Hydrodynamic Investigation of a Series of Hull Models Suitable for Small Flying Boats and Amphibians
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Hugli, W C , Jr↗
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Static properties and resistance characteristics of a family of seaplane hulls having varying length-beam ratio
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Carter, Arthur W↗
Aerodynamic characteristics of a refined deep-step planing-tail flying-boat hull with various forebody and afterbody shapes
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Riebe, John M↗
Aerodynamic Characteristics of Flying-boat Hulls Having Length-beam Ratios of 20 and 30
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Riebe, John M↗
Aerodynamic characteristics of three deep-step planing-tail flying-boat hulls
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Riebe, John M↗
High-speed Wind-tunnel Investigation of a Flying-boat Hull with High Length-beam Ratio
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Riebe, John M↗
Aerodynamic Characteristics of a Flying-boat Hull Having a Length-beam Ratio of 15 and a Warped Forebody
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Macleod, Richard G↗
Preliminary Wind-tunnel Investigation at High-subsonic Speeds of Planing-tail, Blended, and Airfoil-forebody Swept Hulls
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Riebe, John M↗
Hydrodynamic Characteristics of a Swept Planing-tail Hull
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Mckann, Robert E↗
Effect of an Increase in Hull Length-beam Ratio from 15 to 20 on the Hydrodynamic Characteristics of Flying Boats
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Carter, Arthur W↗
Hydrodynamic Characteristics of Aerodynamically Refined Planing-tail Hulls
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Mckann, Robert↗
Aerodynamic Characteristics of an Airfoil-forebody Swept Flying-boat Hull with a Wing and Tail Swept Back 51.3 Degrees at the Leading Edge
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Naeseth, Rodger L↗
Hydrodynamic Directional Behavior of a Swept Planing-tail Hull
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Arabian, Donald D↗
An investigation of the hydrodynamic characteristics of a dynamic model of a transonic seaplane design having a planing-tail hull
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Morse, Archibald E , Jr↗
Theoretical determination of water loads on pitching hulls and shock-mounted hydro-skis
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Schnitzer, Emanuel↗
Statistical approach to the estimation of loads and pressures on seaplane hulls for routine operations
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Steiner, Roy↗
Some Yawing Tests of a 1/30-scale Model of the Hull of the XPB2M-1 Flying Boat
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Locke, F W S , Jr↗
Calculation of Pressure Distribution on Airship Hulls
These calculations were based on the shape of the ZR III, with the following simplifications: cars, fins, and rudders removed; all cross sections replaced by equivalent circular cross sections. Under these assumptions the pressure distribution was calculated for the following cases: symmetrical case, or flow parallel to the axis; unsymmetrical case, or flow at an angle to the axis. In both cases the simple potential flow first forms the basis for the determination of the pressure distribution.
Von Karman, Theodor↗