A review of thrust-vectoring in support of a V/STOL non-moving mechanical propulsion system

[1] Trancossi M., Dumas A., Giuliani I., Bagi I., Ugello capace di deviare in modo dinamico e controllabile un getto sintetico senza parti meccaniche in movimento e suo sistema di controllo, Patent No. RE2011A000049, Italy, 2011. Search in Google Scholar

[2] Vucinic D., Hazarika B., Dinescu C., Visualization and PIV measurements of in-cylinder axisymmetric ows, in SAE Technical Papers, Automotive and Transportation Technology Congress and Exhibition, 2001. 10.4271/2001-01-3273Search in Google Scholar

[3] Vucinic D., Hazarika B., Integrated approach to computational and experimental ow visualization of a double annular conned jet, Journal of Visualization, vol. 4, no. 3, pp. 245–256, 2001. http://dx.doi.org/10.1007/BF0318258510.1007/BF03182585Search in Google Scholar

[4] Pascoa J., Xisto C., Goettlich E., Performance assessment limits in transonic 3D turbine stage blade rows using a mixing-plane approach, Journal of Mechanical Science and Technology, vol. 24, no. 10, pp. 2035–2042, 2010. http://dx.doi.org/10.1007/s12206-010-0713-910.1007/s12206-010-0713-9Search in Google Scholar

[5] Pascoa J., Mendes A., Gato L., A fast iterative inverse method for turbomachinery blade design, Mechanics Research Communications, vol. 36, no. 5, pp. 630–637, 2009. http://dx.doi.org/10.1016/j.mechrescom.2009.01.00810.1016/j.mechrescom.2009.01.008Search in Google Scholar

[6] Pascoa J., Mendes A., Gato L., Redesigning annular turbine blade rows using a viscous-inviscid inverse design method, in Proc. 53rd ASME Turbo Expo 2008, vol. 6 of A, pp. 2209–2217, 2008. Search in Google Scholar

[7] Pascoa J., Mendes A., Gato L., Turbine blade duty re-design by controlling lean and sweep using an innovative iterative inverse design method, in Proc. 51st ASME Turbo Expo, vol. 6, pp. 1249–1256, 2006. Search in Google Scholar

[8] Pascoa J, Mendes A., Gato L., Aerodynamic design of turbomachinery cascades using an enhanced time-marching nite volume method,” CMES-Computer Modeling in Engineering and Sciences, vol. 6, pp. 537–546, 2004. Search in Google Scholar

[9] Smith T., Bingham C., Stewart P., Allarton R. et al., Energy harvesting and power network architectures for the multibody advanced airship for transport high altitude cruiser-feeder airship concept, Journal of Aerospace Engineering, Part G of Proceedings of the Institution of Mechanical Engineers, vol. 227, pp. 586–598, 2013. http://dx.doi.org/10.1177/095441001246931910.1177/0954410012469319Search in Google Scholar

[10] Stewart P., Gladwin D., Parr M., Stewart J., Multiobjective evolutionary-fuzzy augmented flight control for an F16 aircraft,” Journal of Aerospace Engineering, Part G of Proceedings of the Institution of Mechanical Engineers, vol. 224, pp. 293–309, 2010. http://dx.doi.org/10.1243/09544100JAERO61010.1243/09544100JAERO610Search in Google Scholar

[11] Anderson S. B., Historical overview of V/STOL aircraft technology, Tech. Rep. TM-81280, NASA, 1981. Search in Google Scholar

[12] Ilieva G., Pascoa J., Dumas A., Trancossi M., A critical review of propulsion concepts for modern airships, Central European Journal of Engineering, vol. 2, no. 2, pp. 189–200, 2012. http://dx.doi.org/10.2478/s13531-011-0070-110.2478/s13531-011-0070-1Search in Google Scholar

[13] Flight, pp. 289, April 1932 Search in Google Scholar

[14] Thomason T., Bell-Boeing JVX tilt rotor program — flight test program, in AIAA Paper N 83-2726, American Institute of Aeronautics and Astronautics, 1983. 10.2514/6.1983-2726Search in Google Scholar

[15] Aviation international news, pp. 42, February 2012. Search in Google Scholar

[16] Flight international, pp. 1014, June 1962. Search in Google Scholar

[17] Aviation Week — Last Raptor Rolls Off Lockheed Martin Line, December 2011. Search in Google Scholar

[18] Dorr R., Rockwell/MBB X-31, World Air Power Journal, vol. 24, pp. 34–47, 1996. Search in Google Scholar

[19] Saeed B., Exploring the Aerodynamic Characteristics of a Blown Annular-Wing for V/STOL Aircraft. PhD thesis, Brunel University, 2010. Search in Google Scholar

[20] Saeed B., Gratton G., Mares C., A feasibility assessment of annular winged VTOL flight vehicles, The Aeronautical Journal, vol. 115, pp. 683–692, 2011. 10.1017/S0001924000006400Search in Google Scholar

[21] AGARD, V/STOL handling i-criteria and discussion, Tech. Rep. AGARD-R-577-70, Advisory Group for Aerospace Research & Development, 1970. Search in Google Scholar

[22] Moralez E., Merrick V., Schroeder J., Simulation evaluation of an advanced control concept for a V/STOL aircraft, Journal of Guidance Control and Dynamics, vol. 12, pp. 334–341, 1989. http://dx.doi.org/10.2514/3.2041310.2514/3.20413Search in Google Scholar

[23] Naldi R., Marconi L., Optimal transition maneuvers for a class of V/STOL aircraft, Automatica, vol. 47, pp. 870–879, 2011. http://dx.doi.org/10.1016/j.automatica.2011.01.02710.1016/j.automatica.2011.01.027Search in Google Scholar

[24] Strykowski P., Krothapalli A., An experimental investigation of active control of thrust vectoring nozzle flow fields, tech. rep., The University of Minnesota, 1993. Search in Google Scholar

[25] Mason M., Crowther W., Fluidic thrust vectoring of low observable aircraft, in CEAS Aerospace Aerodynamic Research Conference, pp. 1–7, 2002. Search in Google Scholar

[26] Wing D., Static investigation of two fluidic thrustvectoring concepts on a two-dimensional convergentdivergent nozzle, Tech. Rep. TM-4574, NASA Langley Research Center, 1994. Search in Google Scholar

[27] Porzio A., Characteristics of a Confined Jet Thrust Vector Control Nozzle. PhD thesis, Air Force Institute of Technology (USA), 1984. Search in Google Scholar

[28] Trancossi M., Dumas A., A.C.H.E.O.N.: Aerial Coanda High Efficiency Orienting-jet Nozzle, in SAE Aerotech 2011, no. SAE Technical Paper 2011-01-2737, 2011. 10.4271/2011-01-2737Search in Google Scholar

[29] Trancossi M., An overview of scientific and technical literature on coanda effect applied to nozzles, in SAE Aerotech 2011, no. SAE Technical Paper 2011-01-2591, 2011. 10.4271/2011-01-2591Search in Google Scholar

[30] Trancossi M., Dumas A., Coanda synthetic jet deflection apparatus and control, in SAE Aerotech 2011, no. SAE Technical Paper 2011-01-2590, 2011. 10.4271/2011-01-2590Search in Google Scholar

[31] Sagha F., Banazadeh A., Coanda surface geometry optimization for multi-directional co-flow fluidic thrust vectoring, in Proceedings of ASME Turbo Expo 2009: Power for Land, Sea and Air, no. GT2009-59715, 2009. 10.1115/GT2009-59715Search in Google Scholar

[32] AGARD, Special course on V/STOL aerodynamics, Tech. Rep. AGARD-R-710, Advisory Group for Aerospace Research & Development, 1984. Search in Google Scholar

[33] Mabey K., Smith B., Whichard G., McKechnie T., Coanda-assisted spray manipulation collar for a commercial plasma spray gun,” Journal of Thermal Spray Technology, vol. 20, no. 4, pp. 782–790, 2011. http://dx.doi.org/10.1007/s11666-011-9640-210.1007/s11666-011-9640-2Search in Google Scholar

[34] Kim H., Rajesh G., Setoguchi T., Matsuo S., Optimization study of a coanda ejector, Journal of Thermal Science, vol. 15, no. 4, pp. 331–336, 2006. http://dx.doi.org/10.1007/s11630-006-0331-210.1007/s11630-006-0331-2Search in Google Scholar

[35] Vanierschot M., Persoons T., Van den Bulck E., A new method for annular jet control based on cross-flow injection, Physics of Fluids, vol. 21, pp. 025103-1–025103-9, 2009. http://dx.doi.org/10.1063/1.303734310.1063/1.3037343Search in Google Scholar

[36] Patankar U., Sridhar K., Three-dimensional curved wall jets, Journal of Basic Engineering, vol. 94, no. 2, pp. 339–344, 1972. http://dx.doi.org/10.1115/1.342541410.1115/1.3425414Search in Google Scholar

[37] Bevilaqua P., Lee J., Development of a nozzle to improve the turning of supersonic Coanda jets, Tech. Rep. AFWAL-TR-80-3027, Air Force Wright Aeronautical Laboratories (Wright-Patterson Air Force Base), 1980. 10.21236/ADA087709Search in Google Scholar

[38] Favre-Marinet M., Binder G., Hac T., Generation of oscillating jets, Journal of Fluids Engineering, vol. 103, pp. 609–614, 1981. http://dx.doi.org/10.1115/1.324178010.1115/1.3241780Search in Google Scholar

[39] Allen D., Axisymmetric Coanda-Assisted Vectoring. PhD thesis, Utah State University, 2008. 10.1007/s00348-008-0536-ySearch in Google Scholar

[40] Neuendorf R., Lourenco L., Wygnanski I., On large stream-wise structures in a wall jet owing over a circular cylinder, Physics of Fluids, vol. 16, pp. 2158–2169, 2004. http://dx.doi.org/10.1063/1.170353110.1063/1.1703531Search in Google Scholar

[41] Chiang T., Sheu T., Wang S., Side wall effects on the structure of laminar flow over a plane-symmetric sudden expansion, Computers & Fluids, vol. 29, pp. 467–492, 2000. http://dx.doi.org/10.1016/S0045-7930(99)00018-310.1016/S0045-7930(99)00018-3Search in Google Scholar

[42] Nishino T., Hahn S., Shari K, Large-eddy simulations of a turbulent coanda jet on a circulation control airfoil, Physics of Fluids, vol. 22, pp. 125105-1–125105-15, 2010. http://dx.doi.org/10.1063/1.352675710.1063/1.3526757Search in Google Scholar

[43] Dumitrache A., Frunzulica F., Ionescu T., Nonlinearity, Bifurcation and Chaos — Theory and Applications, ch. Mathematical Modelling and Numerical Investigations on the Coanda Effect, pp. 101–132. INTECH, 2012. 10.5772/50403Search in Google Scholar

[44] Payne P., Curved jet ows (vol i), Tech. Rep. USAAML Technical Report 65-20, US Army Aviation Material Laboratories, Fort Eustis, Virginia, USA, 1965. Search in Google Scholar

[45] AGARD, Effects of streamline curvature on turbulent flow, Tech. Rep. AGARDograph N169, Advisory Group for Aerospace Research and Development, 1973. Search in Google Scholar

[46] Kobayashi R., Fujisawa N., Curvature effects on twodimensional turbulent wall jets, Ingenieur-Archiv, vol. 53, pp. 409–417, 1983. http://dx.doi.org/10.1007/BF0053320210.1007/BF00533202Search in Google Scholar

[47] Englar R., Experimental investigation of the high velocity coanda wall jet applied to bluff trailing edge circulation control airfoils, tech. rep., Naval Ship Research and Development Center (USA), 1975. Search in Google Scholar

[48] Bevilaqua P., Lifting surface theory for thrust augmenting ejectors,” tech. rep., Rockwell International Columbus OH (USA), 1982. Search in Google Scholar

[49] Azim M., Sadrul-Islam M., Plane mixing layers from parallel of two streams, Experiments in Fluids, vol. 34, pp. 220–226, 2003. http://dx.doi.org/10.1007/s00348-002-0549-x10.1007/s00348-002-0549-xSearch in Google Scholar

[50] Matsuo S., Setoguchi T., Kudo T, Study on the characteristics of supersonic Coanda jet, Journal of Thermal Science, vol. 7, no. 3, pp. 165–175, 1998. http://dx.doi.org/10.1007/s11630-998-0012-210.1007/s11630-998-0012-2Search in Google Scholar

[51] Alvi F., Strykowski P., Krothapalli A., Forliti D., Vectoring thrust in multiaxes using confined shear layers, Journal of Fluids Engineering, vol. 122, no. 1, pp. 3–13, 2000. http://dx.doi.org/10.1115/1.48322010.1115/1.483220Search in Google Scholar

[52] Cattafesta L., Sheplak M., Actuators for active flow control, Annual Review of Fluid Mechanics, vol. 43, p. 247272, 2011. http://dx.doi.org/10.1146/annurev-fluid-122109-16063410.1146/annurev-fluid-122109-160634Search in Google Scholar

[53] Panzarella P., The use of a Coanda nozzle with parallel secondary injection for the thrust vectoring of a two-dimensional compressible fluid, Master’s thesis, Air Force Institute of Technology (USA), 1965. Search in Google Scholar

[54] Hanson R., Lavoie P., Naguib A., Morrison J., Transient growth instability cancellation by a plasma actuator array, Experiments in Fluids, vol. 49, pp. 1339–1348, 2010. http://dx.doi.org/10.1007/s00348-010-0877-110.1007/s00348-010-0877-1Search in Google Scholar

[55] Corke T., Post M., Orlov D., Sdbd plasma enhanced aerodynamics: concepts, optimization and applications, Progress in Aerospace Sciences, vol. 43, p. 192217, 2007. http://dx.doi.org/10.1016/j.paerosci.2007.06.00110.1016/j.paerosci.2007.06.001Search in Google Scholar

[56] Sosaa R., Artana G., Steady control of laminar separation over airfoils with plasma sheet actuators, Journal of Electrostatics, vol. 64, pp. 604–610, 2006. http://dx.doi.org/10.1016/j.elstat.2005.10.02910.1016/j.elstat.2005.10.029Search in Google Scholar

[57] Orlov D. M., Modeling and simulation of single dielectric barrier discharge plasma actuators. PhD thesis, University of Notre Dame, 2006. Search in Google Scholar

[58] Orlov D., Apker T., He, C. Othman H., et al., Modeling and experiment of leading edge separation control using sdbd plasma actuators, in AIAA 45th Aerospace Sciences Meeting, 2007. 10.2514/6.2007-877Search in Google Scholar

[59] Lemire S., Vo H., Reduction of fan and compressor wake defect using plasma actuation for tonal noise reduction, Journal of Turbomachinery, vol. 133, pp. 133–143, 2011. http://dx.doi.org/10.1115/1.400054010.1115/1.4000540Search in Google Scholar

[60] Grundmann S., Frey M., Tropea C., Unmanned aerial vehicle (UAV) with plasma actuators for separation control, in 47th AIAA Aerospace Sciences Meeting, 2009. 10.2514/6.2009-698Search in Google Scholar

[61] Thomas F., Kozlov A., Corke T., Plasma actuators for cylinder flow control and noise reduction, AIAA Journal, vol. 46, pp. 1921–1931, 2008. http://dx.doi.org/10.2514/1.2782110.2514/1.27821Search in Google Scholar

[62] Whalley R., Turbulent Boundary-Layer Control with DBD Plasma Actuators Using Spanwise Travelling-Wave Technique. PhD thesis, University of Nottingham, 2011. 10.2514/6.2010-4840Search in Google Scholar

[63] Tornabene F., Ceruti A., Mixed static and dynamic optimization of four-parameter functionally graded completely doubly curved and degenerate shells and panels using GDQ method, Mathematical Problems in Engineering, vol. 1, p. 33, 2013. 10.1155/2013/867079Search in Google Scholar

[64] Liverani A., Ceruti A., Caligiana G., Tablet-based 3D sketching and curve reverse modelling, Inter-national Journal of Computer Aided Engineering and Technology, vol. 5, no. 2/3, pp. 188–215, 2013. http://dx.doi.org/10.1504/IJCAET.2013.05293610.1504/IJCAET.2013.052936Search in Google Scholar