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aerodynamic AERONAUTICS TABLE air-flow rate air-flow survey airfoil airplane alinement angle alinement-angle angle of attack calculated calibration COMMITTEE FOR AERONAUTICS computing Continued POINT DRAG coolers in series cooling-air temperatures corner flange correction method curves determined differential flap system differential ratio discontinuity drag equation DRAO dummy supports dynamic pressure effective dihedral equation experimental over-all flap deflection flap-differential ratio flexible bulkhead flows wherein energy identical coolers inlet oil temperature jet-boundary Langley Field Langley Memorial Aeronautical lift coefficient Mach number measured NACA Rep NATIONAL ADVISORY COMMITTEE normal supports obtained oil flow oil-cooler oo+j over-all performance ox*o percent point drag coefficient procedure profile drag reference rotary valves shear stresses slipstream spar caps specific heat dissipation specified over-all effectiveness static pressure support struts tare supports tare tests tion torsion torsion box wake shadow Wind Tunnel wing X-Forces yaw head