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

The advantages associated to Vertical Short-Take-Off and Landing (V/STOL) have been demonstrated since the early days of aviation, with the initial technolology being based on airships and later on helicopters and planes. Its operational advantages are enormous, being it in the field of military, humanitarian and rescue operations, or even in general aviation. Helicopters have limits in their maximum horizontal speed and classic V/STOL airplanes have problems associated with their large weight, due to the implementation of moving elements, when based on tilting rotors or turbojet vector mechanical oriented nozzles. A new alternative is proposed within the European Union Project ACHEON (Aerial Coanda High Efficiency Orienting-jet Nozzle). The project introduces a novel scheme to orient the jet that is free of moving elements. This is based on a Coanda effect nozzle supported in two fluid streams, also incorporating boundary layer plasma actuators to achieve larger deflection angles. Herein we introduce a state-of-the-art review of the concepts that have been proposed in the framework of jet orienting propulsion systems. This review allows to demonstrate the advantages of the new concept in comparison to competing technologies in use at present day, or of competing technologies under development worldwide.

[1]  F. Frunzulică,et al.  Mathematical Modelling and Numerical Investigations on the Coanda Effect , 2012 .

[2]  Cameron Tropea,et al.  Unmanned Aerial Vehicle (UAV) with Plasma Actuators for Separation Control , 2009 .

[3]  Paul Bevilaqua.  Lifting Surface Theory for Thrust-Augmenting Ejectors , 1978 .

[4]  T. Corke,et al.  SDBD plasma enhanced aerodynamics: concepts, optimization and applications , 2007 .

[5]  T. Thomason.  Bell-Boeing JVX tilt rotor program - Flight test program , 1983 .

[6]  David J. Wing,et al.  Static investigation of two fluidic thrust-vectoring concepts on a two-dimensional convergent-divergent nozzle , 1994 .

[7]  P. Bevilaqua.  A lifting surface theory for thrust augmenting ejectors , 1977 .

[8]  Jose´ C. Pa´scoa,et al.  Turbine Blade Duty Re-Design by Controlling Lean and Sweep Using an Innovative Iterative Inverse Design Method , 2006 .

[9]  Seth B. Anderson,et al.  Historical Overview of V/STOL Aircraft Technology , 1997 .

[10]  Barton L Smith,et al.  Axisymmetric Coanda-assisted vectoring , 2008 .

[11]  Lorenzo Marconi,et al.  Optimal transition maneuvers for a class of V/STOL aircraft , 2009, Autom..

[12]  Paul Stewart,et al.  Multi-objective evolutionary—fuzzy augmented flight control for an F16 aircraft , 2010 .

[13]  Antonio Dumas,et al.  Coanda Synthetic Jet Deflection Apparatus and Control , 2011 .

[14]  D. Vucinic,et al.  Visualization and PIV Measurements of In-Cylinder Axisymmetric Flows , 2001 .

[15]  Toshiaki Setoguchi,et al.  Optimization study of a Coanda ejector , 2006 .

[16]  T. Persoons,et al.  A new method for annular jet control based on cross-flow injection , 2009 .

[17]  Chris Bingham,et al.  Energy harvesting and power network architectures for the multibody advanced airship for transport high altitude cruiser–feeder airship concept , 2013 .

[18]  Huu Duc Vo,et al.  Reduction of Fan and Compressor Wake Defect Using Plasma Actuation for Tonal Noise Reduction , 2008 .

[19]  U. M. Patankar,et al.  Three-Dimensional Curved Wall Jets , 1972 .

[20]  Antonio Dumas,et al.  A critical review of propulsion concepts for modern airships , 2012 .

[21]  John D. Lee,et al.  Development of a Nozzle to Improve the Turning of Supersonic Coanda Jets , 1980 .

[22]  Emil Göttlich,et al.  Performance assessment limits in transonic 3D turbine stage blade rows using a mixing-plane approach , 2010 .

[23]  T. Nishino,et al.  Large-eddy simulations of a turbulent Coanda jet on a circulation control airfoil , 2010 .

[24]  Ahmed Naguib,et al.  Transient growth instability cancelation by a plasma actuator array , 2010 .

[25]  M. Azim,et al.  Plane mixing layers from parallel and non-parallel merging of two streams , 2003 .

[26]  Farrukh S. Alvi,et al.  Vectoring thrust in multiaxes using confined shear layers , 2000 .

[27]  Guy Gratton,et al.  A feasibility assessment of annular winged VTOL flight vehicles , 2011 .

[28]  Guillermo Artana,et al.  Steady control of laminar separation over airfoils with plasma sheet actuators , 2006 .

[29]  Michele Trancossi,et al.  An Overview of Scientific and Technical Literature on Coanda Effect Applied to Nozzles , 2011 .

[30]  N. Fujisawa,et al.  Curvature effects on two-dimensional turbulent wall jets , 1983 .

[31]  M. Favre-Marinet,et al.  Generation of Oscillating Jets , 1981 .

[32]  T. Sheu,et al.  Side wall effects on the structure of laminar flow over a plane-symmetric sudden expansion , 2000 .

[33]  William Crowther,et al.  Fluidic thrust vectoring for low observable aircraft , 2002 .

[34]  S. Matsuo,et al.  Study on the characteristics of supersonic Coanda jet , 1998 .

[35]  Thomas Corke,et al.  Plasma Actuators for Cylinder Flow Control and Noise Reduction , 2008 .

[36]  V. K. Merrick,et al.  Simulation evaluation of an advanced control concept for a V/STOL aircraft , 1989 .

[37]  P. Bradshaw.  Effects of Streamline Curvature on Turbulent Flow. , 1973 .

[38]  Dmitriy M. Orlov,et al.  Modelling and simulation of single dielectric barrier discharge plasma actuators , 2006 .

[39]  D. Vucinic,et al.  Integrated approach to computational and experimental flow visualization of a double annular confined jet , 2001 .

[40]  Luís M.C. Gato,et al.  A fast iterative inverse method for turbomachinery blade design , 2009 .

[41]  Richard David Whalley,et al.  Turbulent boundary-layer control with DBD plasma actuators using spanwise travelling-wave technique , 2011 .

[42]  Thomas Apker,et al.  Modeling and Experiment of Leading Edge Separation Control Using SDBD Plasma Actuators , 2007 .

[43]  L. Lourenço,et al.  On large streamwise structures in a wall jet flowing over a circular cylinder , 2004 .

[44]  A. Ceruti,et al.  Mixed Static and Dynamic Optimization of Four-Parameter Functionally Graded Completely Doubly Curved and Degenerate Shells and Panels Using GDQ Method , 2013 .

[45]  Antonio Dumas,et al.  A.C.H.E.O.N.: Aerial Coanda High Efficiency Orienting-jet Nozzle , 2011 .

[46]  Louis N. Cattafesta,et al.  Actuators for Active Flow Control , 2011 .

[47]  Robert J. Englar,et al.  Experimental Investigation of the High Velocity Coanda Wall Jet Applied to Bluff Trailing Edge Circulation Control Airfoils , 1975 .

[48]  Alessandro Ceruti,et al.  Tablet-based 3D sketching and curve reverse modelling , 2013, Int. J. Comput. Aided Eng. Technol..

[49]  A. Krothapalli,et al.  An experimental investigation of active control of thrust vectoring nozzle flow fields , 1994 .

[50]  Luís M.C. Gato,et al.  Aerodynamic Design of Turbomachinery Cascades Using an Enhanced Time-Marching Finite Volume Method , 2004 .

[51]  Luís M.C. Gato,et al.  Redesigning Annular Turbine Blade Rows Using a Viscous-Inviscid Inverse Design Method , 2008 .

[52]  Burhan Saeed,et al.  Exploring the aerodynamic characteristics of a blown-annular wing for V/STOL aircraft , 2010 .

[53]  Afshin Banazadeh,et al.  Coanda Surface Geometry Optimization for Multi-Directional Co-Flow Fluidic Thrust Vectoring , 2009 .