, Ohio, and
John H. Doty, University of Dayton, Dayton, Ohio
2.1 Overview.............................................. 9
2.2 Objectives............................................ 10
2.3 The Second Law of Thermodynamics....................... 11
2.4 Reversible and Irreversible Processes ....................... 24
2.5 The Carnot Principles Applied to Heat Engines................ 32
2.6 Entropy.............................................. 38
2.7 The Entropy Balance.................................... 46
2.8 Isentropic Processes..................................... 50
2.9 Exergy: A Measure of Work Potential ....................... 53
2.10 Types of Exergy........................................ 54
2.11 Exergy and Exergy Change of a System ..................... 57
2.12 Exergy Destruction and Exergy Transfer..................... 60
2.13 Exergy Balance of Closed and Open Systems................. 64
2.14 Second-Law-Based Efficiencies............................ 66
2.15 Exergy Analysis........................................ 74
2.16 Summary............................................. 75
2.17 Conclusion............................................ 75
References................................................. 76
Bibliography................................................ 76
TABLE OF CONTENTS
Chapter 3 Applications of Exergy Analysis ................. 77
John H. Doty, University of Dayton, Dayton, Ohio, and Jose A. Camberos
U.S. Air Force Research Laboratory, Wright-Patterson AFB, Ohio
3.1 Overview.............................................. 77
3.2 Case Study One: Steam Power Turbine....................... 80
3.3 Case Study Two: Supersonic Turbojet/Wing System............. 96
References................................................ 138
Chapter 4 Integrated Subsystem Analysis Using Entropy
Generation Minimization .............................. 141
Richard S. Figliola, Clemson University, Clemson, South Carolina, Robert Tipton,
Lockheed Martin Corporation, Marietta, Georgia, and Haipeng Li, Microsoft
Corporation, Redmond, Washington
4.1 Overview............................................. 141
4.2 Approach............................................. 143
4.3 System Model......................................... 146
4.4 Results and Discussion .................................. 151
4.5 Conclusion............................................ 158
References................................................ 159
Bibliography............................................... 160
Chapter 5 Exergy-Based Design Methodology for Airfoil Shape
Optimization and Wing Analysis ......................... 161
Richard S. Figliola, Clemson University, Clemson, South Carolina
5.1 Overview............................................. 161
5.2 Approach............................................. 162
5.3 Example: Airfoil Shape Optimization........................ 164
5.4 Example: Drag Estimation Using Exergy Methods.............. 167
5.5 Conclusions........................................... 178
References................................................ 179
Bibliography............................................... 180
Chapter 6 Entropy Generation and Aerospace Vehicle
Performance ........................................ 181
David W. Riggins, Missouri University of Science Technology-Rolla,
Rolla, Missouri, David J. Moorhouse, U.S. Air Force Research Laboratory,
Wright-Patterson AFB, Ohio, and Jose A. Camberos, U.S. Air Force Research
Laboratory, Wright-Patterson AFB, Ohio
6.1 Introduction.......................................... 181
TABLE ..OF CONIINTS
6.2 Functional Dependence of Forces Experienced by Fluid in
Streamtubes ......................................... 184
6.3 Vehicle Control Volume Selection and Force Auditing......... 194
6.4 Loss Allocation in Streamtubes with Differential or
Spatial Flow-Field Information............................ 198
6.5 Relationship of Wake Irreversibility to Vehicle
Performance: Theoretical Development .................... 208
6.6 Wake Mixing Process................................... 213
6.7 Universal Law for Aerospace Vehicle Performance and Entropy
Production and Overall Efficiency......................... 216
6.8 Theoretical Framework for General Relationship of
Vehicle Forces to Entropy Production...................... 217
6.9 Irreversibility in Wake Due to Irreversibility over
or Through Vehicle.................................... 224
6.10 Conclusions.......................................... 225
References................................................ 226
Chapter 7 Optimization Using Entropy-Generation
Minimization for Maximum Performance of Hypersonic Vehicles 229
David W. Riggins, Missouri University of Science Technology-Rolla, Rolla,
Missouri, David J. Moorhouse, U.S. Air Force Research Laboratory,
Wright-Patterson AFB, Ohio, Jose A. Camberos, U.S. Air Force Research Laboratory,
Wright-Patterson AFB, Ohio, and Michael von Spakovsky, Virginia Institute of
Technology, Blacksburg, Virginia
7.1 Introduction........................................... 229
7.2 Comparison and Evaluation of Performance/Optimization Metrics 233
7.3 Results and Discussion .................................. 235
7.4 Conclusion............................................ 254
References................................................ 255
Appendix A: Details of Calculation Procedures and Concepts for
Analytical Examples in Text................................. 256
Appendix B: Flow-Field and Performance Data for Selected Cases
for Examples in Text....................................... 265
Chapter 8 Characterization of Aerospace Vehicle Performance
and Mission Analysis Using Exergy ....................... 275
David W. Riggins, Missouri University of Science Technology-Rolla, Rolla,
Missouri, David J. Moorhouse, U.S. Air Force Research Laboratory,
Wright-Patterson AFB, Ohio, and Jose A. Camberos, U.S. Air Force Research
Laboratory, Wright-Patterson AFB, Ohio
8.1 Introduction........................................... 275
TABLE OF CONTENTS
8.2 Availability Balance for Aerospace Vehicles................... 278
8.3 Combination of Availability Balance with Vehicle Equations of
Motion............................................... 280
8.4 Propellant Mass Fraction Analysis.......................... 285
8.5 Availability Loss Rate Description for Aerospace Vehicles........ 290
8.6 Minimization of Overall Lost Availability Rate for Aerospace
Vehicles.............................................. 297
8.7 Conclusions........................................... 304
References................................................ 306
Chapter 9 Mission-Integrated Synthesis and Design
Optimization (MIS/DO) of Aerospace Vehicles .............. 309
Michael von Spakovsky, Virginia Institute of Technology, Blacksburg, Virginia
9.1 Introduction........................................... 309
9.2 System Synthesis/Design Multilevel Optimization Techniques .... 311
9.3 Exergy Modeling and Analysis............................. 326
9.4 Conclusions........................................... 336
References................................................ 336
Chapter 10 MIS/DO Applied to High Performance Aerospace
Vehicles ........................................... 343
Michael von Spakovsky, Virginia Institute of Technology, Blacksburg, Virginia
10.1 Introduction.......................................... 343
10.2 Application of a Decomposition Strategy to the Optimal
Synthesis/Design and Operation of an Advanced Tactical
Aircraft System ....................................... 344
10.3 Energy- vs Exergy-Based Figures of Merit for the Optimal
Synthesis/Design of High Performance Aircraft Systems ....... 378
10.4 Large-Scale Synthesis/Design Optimization and Exergy
Analysis of the Benefits and Design Challenges of
Morphing-Wing Aircraft................................. 394
10.5 Application of an Exergy-Based Approach to the
Generic Analysis and Optimization of Hypersonic Vehicles...... 411
References................................................ 434
Chapter 11 Thermodynamics, Entropy Generation
Minimization, and the Constructal Law .................... 441
Adrian Bejan, Duke University, Durham, North Carolina
TABLE OF CONTENTS
11.1 Thermodynamics, at Odds with the Physics Phenomenon of
Design Generation..................................... 441
11.2 Entropy Generation Minimization (EGM).................... 446
11.3 The Constructal Law................................... 448
11.4 Conclusion........................................... 452
References................................................ 455
Chapter 12 Quantum Thermodynamics and the Modeling of
Nonequilibrium Phenomena: Theory and Future Directions .... 457
Michael von Spakovsky, Virginia Institute of Technology, Blacksburg, Virginia
12.1 Introduction.......................................... 457
12.2 Irreversibility Paradox: Proposed Resolutions ................ 460
12.3 Kinematics of QT...................................... 466
12.4 Dynamics of QT....................................... 474
References................................................ 501
Chapter 13 Numerical Methods in Light of the Second Law ... 507
Jose A. Camberos, U.S. Air Force Research Laboratory, Wright-Patterson AFB, Ohio
13.1 Overview........................................... 507
13.2 Introduction......................................... 507
13.3 Entropy, Stability, and Probability........................ 512
13.4 The Construction of Entropy Balance Equations............. 526
13.5 Continuum Thermomechanics........................... 531
13.6 The Construction of Exergy Balance Equations.............. 534
13.7 Exergy Balance Equation............................... 541
13.8 Applications: Numerical Error and Stability................. 548
13.9 Analysis of Numerical Error............................. 555
13.10 Numerical Experiments................................ 587
13.11 Conclusions......................................... 595
References................................................ 596
Postlude ............................................601
Index ..............................................605
Supporting Materials ..................................633
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| series2 | Progress in astronautics and aeronautics |
| spelling | Exergy analysis and design optimization for aerospace vehicles and systems ed. by José A. Camberos ... Reston, Va American Inst. of Aeronautics & Astronautics 2011 XXIV, 632 S. graph. Darst. txt rdacontent n rdamedia nc rdacarrier Progress in astronautics and aeronautics 238 Exergie (DE-588)4015955-3 gnd rswk-swf Aerodynamik (DE-588)4000589-6 gnd rswk-swf Turbine (DE-588)4061226-0 gnd rswk-swf Tragflügel (DE-588)4060582-6 gnd rswk-swf Turbine (DE-588)4061226-0 s Tragflügel (DE-588)4060582-6 s Aerodynamik (DE-588)4000589-6 s Exergie (DE-588)4015955-3 s DE-604 Camberos, José A. Sonstige oth Progress in astronautics and aeronautics 238 (DE-604)BV001890233 238 HBZ Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=027934267&sequence=000002&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | Exergy analysis and design optimization for aerospace vehicles and systems Progress in astronautics and aeronautics Exergie (DE-588)4015955-3 gnd Aerodynamik (DE-588)4000589-6 gnd Turbine (DE-588)4061226-0 gnd Tragflügel (DE-588)4060582-6 gnd |
| subject_GND | (DE-588)4015955-3 (DE-588)4000589-6 (DE-588)4061226-0 (DE-588)4060582-6 |
| title | Exergy analysis and design optimization for aerospace vehicles and systems |
| title_auth | Exergy analysis and design optimization for aerospace vehicles and systems |
| title_exact_search | Exergy analysis and design optimization for aerospace vehicles and systems |
| title_full | Exergy analysis and design optimization for aerospace vehicles and systems ed. by José A. Camberos ... |
| title_fullStr | Exergy analysis and design optimization for aerospace vehicles and systems ed. by José A. Camberos ... |
| title_full_unstemmed | Exergy analysis and design optimization for aerospace vehicles and systems ed. by José A. Camberos ... |
| title_short | Exergy analysis and design optimization for aerospace vehicles and systems |
| title_sort | exergy analysis and design optimization for aerospace vehicles and systems |
| topic | Exergie (DE-588)4015955-3 gnd Aerodynamik (DE-588)4000589-6 gnd Turbine (DE-588)4061226-0 gnd Tragflügel (DE-588)4060582-6 gnd |
| topic_facet | Exergie Aerodynamik Turbine Tragflügel |
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