A model of one of the twin hulls of the Italian Savoia S-55-X flying boat (N.A.C.A. Model 46) was tested in the N.A.C.A. tank according to the general method. The data obtained from these tests cover a broad range of speeds, loads, and trims and are given in nondimensional form to facilitate their use in applying this form of hull to any other flying boat or comparing it's performance with the performance of any other hulls. The results show that the resistance characteristics at best trim of this model are excellent throughout the speed range. In order to compare the performance of the S-55-X hull with that of the 35, a pointed-step hull developed at the N.A.C.A. tank, the data are used in the computations of take-off example of a twin-hul...
The results of a general tank test of a 1/6 full-size model of the hull of the Pem-1 flying boat (N....
Tests were made in the NACA tank and in the NACA 7 by 10 foot wind tunnel on two models of transvers...
Four models with longitudinal steps on the forebody were developed by modification of a model of a c...
A general test was made in the N.A.C.A. tank of a 1/12-size model of the hull of the British Singapo...
A model of one of the twin hulls of the Italian Savoia S-55-X flying boat (N.A.C.A. Model 46) was te...
This note discusses the limitations of the conventional tank test of a seaplane model. The advantage...
A 1/7.06 full-size model of the NC-type hull was tested in the N.A.C.A. tank by both the general met...
A 1/10-size model of the hull of the French flying boat Latecoere 521 was tested in the NACA tank. T...
The results of a complete test in the N.A.C.A. tank on a model of the hull of Sikorsky S-40 flying b...
The hydrodynamic characteristics of a model of the hull of the Short Calcutta (N.A.C.A. Model 47) ar...
This note discusses the limitations of the conventional tank test of a seaplane model. The advantage...
Model No. 11-A was designed as an improvement over N.A.C.A. Model No. 11, a complete test of which i...
The results of tank tests of three models of flying-boat hulls of the pointed-step type with differe...
Large models of the Mark V and Mark VI floats used for single float seaplanes (National Advisory Com...
The present tests illustrate how the aerodynamic drag of a flying boat hull may be reduced by follow...
The results of a general tank test of a 1/6 full-size model of the hull of the Pem-1 flying boat (N....
Tests were made in the NACA tank and in the NACA 7 by 10 foot wind tunnel on two models of transvers...
Four models with longitudinal steps on the forebody were developed by modification of a model of a c...
A general test was made in the N.A.C.A. tank of a 1/12-size model of the hull of the British Singapo...
A model of one of the twin hulls of the Italian Savoia S-55-X flying boat (N.A.C.A. Model 46) was te...
This note discusses the limitations of the conventional tank test of a seaplane model. The advantage...
A 1/7.06 full-size model of the NC-type hull was tested in the N.A.C.A. tank by both the general met...
A 1/10-size model of the hull of the French flying boat Latecoere 521 was tested in the NACA tank. T...
The results of a complete test in the N.A.C.A. tank on a model of the hull of Sikorsky S-40 flying b...
The hydrodynamic characteristics of a model of the hull of the Short Calcutta (N.A.C.A. Model 47) ar...
This note discusses the limitations of the conventional tank test of a seaplane model. The advantage...
Model No. 11-A was designed as an improvement over N.A.C.A. Model No. 11, a complete test of which i...
The results of tank tests of three models of flying-boat hulls of the pointed-step type with differe...
Large models of the Mark V and Mark VI floats used for single float seaplanes (National Advisory Com...
The present tests illustrate how the aerodynamic drag of a flying boat hull may be reduced by follow...
The results of a general tank test of a 1/6 full-size model of the hull of the Pem-1 flying boat (N....
Tests were made in the NACA tank and in the NACA 7 by 10 foot wind tunnel on two models of transvers...
Four models with longitudinal steps on the forebody were developed by modification of a model of a c...