Validation of the Flow Topology Around Several Airdrop Cargo Configurations at Static Conditions

A numerical study was carried out to assess the interference effects between the wake of a transport aircraft and several generic cargo bodies during the early stage of an airdrop scenario. Based on experimental data and preceding numerical simulations distinct positions of the trajectory being subject to strong interference effects were stati- cally reproduced. The flow field around the bodies was experimentally investigated using stereoscopic Particle Image Velocimetry and compared to steady and unsteady Reynolds- averaged Navier-Stokes (RANS) computations. The latter were carried out using the unstructured DLR TAU code. The primary focus is to assess the suitability, accuracy and the limitations of RANS methods in such challenging flow conditions. Therefore, the influence of several turbulence models was investigated and compared to experimental field velocity data. Although deviations in the wake of the bodies were observed, the qualitative agreement between the steady simulations and experiment was very good. Quantitatively, however, the steady approach leaves room for further improvements. The gap to the experimental data could partially be reduced in applying unsteady RANS methods.

[1]  Z. Lei Effect of RANS Turbulence Models on Computation of Vortical Flow over Wing-Body Configuration , 2005 .

[2]  T. Gerhold,et al.  Calculation of Complex Three-Dimensional Configurations Employing the DLR-tau-Code , 1997 .

[3]  Andreas Schröder,et al.  Coherent wake structures for transport aircraft at cargo airdrop configurations including parachutes , 2013 .

[4]  Niko Schade,et al.  Simulation of Trajectories of Cuboid Cargos Released from a Generic Transport Aircraft , 2011 .

[5]  Sven Geisbauer,et al.  Experimental and Numerical Investigation of the Flow Topology During Airdrop Operations , 2011 .

[6]  Bernhard Eisfeld Numerical Simulation of Aerodynamic Problems with the SSG/LRR-ω Reynolds Stress Turbulence Model Using the Unstructured TAU Code , 2007 .

[7]  David W. Roberts,et al.  Separation Flight Tests of a Small Unmanned Air Vehicle from a C-130 Transport Aircraft , 2005 .

[8]  Kenneth J. Desabrais,et al.  Aerodynamic Forces on an Airdrop Platform , 2005 .

[9]  Thomas Gerhold,et al.  Overview of the Hybrid RANS Code TAU , 2005 .

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

[11]  P. Spalart,et al.  On the sensitization of turbulence models to rotation and curvature , 1997 .

[12]  Andreas Bergmann,et al.  Capabilities of Deployment Tests at DNW-NWB , 2006 .

[13]  A. Bergmann Modern Wind Tunnel Techniques for Unsteady Testing – Development of Dynamic Test Rigs , 2009 .

[14]  Sven Geisbauer Numerical Spoiler Wake Investigations at the Borders of the Flight Envelope , 2011 .

[15]  Norbert Kroll,et al.  MEGAFLOW - A Numerical Flow Simulation Tool For Transport Aircraft Design , 2002 .

[16]  Kenneth Desabrais The Motion and Aerodynamics of an Airdrop Platform , 2004 .

[17]  Sven Geisbauer,et al.  Approximated Steady Aerodynamic Coefficients for Two Cuboids and a Hemispherical Shell Used in Airdrop Simulation , 2013 .

[18]  Olaf Brodersen,et al.  DLR Results from the Fourth AIAA CFD Drag Prediction Workshop , 2010 .

[19]  A. Jameson,et al.  Numerical solution of the Euler equations by finite volume methods using Runge Kutta time stepping schemes , 1981 .

[20]  Thomas Jann,et al.  Coupled Simulation of Cargo Airdrop from a Generic Military Transport Aircraft , 2011 .

[21]  Frank Thiele,et al.  MEGAFLOW - A Numerical Flow Simulation System , 1998 .

[22]  Jean Potvin,et al.  Simulating the Flows About Cargo Containers Used During Parachute Airdrop Operations , 2011 .

[23]  Andreas Bergmann,et al.  The Aeroacoustic Wind Tunnel DNW-NWB , 2012 .

[24]  Ralf Heinrich,et al.  The DLR TAU-Code: Recent Applications in Research and Industry , 2006 .

[25]  Jean Potvin,et al.  Effect of the Transient Nature of Flow on Annular Parachute Drag Prediction , 2012 .

[26]  F. Menter Two-equation eddy-viscosity turbulence models for engineering applications , 1994 .

[27]  Robert Tomaro,et al.  An Overset Unstructured Grid Methodology Applied to a C-130 with a Cargo Pallet and Extraction Parachute , 2006 .

[28]  William Johnson,et al.  Computational Aerodynamics of the C-130 in Airdrop Configurations , 2003 .

[29]  Andreas Schröder,et al.  Experimental investigation of the flow field topology for several cargo drop configurations , 2012 .