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GemmusBoeurlag ject Comtract No.EVE-16-2929 <br /> Tethoology Devtiopmen t CLIProjectNa.160731 <br /> 3..4.1 Estimation of Airflow Accuracy&Maximum Velocity .50 <br /> 3A.2 Estimation of%LEL Distribution Accuracy&Maximum Error_._____._......___.52 <br /> 4 Modified 45-03 Hangar CFD Modeling&Results(Case 2&3) 53 <br /> 4.1 Case.2&3 Flow Volume Geometry&CFD Model Description 54 <br /> 41 Modeling Results ....________..... ......... ..........._________.......... <br /> 4.11 Case 2/Scenario 1 —Paint Mode Normal --------------------------------------55 <br /> 4.2.2 Case 2/Scenario 2—Ventilation Fail Off. 63 <br /> 41.3 Case 3/Scenario 5d—75%Ventilation Mode _68 <br /> 4.2.4 Case 3/Scenario 1 —75%Ventilation Mode,Wing&Horizontal Stabilizer Paint <br /> Configuration 1 75 <br /> 4.2.5 Case 3/Scenario 2c—75%Ventilation Mode, Wing &Horizontal Stabilizer Paint <br /> Configuration2___ .................. ..........................___________............ ...... 83 <br /> 4.2.6 Case 3/Scenario 3—75%Ventilation Mode,Wing&Horizontal Stabilizer Paint <br /> Configuration 3 91 <br /> 41_7 Case 3/Scenario 4b—75%Ventilation Mode,Wing &Horizontal Stabilizer Paint <br /> Configuration 4 98 <br /> 5 Summary/Conclusions 106 <br /> Si General Airflow&%LEL CFD Modeling 0f45-03 Hangar 106 <br /> 5.2 %LEL Predictions For New 45-03 Hangar Configuration.......... ...... <br /> 5.3 Analysis Key Parameters 107 <br /> 6 References 108 <br />