Effects of Detailed Aircraft Geometry on Wake Vortex Dynamics During Landing
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[1] Nikola Tchipev,et al. Wind Impact on Single Vortices and Counterrotating Vortex Pairs in Ground Proximity , 2016 .
[2] C. Meneveau,et al. A Lagrangian dynamic subgrid-scale model of turbulence , 1994, Journal of Fluid Mechanics.
[3] Jürgen Quest,et al. Flow Field Measurements by PIV at High Reynolds Numbers , 2013 .
[4] Takashi Misaka,et al. Large-Eddy Simulation of Aircraft Wake Evolution from Roll-Up Until Vortex Decay , 2015 .
[5] Eike Stumpf,et al. Study of Four-Vortex Aircraft Wakes and Layout of Corresponding Aircraft Configurations , 2005 .
[6] Norbert Kroll,et al. MEGADESIGN and MegaOpt - German Initiatives for Aerodynamic Simulation and Optimization in Aircraft Design , 2009 .
[7] François Garnier,et al. Analysis of wake vortex decay mechanisms in the atmosphere , 2003 .
[8] Niko Bier,et al. Maximum lift predictions of a realistic commercial aircraft in landing configuration , 2012 .
[9] G. D. J. Constant,et al. Coherent Laser Radar and the Problem of Aircraft Wake Vortices , 1994 .
[10] C. L. Rumsey,et al. Summary of the First AIAA CFD High Lift Prediction Workshop (invited) , 2011 .
[11] Fred H. Proctor,et al. Wake Vortex Transport and Decay in Ground Effect: Vortex Linking with the Ground , 2000 .
[13] Stefan Keye,et al. Stall Maneuver Simulation of an elastic Transport Aircraft based on Flight Test Data , 2015 .
[14] Sheila E. Widnall,et al. An analytic solution for two- and three-dimensional wings in ground effect , 1970, Journal of Fluid Mechanics.
[15] Igor N. Smalikho,et al. Characterization of Aircraft Wake Vortices by 2-μm Pulsed Doppler Lidar , 2004 .
[16] Egbert Torenbeek. The general arrangement , 1982 .
[17] S. Rahm,et al. Method of radial velocities for the estimation of aircraft wake vortex parameters from data measured by coherent Doppler lidar. , 2015, Optics express.
[19] Takashi Misaka,et al. Vortex bursting and tracer transport of a counter-rotating vortex pair , 2012 .
[20] P. Spalart. A One-Equation Turbulence Model for Aerodynamic Flows , 1992 .
[21] Ralf Rudnik,et al. HINVA - High Lift INflight VAlidation - Project Overview and Status , 2012 .
[22] Christian Breitsamter,et al. Wake vortex characteristics of transport aircraft , 2011 .
[23] Takashi Misaka,et al. Hybrid Simulation of Wake-Vortex Evolution During Landing on Flat Terrain and with Plate Line , 2014 .
[24] Thomas Gerz,et al. Commercial aircraft wake vortices , 2002 .
[25] I. N. Smalikho,et al. Lidar investigations of the effects of wind and atmospheric turbulence on an aircraft wake vortex , 2010 .
[26] Frank Holzäpfel,et al. Probabilistic Two-Phase Wake Vortex Decay and Transport Model , 2003 .
[27] D. Fischenberg. Ground Effect Modeling Using a Hybrid Approach of Inverse Simulation and System Identification , 1999 .
[28] Kozo Fujii,et al. Unified zonal method based on the fortified solution algorithm , 1992 .
[29] R. V. Jategaonkar,et al. Flight Vehicle System Identification: A Time-Domain Methodology, Second Edition , 2015 .
[30] Michael Manhart,et al. A zonal grid algorithm for DNS of turbulent boundary layers , 2004 .
[31] Takashi Misaka,et al. Aircraft Wake-Vortex Decay in Ground Proximity—Physical Mechanisms and Artificial Enhancement , 2013 .
[32] Michael Manhart,et al. Compact fourth-order finite volume method for numerical solutions of Navier-Stokes equations on staggered grids , 2010, J. Comput. Phys..
[33] Arpiruk Hokpunna,et al. Compact Fourth-order scheme for Numerical Simulations of Navier-Stokes Equations , 2009 .
[34] Philippe R. Spalart,et al. AIRPLANE TRAILING VORTICES , 1998 .