Analysis of planing data for use in predicting hydrodynamic impact loads
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HYDRODYNAMICS↗
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Effect of increase in afterbody length on the hydrodynamic qualities of a flying-boat hull of high length-beam ratio
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HULL AFTERBODIES↗
Water Landing Investigation of a Model Having a Heavy Beam Loading and a 30 Degree Angle of Dead Rise
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HULLS - IMPACT↗
Effect of an Increase in Angle of Dead Rise on the Hydrodynamic Characteristics of a High-length-beam-ratio Hull
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HULLS - SPRAY REDUCTION↗
Landing characteristics in waves of three dynamic models of flying boats
Powered models of three different flying boats were landed in oncoming waves of various heights and lengths. The effects of varying the trim at landing, the deceleration after landing, and the size of the waves were determined. Data are presented on the motions and accelerations obtained during landings in rough water.
LOADS, LANDING - IMPACT, WATER↗
Tests of a 1/40-scale Wing-hull Model and a 1/10-scale Float-strut Model of the Hughes-kaiser Cargo Airplane in the Two-Dimensional Low-Lurbulence Pressure Tunnel
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WIND TUNNEL TESTS - NACA - PRESSURE, LOW-TURBULENC↗
Control-Motion Studies of the PBM-3 Flying Boat in Abrupt Pull-Ups
No abstract available
INSTRUMENTS - CONTROL POSITION RECORDERS - NACA↗
Design criterions for the dimensions of the forebody of a long-range flying boat
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HULLS - SPRAY REDUCTION↗
Landing characteristics of a model of a flying boat with the depth of step reduced to zero by means of a retractable planing flap
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HULL FLAPS, RECTRACTABLE↗
JRM-1 Landing Impact Characteristics from Model Tests
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SEAPLANES - IMPACT↗
Some Lift and Drag Measurements of Two Configurations of a Nacelle and Oil-cooler Scoop for the Hughes-kaiser Cargo Airplane
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WIND TUNNEL TESTS (NACA - PRESSURE, LOW-TURBULENCE↗
An analysis of the main spray characteristics of some full-size multi-engined flying boats
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CHARTS - FLYING BOATS↗
Theoretical and Experimental Wing-tip Accelerations of a Small Flying Boat During Landing Impacts
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LOADS, LANDING↗
An analysis of the airspeeds and normal accelerations of Martin M-130 airplanes in commercial transport operation
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ACCELERATIONS - MARTIN 1130↗
Hydrodynamic Qualities of a Hypothetical Flying Boat with a Low-drag Hull Having a Length-beam Ratio of 15
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HULLS - NACA 213 - CHARACTERISTICS - TANK TESTS (N↗
Hydrodynamic Impact Loads in Rough Water for a Prismatic Float Having an Angle of Dead Rise of 30 Degrees
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LOADS - FLOATS↗
Effect of Longitudinal Steps on Skipping Characteristics of PB2Y-6 Flying Boat
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AUTHORS (2)↗
A Study of Water Pressure Distribution During Landings with Special Reference to a Prismatic Model Having a Heavy Beam Loading and a 30 Degree Angle of Dead Rise
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FLOATS & HULLS↗