20th International Workshop on Principles of Diagnosis paper

Finite element for Structured Model - Temperature 293deg R

HIRENASD References
Reiner, Boucke, Ballman and Behr - COMPUTATIONAL ANALYSIS OF HIGH REYNOLDS NUMBER AERO-STRUCTURAL DYNAMICS (HIRENASD) EXPERIMENTS
chen, Brakhage, Behr, and Ballmann - NUMERICAL SIMULATIONS FOR PREPARING NEW AERO-STRUCTURAL DYNAMIC EXPERIMENTS IN ETW WITH A MODIFIED HIRENASD WING MODEL
Ballmann, etal - Experimental Analysis of High Reynolds Number Aero-Structural Dynamics in ETW
Neumann, Nitzsche and Voss - Aeroelastic Analysis by Coupled Non-linear Time Domain Simulation
Neumann and Ritter - STEADY AND UNSTEADY AEROELASTIC SIMULATIONS OF THE HIRENASD WIND TUNNEL EXPERIMENT

RTO-2008-Aeroelastic Analysis by Coupled Non.pdf

Oscillating Turntable for the Measurment of Unsteady Aerodynamic Phenomenon (BSCW)
A New Forced Oscillation Capability for the TDT
Physical Properties of Benchmark SCW (includes measured coordinates in tables)

RSW Airfoil Coordinates of model tested in 1980's by Ricketts
MBB_A3 coordinates - theoretical and actual comparison

Meyer et al. - 2003 - Propulsion IVHM Technology Experiment Overview.pdf

workshop presentations access page (updated Dec 11,2010 JH)
workshop presentations access, v3 (updated JHeeg, Dec 11, 2012)

mode shapes interpolated on coarse grid form Centaur

IGES file
Geom.and Str. Properties of a Rectangular Supercritical Wing Oscillated in Pitch for Measurement of Unsteady Transonic Pressure Distributions, Ricketts, Watson, Sandford, Seidel - Nov 1983 (Ricketts)
Transonic Pressure Distributions on a Rectangular Supercritical Wing Oscillating in Pitch, Ricketts, Sandford, Seidel, Watson, JA Vol 21 No 8, 1983
Computational Test Cases - early RSW (Ricketts - in RTO publicaton) - Complete results are in NASA TM 85765 - Subsonic and Transonic Unsteady- and Steady-Pressure Measurements on a Rectangular Supercritical Wing Oscillated in Pitch by Ricketts, Sandford, W
PLEASE USE UPDATED FILE (RSW_AePW_expdata_Fegb10_2012.zip instead) Steady Experimental TestCase Results (Tecplot format)
PLEASE USE UPDATED FILE (RSW_AePW_expdata_Fegb10_2012.zip instead) Unsteady Experimental TestCase Results (Tecplot format)
RSW wing only (NO splitter plate)
RSW wing WITH splitter plate
Updated data files to remove bad data points and correct data zone mislabeling
Assessment of bad data points, Feb 2012
February 10, 2012 update