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advance research results Advance Restricted Report AERONAUTICS WARTIME REPORT air drag angle of attack attitude authorized group requiring balanced split flap belt method blade angle carburetor clean-wing condition climb COMMITTEE FOR AERONAUTICS contravanes conventional propeller cooling-air pressures cowl flaps Curtiss-Wright Corporation cylinder elevator deflection engine expedite general distribution Flap deflection FLIGHT INVESTIGATION flight tests ground-run distance Grumman fairing gun barrel gun fairings inches inches of mercury indicated airspeed landing Langley Memorial Aeronautical lift coefficient Memorial Aeronautical Laboratory miles per hour NACA WARTIME REPORTS NATIONAL ADVISORY COMMITTEE nically edited papers originally issued partial power percent pressure distribution projecting gun propulsive efficiency provide rapid distribution REPORT ORIGINALLY ISSUED root chord Ryan ST short-nose slipstream stall at altitude stalling speed submerged gun surface orifices tail wheel temperatures Three point tion true airspeed unfaired guns velocity viously held WARTIME REPORT ORIGINALLY Wheels first bounced yaw angle