Rudimentary Landing Gear Results at the 2012 BANC-II Airframe Noise Workshop

The results of large-eddy and similar simulations and acoustic propagation calculations provided by six participants for the Rudimentary Landing Gear (RLG) category of the 2012 BANC-II workshop are analyzed and compared with experimental results. The general conclusion is that industrial accuracy remains elusive, and very significant differences exist between methods, so that the field needs more maturity, in addition to computing power. We present both blind comparisons from the workshop, and revised results the participants were invited to provide after having access to the experimental data. We recall that BANC-I and other comparisons indicate good code-to-code and experimental agreement for time-averaged pressures, but not so much for unsteady pressures and forces. Possibly as a result of these differences, the agreement for radiated noise is quite poor in the blind test, with typical differences of over 5 dB for the SPL and for the spectra over the dominant frequency range, and reaching 10 dB towards both ends of the spectra. The collection of numerical results brackets the experimental result. Some differences arise from misunderstandings, which were not corrected. The post-workshop results are much closer to experiment, with differences reduced to about 3 dB for SPL, and for spectra up to a Strouhal number of 15. This is not up to industrial needs, but is very encouraging and close to the accuracy achieved for jet noise. The results are sensitive to the use of solid or permeable surfaces in the Ffowcs Williams-Hawkings (FW-H) equation, and to numerous simulation details such as upwind-biased differencing.

[1]  Hudong Chen,et al.  Realization of Fluid Boundary Conditions via Discrete Boltzmann Dynamics , 1998 .

[2]  Philippe R. Spalart,et al.  On the precise implications of acoustic analogies for aerodynamic noise at low Mach numbers , 2013 .

[3]  Philippe R. Spalart,et al.  Sensitivity of Landing-Gear Noise Predictions by Large-Eddy Simulation to Numerics and Resolution , 2012 .

[4]  S. Noelting,et al.  Flow and noise predictions for the tandem cylinder aeroacoustic benchmarka) , 2012 .

[5]  Ulf Michel,et al.  Ffowcs Williams & Hawkings Formulation for the Convective Wave Equation and Permeable Data Surface , 2010 .

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

[7]  Matthaeus,et al.  Recovery of the Navier-Stokes equations using a lattice-gas Boltzmann method. , 1992, Physical review. A, Atomic, molecular, and optical physics.

[8]  Laurent Sanders,et al.  LAGOON: New Mach Landing Gear Noise Computation and further analysis of the CAA process , 2012 .

[9]  Philippe R. Spalart,et al.  Initial noise predictions for rudimentary landing gear , 2011 .

[10]  Philippe R. Spalart,et al.  Analysis of Experimental and Numerical Studies of the Rudimentary Landing Gear , 2011 .

[11]  Fei Liu,et al.  A Comparative Study of a 1/4-Scale Gulfstream G550 Aircraft Nose Gear Model , 2009 .

[12]  N. Curle The influence of solid boundaries upon aerodynamic sound , 1955, Proceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences.

[13]  P. Spalart,et al.  A hybrid RANS-LES approach with delayed-DES and wall-modelled LES capabilities , 2008 .

[14]  P. Spalart,et al.  A New Version of Detached-eddy Simulation, Resistant to Ambiguous Grid Densities , 2006 .

[15]  S. Orszag,et al.  Expanded analogy between Boltzmann kinetic theory of fluids and turbulence , 2004, Journal of Fluid Mechanics.

[16]  D. Casalino An advanced time approach for acoustic analogy predictions , 2003 .

[17]  S. Orszag,et al.  Renormalization group analysis of turbulence. I. Basic theory , 1986 .

[18]  Mortaza Mani,et al.  Grid Sensitivity of the Rudimentary Landing Gear Using Unstructured Finite Volume Methods , 2012 .

[19]  P. Spalart,et al.  Physical and Numerical Upgrades in the Detached-Eddy Simulation of Complex Turbulent Flows , 2002 .

[20]  F. Thiele,et al.  Detached-Eddy Simulation of Landing-Gear Noise , 2013 .

[21]  Philippe R. Spalart,et al.  Variants of the Ffowcs Williams - Hawkings Equation and Their Coupling with Simulations of Hot Jets , 2009 .

[22]  P. Spalart,et al.  Noise Prediction for Increasingly Complex Jets. Part I: Methods and Tests , 2005 .

[23]  R. K. Amiet Refraction of sound by a shear layer , 1977 .

[24]  Florian R. Menter,et al.  Rudimentary Landing Gear Noise Predictions Using Scale-Resolving Simulations , 2013 .

[25]  N. Karthikeyan,et al.  Experimental Studies on a Rudimentary Four Wheel Landing Gear , 2011 .

[26]  Fei Liu,et al.  An Experimental Study of the Rudimentary Landing Gear , 2013 .

[27]  Luc Mongeau,et al.  An acoustic analogy formulation for moving sources in uniformly moving media , 2011, Proceedings of the Royal Society A: Mathematical, Physical and Engineering Sciences.

[28]  Yukio Kaneda,et al.  Thin Shear Layers in High Reynolds Number Turbulence—DNS Results , 2013 .

[29]  Taku Nagata,et al.  Aeroacoustic Analysis of the Rudimentary Landing Gear Using Octree Unstructured Grid with Boundary-fitted Layer , 2012 .

[30]  Taku Nagata,et al.  Validation of new CFD tool using Non-orthogonal Octree with Boundary-fitted Layer Unstructured Grid , 2012 .

[31]  P. D. Francescantonio A NEW BOUNDARY INTEGRAL FORMULATION FOR THE PREDICTION OF SOUND RADIATION , 1997 .

[32]  R Spalart Philippe,et al.  Young-Person''s Guide to Detached-Eddy Simulation Grids , 2001 .