Short duration force measurements in impulse facilities

A new multiple component stress wave force balance has been designed, calibrated and tested in the High Enthalpy Shock Tunnel Gottingen (HEG) of the German Aerospace Center (DLR). The balance is able to measure forces of short duration (milliseconds) on instrumented models from angles of attack from -40 to 20 degrees. Two models, a blunt cone 303mm long and a standard force reference model (HB-2) of 70mm diameter, are used to establish the accuracy of the force balance. The blunt cone tests were conducted at two different test conditions with a constant Mach number of 7.8 and total enthalpies of 3.0 and 3.5MJ/kg. At 0 degrees angle of attack and an enthalpy of 3.0MJ/kg, the measured axial coefficient was recovered to within 6% when compared to computational fluid dynamic (CFD) simulations. At –10 degrees, the axial and normal coefficients were within 6% and 9% respectively of CFD predictions while the center of pressure (based on chord length) was within 2%. Tests with the HB-2 standard force reference model were conducted at enthalpies ranging from 12 to 22 MJ/kg at an angle of attack of 0 degrees. A linear variation of the axial coefficient with the viscous similarity parameter was predicted with non-equilibrium CFD simulations assuming a laminar boundary layer. The recovered axial force coefficient remained within 6% of the CFD predictions and compared well with experimental results from other wind tunnel facilities. Reasonable comparison of pressure and heat flux measurements along longitudinal symmetry lines of the model was obtained. The accuracy of the force balance is estimated at approximately 5% for the axial component and 4% for the normal and pitching moment components.

[2]  H. Olivier,et al.  Force Measurements in Hypersonic Impulse Facilities , 1998 .

[3]  Rémy Prost,et al.  Discrete constrained iterative deconvolution algorithms with optimized rate of convergence , 1984 .

[4]  Allan Paull,et al.  Scramjet thrust measurement in a shock tunnel , 1995 .

[5]  Mario Carbonaro Aerodynamic Force Measurements in the VKI Longshot Hypersonic Facility , 1993 .

[6]  Allan Paull,et al.  Experiments on cruise propulsion with a hydrogen scramjet , 1998 .

[7]  William J.T. Daniel,et al.  Three-component force balance for flows of millisecond duration , 1996 .

[8]  J D Gray SUMMARY REPORT ON AERODYNAMIC CHARACTERISTICS OF STANDARD MODELS HB-1 AND HB-2 , 1964 .

[9]  Klaus Hannemann,et al.  The influence and the delay of driver gas contamination in HEG , 2000 .

[10]  Klaus Hannemann,et al.  High Enthalpy Flows in the HEG Shock Tunnel: Experiment and Numerical Rebuilding (Invited) , 2003 .

[11]  Richard A. Thompson,et al.  A review of reaction rates and thermodynamic and transport properties for the 11-species air model for chemical and thermal nonequilibrium calculations to 30000 K , 1989 .

[12]  S R Sanderson,et al.  Drag balance for hypervelocity impulse facilities , 1991 .

[13]  K. W. Naumann,et al.  Millisecond aerodynamic force measurement with side-jet model in theISL shock tunnel , 1993 .

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

[15]  J.M.A. Longo,et al.  The sharp edge flight experiment SHEFEX , 2002 .