National Air and Space Museum:

Radiance Lighting Analysis of the proposed National Air and Space Museum at the Dulles International Airport, by Lawrence Berkeley National Laboratory

November 4 1999 

Methods of Analysis

The preliminary analyses were performed using simplified 3D models created by Lawrence Berkeley National Laboratory. The simplified models were developed from the printed 100% CD drawing set and AutoCAD data files provided by the Smithsonian.

The final analyses were performed with more complex geometry. The geometry for the Radiance 3D model as modeled by Interface Multimedia was provided by the Smithsonian. The FormZ drawing files were initially exported into Radiance through the Wavefront/OBJ file format and tested extensively for light leaks and consistency with the 100% CD documents. Significant differences between the 3D model and the drawings were resolved where possible, but some differences remain. For example, the 3D model contained geometry for only 1/2 of the Space Hangar. We presumed that the hangar was bilaterally symmetrical and mirrored the north side to the south. This has since been discovered to be incorrect. However, due to time and budget constraints and the fact that the implications for the lighting analysis are nominal, this was not corrected for the final renderings. On the other hand, the 3D model was discovered to contain windows along the northwest side of the Aviation Hangar. These windows were replaced with opaque wall material for the final analysis.

The approximately 200 aircraft suspended in the Aviation Hangar were presumed to have a significant impact on the overall lighting levels. To address this concern, 3D models of many aircraft were provided by the Smithsonian. A model of the SR-71 was purchased from Viewpoint Digital. Models of the vast majority of the aircraft, however, were not available. The AutoCAD drawings were then used as a template to extrude the plan outlines into "pancake" representations of actual aircraft. The thickness of these extrusions varied from 1200cm to 400cm depending upon the overall size of the aircraft. The aircraft were then "hung" in the hangar at four different heights depending upon the "level" they belong to.

Assumptions of the Model

Surface Reflectances were measured from samples provided by the Smithsonian. Total hemispherical reflectance was measured with a Minolta CM2002 spectrophotometer. The spectral color and specular reflectance at 7 degrees was also measured using this device for the Radiance model.

Simulation Parameters

The final Radiance simulations were performed using the following simulation parameters:

These parameters instruct Radiance to calculate two ambient bounces of light (-ab 2) and to perform a very accurate estimate of the ambient component (-ad 1200 -as 600 -aa .175). In addition, the specular threshold was set to 1% (-st .01) to account for the small semi-specular component measured in the material samples. The sub-sampling of direct light sources was also turned on to improve the accuracy of the luminaire distributions a close proximity to other surface geometry (-ds .5). The background ambient value was empirically determined through an iterative Radiance simulation and set accordingly (-av .02 .02 .02).

For more information about these parameters, please see the Radiance Reference Manual for the rpict command.

Calculation of Energy Savings

Energy Savings were based upon the assumption that the quartz halogen emergency lighting would be required to stay on at all times. This has since been discovered to be incorrect.

Limitations of the Analysis

Limitations of this lighting simulation are related to the input, calculation method, and analysis techniques.


 

|Analysis and Conclusions|