Jet-Engines Revised Dictionary for the 6th-Generation-R&D in a New Era

References and notes

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21. Editorial, Jet-Engine-Steered (JES), lack of updated textbooks to design 6th-generation air and sea combat vehicles, Int’l J. Turbo & Jet Engines, 32(3), Jan 2015. DOI: 10.1515/tjj-2015-1001.10.1515/tjj-2015-1001Search in Google Scholar

22. 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

23. 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

24. 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

25. Editorial, Old-New European debate on thrust vectoring and adverse effects of canards, Int’l J. Turbo & Jet Engines, Jan 1997. Cf. [33, 34].Search in Google Scholar

26. Editorial, RE-EDUCATING THE JET-ENGINE RESEARCHERS TO STAY RELEVANT, Int’l J. Turbo & Jet Engines, 33(2), July 2016; DOI: 10.1515/tjj-2016-5001.10.1515/tjj-2016-5001Search in Google Scholar

27. 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

28. Editorial, CANCELED UCLASS-UCAV- STRIKE-PROGRAMS, down playing 6th-gen-WVR-JES, Design Team induces F-35 run-away costs & performance compromises. Int’l J. Turbo & Jet Engines, Sep 2011. Cf. GAO, [69].Search in Google Scholar

29. Editorial, JET ENGINE STEERING TECHNOLOGY TRANSFERS, Int’l J. Turbo & Jet Engines, 31(4):277-285, Dec 2014; DOI: 10.1515/tjj-2014-1001.10.1515/tjj-2014-1001Search in Google Scholar

30. Editorial, FUTURE JET TECHNOLOGIES: 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

31. Editorial, FUTURE JET TECHNOLOGIES: Fleets of low-cost, stealth, jet-steered drones designed to fly ahead of fighter aircraft and bombers into congested regions. Int’l J. Turbo & Jet Engines, Jan 2013.Search in Google Scholar

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34. Gal-Or, B., “An Old-New European Debate on Thrust Vectoring and adverse effects of canards”, Polskiej Nauki, PRACE Instytutu Lotnictwa, Poland, 152, pp. 3-8, 1998.Search in Google Scholar

35. Aviation Week & Space Technology: “Israelis Flight Test Jet-Powered RPV Fitted With Thrust Vectoring Nozzles [JET-ENGINE-STEERED-(JES)], May 18, p. 21, 1987.Search in Google Scholar

36. Aviation Week & Space Technology: more on first 3-D-Vectored-stealth-RPV-prototype performing post-stall Maneuvers, (Figures 3, 4), May 30, 1987; FLIGHT INT’L, May 30, 1987; JANE’S ALL THE WORLD’S AIRCRAFT, 1987.Search in Google Scholar

37. Gal-Or, B., “Upgraded, Completely Vectored F-22”, USAF-AFOSR-EOARD, CONTRACT F61708-92-W, UNITED STATES AIR FORCE, Report: February 28, 1993.Search in Google Scholar

38. Gal-Or, B. with Lijun Qian and E. Kreindler, Minimum-time maneuvers of thrust-vectored aircraft; Journal of Guidance Control and Dynamics, Mar 1998.Search in Google Scholar

39. Gal-Or, Benjamin, Valery Sherbaum and Lichtsinder Michael, U.S.-PATENT No. 5,782,431, on “Civilizing Military Thrust Vectoring Flight Control”, [saving many lives and preventing much damage by simple, add-on, TV devices], It includes review on first proof-of-concept flight test funded by U.S. FAA during 1994-1995, April, 1998.Search in Google Scholar

40. Aviation Week & Space Technology: THRUST VECTOR CONTROL EYED FOR TRANSPORT, August 28, 1995.Search in Google Scholar

41. AEROSPACE AMERICA, “Civilizing Military Technology for safest civil Flight Control”, 1995.Search in Google Scholar

42. Mishra, R.K., J. Thomas, k. srinivasan, v. nandi,, r. bhatt; investigation of HP turbine blade failure in a military turbofan engine; Int’l J. Turbo & Jet Engines, 2014 Vol. 34 issue 1, 23-32, DOI: 10.1515/tjj-2015-0049.10.1515/tjj-2015-0049Search in Google Scholar

43. Gal-Or, B., The Fundamental Concepts of Vectored Propulsion, AIAA J. Propulsion and Power, 6, 747-757, 1990.10.2514/3.23281Search in Google Scholar

44. Gal-Or, B., Maximizing Post-Stall, Thrust-Vectoring Agility and Control Power, AIAA J. Aircraft, 29, 647-651, 1992.10.2514/3.46214Search in Google Scholar

45. Gal-Or, B., Thrust Vectoring: Theory, Laboratory, and Flight Tests, AIAA J. Propulsion & Power, 9, 51-58, 1993.10.2514/3.11484Search in Google Scholar

46. Gal-Or, B. with A. Rasputnis, Valery Sherbaum and Michael Lichtsinder, 1991-1999, various reports, patent, [39], and publications on JES-full-scale-tests with hot jet engines, [32 at 53, 76, 77, 109-113, 131, 132, 149], on JES–engine inlets calibrations, flight tests, computer simulations.Search in Google Scholar

47. Gal-Or, B., FUNDAMENTALS OF CATASTROPHIC FAILURE PREVENTION BY THRUST VECTORING. AIAA Journal of Aircraft, May 1995. Cf., A remotely piloted, reduced-scale TVC-Boeing 727 flight tested in May 1995 to demonstrate the potentials for low-weight, add-on JES-kits for catastrophic failure prevention (1996)”; Id. and Ref. 39-41.Search in Google Scholar

48. Gal-Or, B., Proposed flight testing standards for engine thrust vectoring to maximize kill ratio, post-stall agility and flight safety, Int’l J. Turbo & Jet Engines, Dec 1995. Gal-Or, B., Thrust-Vectoring of Converging-Diverging Nozzles, AIAA J. of Propulsion and Power, 16, 202-206, 2000.10.1515/TJJ.1995.12.4.252Search in Google Scholar

49. Gal-Or, B., Thrust-Vectoring of Converging-Diverging Nozzles, AIAA J. of Propulsion and Power, 16, 202-206, 2000.10.2514/2.5584Search in Google Scholar

50. Gal-Or, B. FUNDAMENTALS and SIMILARITY TRANSFORMATIONS OF VECTORED AIRCRAFT, AIAA. Journal of Aircraft, Jan 1994.10.2514/3.46472Search in Google Scholar

51. Mishra, R.K., S. K. Kumar, S. Chandel; Lean blow-out studies in a swirl stabilized annular gas turbine combustor; Effect of fuel particle size on the stability of swirl stabilized flame in gas turbine combustor, Int’l J. Turbo & Jet Engines, 2015, 32(2):117-141, Dec 2014; DOI: 10.1515/tjj-2014-0028; –0027Search in Google Scholar

52. Gal-Or, B., MATHEMATICAL PHENOMENOLOGY FOR THRUST VECTORING–INDUCED AGILITY COMPARISONS, Deficiencies vs. compromises regarding basic rules for maximization of jet-deflection rates are formulated. AIAA Journal of Aircraft, Mar 1993.10.2514/3.48273Search in Google Scholar

53. Gal-Or, B., THRUST VECTORING [JES] – THEORY, LABORATORY, and FLIGHT TESTS, AIAA Journal of Propulsion and Power, Jan 1993.10.2514/3.11484Search in Google Scholar

54. Gal-Or, B., “Novel, Post-Stall, Thrust-Vectored F-15 RPVs: Laboratory and Flight Tests” Funded since 1987 by USAF, (1) Canarded v. Canard-less, ROUNDED v. RECTANGULAR JES-EXHAUSTS to 1, 2 or 3 COLD-FAN-JET-ENGINES, 1/7-scaled-JES-F-15 flight-testing in abandoned airfield in ISRAEL, [32], (2) F-15-AIR-INLET-to-HOT-OPERATING-JET-ENGINE-MARBORE-II-full-scale-PERFORMANCE, [Id.], (3) SUB-SCALED-F-15-INLET-PERFORMANCE DURING POST-STALL HIGH AOA, 188-page-Report-I, 1987-1992 PROJECTS. PART I of 9 REPORTS ORIGINALLY CLASSIFIED.Search in Google Scholar

55. Gal-Or, B., “Tailless Vectored Fighters: Theory, Laboratory and Flight Tests”, USAF funding, WPAFB, Ohio, USA, AFOSR FY 1456-8905052, 196-page-Report-II, July 15, 1991.Search in Google Scholar

56. Gal-Or, B., “Tailless Vectored Fighters: Theory, Laboratory and Flight Tests”, USAF funding, 196-page-Report-III, July 15, 1991.Search in Google Scholar

57. Gal-Or, B., “Vectorable Inlets/Nozzles and Tailless Flying Models vs. Pilot’s Tolerances Affecting Maximum Post-Stall Vectoring Agility”; USAF funding, 238-page-Report-IV.Search in Google Scholar

58. Gal-Or, B., “Dynamic Scaling, Pilot v. G-Loads under post-stall Maneuvers with vectored fighters”, USAF Funded series of projects in Israel E. g., (i) San Antonio, BAFB, 1990, submitted to USAF Colonel J. Tedor team, Report-V.Search in Google Scholar

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63. Gal-Or, B., Agility Benefits of Integrated Aerodynamic & Thrust Vectoring Control, GD/Lockheed-Martin RFP Ref. TECH-RRJ-JK-0001, TIIT-TRDF 160-779, 1993-1995, Progress Report No. 2, February 10, 1995.Search in Google Scholar

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70. INDIA-RUSSIA-TREATY-VOIDED? (I), CF. Figure 9 and April 23, 2018 by Franz Stefa Gady at https://thediplomat.com/2018/04/india-pulls-out-of-joint-stealth-fighter-project-with-russia/, April 23, 2018, [71].Search in Google Scholar

71. INDIA-RUSSIA-TREATY-VOIDED? (II), CF. “India has reportedly withdrawn from a 11-year joint program to develop a 5th generation fighter jet with Russia”; “the Sukhoi/HAL Fifth Generation Fighter Aircraft (FGFA), also known in India as the Perspective Multi-role Fighter (PMF).”, [72].Search in Google Scholar

72. INDIA-RUSSIA-TREATY-VOIDED? (III), CF. “Neither the Indian nor Russian governments have so far publicly confirmed New Delhi’s decision”, [Id.]. “After evaluating the first PAK FA T-50 [Su-57] prototype (the Russian prototype of the PMF), the [IAF] wanted more than 40 changes addressing, among other things, perceived weaknesses in the plane’s engine, stealth, and weapon-carrying capabilities; http://www.pravdareport.com/russia/economics/15-07-2008/105795-unmanned-0/75, https://nationalinterest.org/blog/the-buzz/russia-india-had-plans-build-stealth-fighter-those-plans-are-25592Search in Google Scholar

73. HISTORY NOTE 1: “China’s J-10(B) fighter equipped with our JES “was built with Israeli assistance”; “Using this technology, the F-22 Raptor can angle its thrust up to 24 degrees up or down.” “Now China’s J-10 joins this elite club of super-maneuverable fighter jets.” Russian uses JES since mid 1990’s, [21–31]. https://www.youtube.com/watch?v=xApU00KdRLY;https://www.popularmechanics.com/military/a24742661/china’s-j-10-thrust-vector-control/?source=nl&utm_source=nl_pop&utm_medium=email&date=100118 and www.flightglobal.com/news/articles/j-10b-tvc-wows-zhuhai-crowds-with-surprise-performa-453352/;Search in Google Scholar

74. HISTORY NOTE 2: China published author’s Review of JES v. canards-debates by its Journal of Thermal Science, Mar 1998, [25, 33, 34], invites Keynote Lecture to Chinese Academy of Sciences, 3rd Int’l Conf. ISIAF, [65], repeated to its top designers at CHENGDU. On November 6, 2018, via JES-J-10B CHINA joins the JES-revolution. https://www.janes.com/article/76804/image-suggests-china-may-be-testing-thrust-vectoring-engine-on-j-10-fighter#;https://www.popularmechanics.com/military/aviation/a24680684/all-the-new-tech-from-chinas-big-airshow/Search in Google Scholar

75. HISTORY NOTE 3: Post PST-1987-1st JES-Flight-tests, [36, 37], Russia joins the JES revolution and a new GLOBAL-JES-RACE is established.Search in Google Scholar

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78. ARROW-3: “U.S. Missile Defense Director: ARROW-3 is more advanced than what we have ever attempted in the U.S. with our programs. … [with] greater flexibility and other aspects, such as propulsion systems.”https://defense-update.com/products/a/arrow3.html; https://nationalinterest.org/blog/buzz/meet-russias-s-500-can-it-kill-f-22-or-f-35-37072;Search in Google Scholar

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80. INF TREATY: Intermediate-Range Nuclear Forces Treaty was signed in Washington, D.C. on December 8, 1987. It eliminated all nuclear and conventional missiles and their launchers with ranges of 500–1,000 kilometers (short-range) and 1,000–5,500 km (intermediate-range). Russia claims it did not include GHST. https://www.express.co.uk/news/world/1065145/ww3-vladimir-putin-cuba-soviet-union-bases-cold-war-nuclear-donald-trump-spt/.Search in Google Scholar

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