Reasons for Triple-Funding of the Jet-Engine-Industry to Meet 2020–2040 6th-Gen-Challenge: Counter-Air Penetration, CAP
Abstract
I often open my lectures with a question: Do you agree that as speed goes down in any landing, the vertical tail fails to orient the nose back to the runway under strong side winds while ONLY side deflecting jet-engine-steering (JES) can safely re-orient it to safe landing?Just facts, less opinions; And if you do, you accept the 1ST-element of jetonautics defined by 12 figures below, text and references 1 to 48.
References and Notes
1. CITATION: Forward by USAF Chief Scientist defines “Vectored Propulsion, Supermaneuverability and Robot Aircraft” by Benjamin Gal-Or, “LANDMARK BOOK”. Published by Springer Verlag, N.Y. and Heidelberg, 1989-present, multiple reprints. ISBN 0387-97,161-0, 3-540-87,161-0, TL685.3.G23 1989, 629.I34ʹ353-de20, 89-21,797. 237 references. 182 drawings.Search in Google Scholar
2. CITATION: U.S. AIR FORCE & NATO review from U.S., UK, Germany and JAPAN:“Benjamin Gal-Or & Wolfgang Herbst have influenced the direction of fighter aircraft design.” “Many of Gal-Or’s ideas, and those of Herbst, are now being tested and flown operationally” “Their technology will offer new challenges — Solving the inevitable human points problems that will emerge, involve questioning established doctrine and reaching for innovative and imaginative solutions.” Naval Post Graduate School, Introduction; ISBN 92-837—1065-7; RTO-EN-12, RTO-TR-015/HFM-015.Search in Google Scholar
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4. EDITORIAL:Jet Engine Steering(JES)– The new master of advanced flight control;Civilizing military JES technology maximizes flight safety and allows pilot recovery when AOOF fails to prevent a crash; Int’l J. Turbo & Jet Engines, 35(2):95–99, DOI: 10.1515/tjj-2018-9010. May 2018.10.1515/tjj-2018-9010Search in Google Scholar
5. Scientific mistakes that lead to denials of post-stall-flight by JES and its benefits: (1) First in Israel: with added compliments: “nonsense”, “you cannot fly post stall”, “read the textbooks”, “you bring shame on the Technion for such lunatic ideas”, “you should be fired for that nonsense”;(2) same: with Shidlovski’s Turbomeca in France and in Israel; (3) same: RR, less complements, in a meeting, Coventry, UK. Cf. 24, 26, 48 below and Figure 2.Search in Google Scholar
6. “Israelis Flight Test Jet-Powered RPV (Unmanned, Radio Controlled JES-Air-Vehicle) Fitted With Thrust Vectoring Nozzles”, AVIATION WEEK, May 18, p. 21, 1987; 30th May 1987.Search in Google Scholar
7. “ISRAEL FLIES VECTORING RPV”, FLIGHT INT’L, 30th May 1987; “Israel”, “RPVs”, JANE’S ALL THE WORLD’S AIRCRAFT. 1987. [First-time post-stall flight in the history of aviation of JES-STEALTH air vehicles – conducted at Megiddo Airfield, Israel, up to 170 AoA via first yaw-pitch-roll-JES combat Maneuvers including the first Performance of the post-stall “COBRA”].Search in Google Scholar
8. THRUST VECTOR CONTROL EYED FOR TRANSPORT, Aviation Week & Space Technology, 28th August 1995.Search in Google Scholar
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10. EDITORIAL:Global needs for Jet-Engine-Steered (JES) strike drones vs. lack of updated textbooks to design 6th generation UCLASS due to UCAV failure. Int’l J. Turbo & Jet Engines, 32(3), Jan 2015. DOI: 10.1515/tjj-2015-1001.10.1515/tjj-2015-1001Search in Google Scholar
11. EDITORIAL:RE-EDUCATING THE JET-ENGINE RESEARCHERS TO STAY RELEVANT, should follow changing uses of small and large jet engines, especially those anticipated to be used by/in the next generation. Int’l J. Turbo & Jet Engines, 33(2), July 2016; DOI: 10.1515/tjj-2016-5001.10.1515/tjj-2016-5001Search in Google Scholar
12. CITATION: “DESIGN PROJECT AT SIX UNIVERSITIES”:“Steps are being taken by major companies to take advantage of this. For instance, General Electric has been creating an axisymmetric vectoring exhaust nozzle. NASA and the United State Navy have been designing similar systems for controlling the direction of the exhaust.” Citing Int’l J. Turbo & Jet Engines, Editorials. https://www.researchgate.net/Search in Google Scholar
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18. EDITORIAL:FUTURE JET TECHNOLOGIES: THE JES-revolution in Air-&-Sea-Propulsion Science and R&D; Int’l J. Turbo & Jet Engines, Jan 2014. DOI: 10.1515/tjj-2014-1000.10.1515/tjj-2014-1000Search in Google Scholar
19. EDITORIAL:FUTURE JET TECHNOLOGIES: Fleets of low-cost, stealth, jet-steered drones are designed to fly ahead of fighter aircraft and bombers into congested regions. Int’l J. Turbo & Jet Engines, Jan 2013.Search in Google Scholar
20. EDITORIAL:FUTURE JET TECHNOLOGIES: Joint Design Team induce F-35 run-away costs, delays and performance compromises. Int’l J. Turbo & Jet Engines, Sep 2011.Search in Google Scholar
21. EDITORIAL:FUTURE JET TECHNOLOGIES: Air, Land and Marine applications of Jet Engine Steering aka as 3D thrust vectoring flight control or 2D-water TVC of super-agile boats or super-agile Littoral Combat Ships, [LCS]. Int’l J. Turbo & Jet Engines, Apr 2011.Search in Google Scholar
22. EDITORIAL:FUTURE JET TECHNOLOGIES: JES for advanced Unmanned Combat Air Vehicles, [JES-UCAV.]. Int’l J. Turbo & Jet Engines, Mar 2010.Search in Google Scholar
23. EDITORIAL:FUTURE JET TECHNOLOGIES: JET ENGINES AS PRIME FLIGHT EFFECTORS. THE FIRST KEY DESIGN RULES. Int’l J. Turbo & Jet Engines, Jul 1999, Dec 2000, Jan 2001 and Jan 2003.Search in Google Scholar
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25. CITATION;“The benefits of JES to fighter aircraft agility and to close-range combat ability, are now well recognized; several fighters with JES (e. g., F22, SU-37/30 MKI) are soon to be operational. Gal-or (Gal-Or, 1998). Classes of new aircraft controllability domains have been defined recently (Gal-Or, 1994; Gal-Or, Sherbaum and Lichtsinder, 1995; Gal-Or, 1995). A remotely piloted, reduced-scale Boeing 727 ‘With both AOOF and JES was flight tested in May 1995 to demonstrate the potentials for low-weight, add-on JES-kits for catastrophic failure prevention (Gal-Or, 1996)’; Also “a missile equipped with JES can effectively control its acceleration direction when the missile built only with aero fins fails, then maneuverability/controllability can be greatly enhanced by JES. Reference: Design of optimal midcourse guidance sliding-mode control for missiles with TVC”. Citing Id.Search in Google Scholar
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© 2018 Walter de Gruyter GmbH, Berlin/Boston
Articles in the same Issue
- Frontmatter
- Editorials
- Reasons for Triple-Funding of the Jet-Engine-Industry to Meet 2020–2040 6th-Gen-Challenge: Counter-Air Penetration, CAP
- Reasons for triple-funding of the jet-engine-industry to meet 2020-2040 6TH-Gen-Challenge: Counter-Air Penetration, CAP
- Original Research Articles
- Experimental Investigation of Reacting Flow Characteristics in a Dual-Mode Scramjet Combustor
- Experimental Investigation of Shape Transition Effects on Isolator Performance
- Effects of Inlet Parameters on Combustion Performance in Gas Turbine Combustor
- Gas Turbine Engine Gas-path Fault Diagnosis Based on Improved SBELM Architecture
- The Effects of Turbulent Burning Velocity Models in a Swirl-Stabilized Lean Premixed Combustor
- Inverse Simulation for Gas Turbine Engine Control through Differential Algebraic Inequality Formulation
- Aerodynamic Optimization of Turbine Based Combined Cycle Nozzle
- Nonlinear System Modeling based on System Equilibrium Manifold
- Numerical Study on Heat Transfer Enhancement of Swirl Chamber on Gas Turbine Blade
Articles in the same Issue
- Frontmatter
- Editorials
- Reasons for Triple-Funding of the Jet-Engine-Industry to Meet 2020–2040 6th-Gen-Challenge: Counter-Air Penetration, CAP
- Reasons for triple-funding of the jet-engine-industry to meet 2020-2040 6TH-Gen-Challenge: Counter-Air Penetration, CAP
- Original Research Articles
- Experimental Investigation of Reacting Flow Characteristics in a Dual-Mode Scramjet Combustor
- Experimental Investigation of Shape Transition Effects on Isolator Performance
- Effects of Inlet Parameters on Combustion Performance in Gas Turbine Combustor
- Gas Turbine Engine Gas-path Fault Diagnosis Based on Improved SBELM Architecture
- The Effects of Turbulent Burning Velocity Models in a Swirl-Stabilized Lean Premixed Combustor
- Inverse Simulation for Gas Turbine Engine Control through Differential Algebraic Inequality Formulation
- Aerodynamic Optimization of Turbine Based Combined Cycle Nozzle
- Nonlinear System Modeling based on System Equilibrium Manifold
- Numerical Study on Heat Transfer Enhancement of Swirl Chamber on Gas Turbine Blade