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airplane model analysis Ang/e angle of attack angle of yaw calculations carbon dioxide centimeters Circular Fuselage clear atmosphere cloud indicator column and plate COMMITTEE FOR AERONAUTICS computed CONFIDENTIAL dihedral angle downwash angle Effect of changing emission exchange of radiation field of view flight half-angle horizontal tail impact tube infrared radiation investigation Langley Field Langley Memorial Aeronautical Langley stability tunnel lens unit lift coefficient Mach number Memorial Aeronautical Laboratory meter millibars monochromatic radiation NACA NATIONAL ADVISORY COMMITTEE nondimensional nozzle obtained oi 2i ozone percent plate compressive strengths present pressure radiation chart range reference relaxation self-emission shown in figure slab slope small positive angles span load distribution specific humidity spectral transmission factor stress-strain curves tables and chart tail surfaces temperature tests thermoelectric eye thermopile tion total-head defects vertical tail vertical-tail area WARTIME REPORT water vapor wave number wing yield stress