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aerodynamic aileron effectiveness airspeed angle of attack blade angle bomb bomb-bay doors bulkhead calm and rough CD CD chord COMMITTEE FOR AERONAUTICS condition ditching behavior ditching performance DITCHING TESTS dive doors removed double-slotted flaps dual-rotating propeller dynamic elevator deflection flaps deflected full-scale airplane fuselage hydrofoil increased indicated airspeed landing attitude landing speeds Langley Field Langley Memorial Aeronautical Langley tank load Margaret F maximum deceleration maximum lift coefficient Memorial Aeronautical Laboratory miles per hour nacelles NATIONAL ADVISORY COMMITTEE North American Aviation nose obtained orifices outdoor catapult partial-span peak pressure percent Photographs porpoising pounds presented in figure pressure impulse Reynolds number rH rH rough water rudder shown in figure simulated damage Simulated failure single-blade propeller slotted spoiler stalling characteristics STANFORD UNIVERSITY tail surfaces tank tests thrust line V/nD velocity vertical waist-gun doors WARTIME REPORT Wave crests wheel doors wind exists