Aerodynamic Installation Effects of an Over-the-Wing Propeller on a High-Lift Configuration

Preliminary design studies indicate that a cruise-efficient short takeoff and landing aircraft has enhanced takeoff performance at competitive direct operating costs when using high-speed propellers in combination with internally blown flaps. The original tractor configuration is compared to an over-the-wing propeller, which allows for noise shielding. An additional geometry with partially embedded rotor similar to a channel wing is considered to increase the beneficial interaction. This paper shows the aerodynamic integration effects with a focus on climb performance and provides an assessment of the three aforementioned configurations for a simplified wing segment at takeoff conditions. Steady Reynolds-averaged Navier–Stokes simulations have been conducted using an actuator disk model and were evaluated based on the overall design. Interacting with the blown flap, the conventional tractor propeller induces large lift and drag increments due to the vectored sliptream. Although this effect is much smaller...

[1]  Jochen Wild,et al.  Large scale separation flow control experiments within the German Flow Control Network , 2009 .

[2]  Cord-Christian Rossow,et al.  Numerical simulation of engine/airframe integration for high-bypass engines , 2002 .

[3]  Carsten Lenfers,et al.  Propeller Design for a future QESTOL Aircraft in the BNF Project , 2012 .

[4]  Jerome Pasamanick Langley full-scale-tunnel tests of the Custer Channel Wing airplane , 1953 .

[5]  Peter Horst,et al.  Multidisciplinary Integrated Preliminary Design Applied to Unconventional Aircraft Configurations , 2008 .

[6]  P. Spalart,et al.  Turbulence Modeling in Rotating and Curved Channels: Assessing the Spalart-Shur Correction , 2000 .

[7]  M. G. Mayo,et al.  Prop-fan data support study , 1978 .

[8]  Ilan Kroo,et al.  Propeller^Wing Integration for Minimum Induced Loss , 1986 .

[9]  Osama A. Kandil,et al.  Aerodynamic Investigations of an Advanced Over-the-Wing Nacelle Transport Aircraft Configuration , 2007 .

[10]  John S. Sullivan,et al.  Aerodynamic interaction between propellers and wings , 1989 .

[11]  Edward F. Blick,et al.  Power-on channel wing aerodynamics , 1971 .

[12]  H. Hoheisel Aerodynamic aspects of engine-aircraft integration of transport aircraft , 1997 .

[13]  Robert J. Englar,et al.  Development of Pneumatic Over-the-Wing Powered-Lift Technolgy. Part I: Aero/Propulsive , 2009 .

[14]  F. Moens,et al.  Numerical simulation of the propeller/wing interactions for transport aircraft , 2001 .

[15]  Peter Horst,et al.  Improved Representation of High-Lift Devices for a Multidisciplinary Conceptual Aircraft Design Process , 2009 .

[16]  Robert J. Englar,et al.  PNEUMATIC CHANNEL WING POWERED-LIFT ADVANCED SUPER- STOL AIRCRAFT , 2002 .

[17]  E. R. White,et al.  Exploratory low-speed wind-tunnel investigation of advanced commuter configurations including an over-the-wing propeller design , 1983 .

[18]  P. Spalart A One-Equation Turbulence Model for Aerodynamic Flows , 1992 .