Benjamin Gal-Or
Vectored Propulsion, Supermaneuverability and Robot Aircraft
Benjamin Gal-Or
Vectored Propulsion, Supermaneuverability and Robot Aircraft
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This book is designed to fill a professional vacuum in the new field of advance, high-angle, vectored stealth aircraft. The subject matter presented in the volume has never before been investigated and presented as a unified field of study because it covers entirely new fields and because specialized fragments of this unified field are scattered throughout literature in specific problems. The book is of interest to aeronautical and mechanical engineers, electrical and control engineers, aerospace industry, USAF, US Navy, NASA, pilots and instructors.
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This book is designed to fill a professional vacuum in the new field of advance, high-angle, vectored stealth aircraft. The subject matter presented in the volume has never before been investigated and presented as a unified field of study because it covers entirely new fields and because specialized fragments of this unified field are scattered throughout literature in specific problems. The book is of interest to aeronautical and mechanical engineers, electrical and control engineers, aerospace industry, USAF, US Navy, NASA, pilots and instructors.
Hinweis: Dieser Artikel kann nur an eine deutsche Lieferadresse ausgeliefert werden.
Hinweis: Dieser Artikel kann nur an eine deutsche Lieferadresse ausgeliefert werden.
Produktdetails
- Produktdetails
- Verlag: Springer / Springer New York / Springer, Berlin
- Artikelnr. des Verlages: 978-0-387-97161-2
- 1991.
- Seitenzahl: 280
- Erscheinungstermin: 12. März 1991
- Englisch
- Abmessung: 244mm x 170mm x 16mm
- Gewicht: 510g
- ISBN-13: 9780387971612
- ISBN-10: 0387971610
- Artikelnr.: 24470388
- Herstellerkennzeichnung
- Books on Demand GmbH
- In de Tarpen 42
- 22848 Norderstedt
- info@bod.de
- 040 53433511
- Verlag: Springer / Springer New York / Springer, Berlin
- Artikelnr. des Verlages: 978-0-387-97161-2
- 1991.
- Seitenzahl: 280
- Erscheinungstermin: 12. März 1991
- Englisch
- Abmessung: 244mm x 170mm x 16mm
- Gewicht: 510g
- ISBN-13: 9780387971612
- ISBN-10: 0387971610
- Artikelnr.: 24470388
- Herstellerkennzeichnung
- Books on Demand GmbH
- In de Tarpen 42
- 22848 Norderstedt
- info@bod.de
- 040 53433511
Preface.- Acknowledgements.- Glossary and Notation.- The main problems of thrust-vectored maneuverability - Vectored Aircraft: Breaking the "Stall Barrier" - The New Standard Technology - Civil Applications.- Soviet and Western Concepts - Research tools - Cold propulsion - The Fundamental Definitions of Pure Vectored Aircraft (PVA).- Pure Sideslip Maneuvers (PSM) - Combat Applications -.- Partially-Vectored Aircraft.- Agility, Supermaneuverability and Supercontrollability.- Load factors.- "Energy" Vs. "Angles" Fights - Time Lags -.- The Overall Combat Picture.- Minimum Time Turns - Low Observability - Stealth RPVs.- The Time Gaps.- New Educational Shifts.- Concluding Remarks.- Lecture I: Fundamental Concepts Revisited and Redefined.- New Missions and Modified Design Trends.- Early Conceptual Design Limitations.- Internal Thrust Vectoring.- Engine Nozzle Redefined.- Performance Comparisons.- Subsonic Yaw-Pitch-Roll Thrust Vectoring.- Lecture II: Vectored Aircraft and Supermaneuverability.- Yaw-Pitch Vectoring and Supercirculation.- Pure Jetborne Flight Control.- STOL or V/STOL Vectored Aircraft.- Dimensionless Numbers for Pure Vectored Aircraft.- Emergency Landing.- Air-to-Air Operations.- Air-to-Ground Operations.- Propulsion and Supermaneuverability.- Maneuver Analysis.- Controllability Limits.- High-Alpha Flight Envelopes.- The Non-Availability of a "Vectored Inlet".- Lecture III: The Matrix of Unknown Variables of Vectored Aircraft.- Reservations and Precautions.- Technology Limits.- Cooling Limits.- Nozzle Aspect Ratio Limits.- Aerodynamic Effects.- Nozzle Coefficients Revisited.- Thrust Vectoring Range.- Induced drag and Supercirculaton.- Lecture IV: Vectored Aircraft as R&D Tools, or as Super-Agile Robotic Flying Systems.-Cruise Missiles, RPVs, etc.- Expanded Missions Vs. R&D tools.- Cost-Effectiveness of Flying Vectored RPVs.- Synergetic Studies.- Master Plan and New Programs.- Scaling Consideratons.- Lecture V: Partially Vectored Aircraft.- Canard-Configured Vectored Aircraft.- Upgrading extant Aircraft to Become Vectored Fighters - The Vectored F-15 Fighter.- Upgrading F-l8 and F-16 Fighters.- The Search for Design Philosophy in the Post-ATF Era.- Lecture VI: The Pros and Cons of Internal Thrust Vectoring.- Is ETV Effective in the RaNPAS-PST Domain?.- The Propulsion System of the Vectored X-31, X-29, etc.- Stability and Flight Control.- Power-Lift Aircraft.- Appendix A: A Brief Historical Survey.- Appendix B: Powerplant Technology Limits.- Beyond the Year 2000/RCC/STOVL.- Current-Technology Limits and Trends.- Whole-System Engineering Approach.- European Fighter Engines.- New Fighter Engines: The ATF and Other New Engines.- The MiG-29 and Su-27 Propulsion Systems.- Variable Cycle, Turbine Bypass, and Supersonic-Fan Engines.- Appendix C: Nozzle Performance [Data-Base-1].- Appendix D Nozzle Synergetic Effects [Data-Base-2].- Appendix E: Temperature Distribution Test Facility.- Appendix F: Limiting Engine-Inlet Envelopes and IFPC.- PST Inlet Design.- IFPC Transient Definitions.- Appendix G: On Some Other Vectored/Stealth Aircraft Consideratons.- Appendix H: Thought-Provoking and Thought-Depressing Quotations.- References.
Preface.- Acknowledgements.- Glossary and Notation.- The main problems of thrust-vectored maneuverability - Vectored Aircraft: Breaking the "Stall Barrier" - The New Standard Technology - Civil Applications.- Soviet and Western Concepts - Research tools - Cold propulsion - The Fundamental Definitions of Pure Vectored Aircraft (PVA).- Pure Sideslip Maneuvers (PSM) - Combat Applications -.- Partially-Vectored Aircraft.- Agility, Supermaneuverability and Supercontrollability.- Load factors.- "Energy" Vs. "Angles" Fights - Time Lags -.- The Overall Combat Picture.- Minimum Time Turns - Low Observability - Stealth RPVs.- The Time Gaps.- New Educational Shifts.- Concluding Remarks.- Lecture I: Fundamental Concepts Revisited and Redefined.- New Missions and Modified Design Trends.- Early Conceptual Design Limitations.- Internal Thrust Vectoring.- Engine Nozzle Redefined.- Performance Comparisons.- Subsonic Yaw-Pitch-Roll Thrust Vectoring.- Lecture II: Vectored Aircraft and Supermaneuverability.- Yaw-Pitch Vectoring and Supercirculation.- Pure Jetborne Flight Control.- STOL or V/STOL Vectored Aircraft.- Dimensionless Numbers for Pure Vectored Aircraft.- Emergency Landing.- Air-to-Air Operations.- Air-to-Ground Operations.- Propulsion and Supermaneuverability.- Maneuver Analysis.- Controllability Limits.- High-Alpha Flight Envelopes.- The Non-Availability of a "Vectored Inlet".- Lecture III: The Matrix of Unknown Variables of Vectored Aircraft.- Reservations and Precautions.- Technology Limits.- Cooling Limits.- Nozzle Aspect Ratio Limits.- Aerodynamic Effects.- Nozzle Coefficients Revisited.- Thrust Vectoring Range.- Induced drag and Supercirculaton.- Lecture IV: Vectored Aircraft as R&D Tools, or as Super-Agile Robotic Flying Systems.-Cruise Missiles, RPVs, etc.- Expanded Missions Vs. R&D tools.- Cost-Effectiveness of Flying Vectored RPVs.- Synergetic Studies.- Master Plan and New Programs.- Scaling Consideratons.- Lecture V: Partially Vectored Aircraft.- Canard-Configured Vectored Aircraft.- Upgrading extant Aircraft to Become Vectored Fighters - The Vectored F-15 Fighter.- Upgrading F-l8 and F-16 Fighters.- The Search for Design Philosophy in the Post-ATF Era.- Lecture VI: The Pros and Cons of Internal Thrust Vectoring.- Is ETV Effective in the RaNPAS-PST Domain?.- The Propulsion System of the Vectored X-31, X-29, etc.- Stability and Flight Control.- Power-Lift Aircraft.- Appendix A: A Brief Historical Survey.- Appendix B: Powerplant Technology Limits.- Beyond the Year 2000/RCC/STOVL.- Current-Technology Limits and Trends.- Whole-System Engineering Approach.- European Fighter Engines.- New Fighter Engines: The ATF and Other New Engines.- The MiG-29 and Su-27 Propulsion Systems.- Variable Cycle, Turbine Bypass, and Supersonic-Fan Engines.- Appendix C: Nozzle Performance [Data-Base-1].- Appendix D Nozzle Synergetic Effects [Data-Base-2].- Appendix E: Temperature Distribution Test Facility.- Appendix F: Limiting Engine-Inlet Envelopes and IFPC.- PST Inlet Design.- IFPC Transient Definitions.- Appendix G: On Some Other Vectored/Stealth Aircraft Consideratons.- Appendix H: Thought-Provoking and Thought-Depressing Quotations.- References.