The NACA model 11-B, which has a longitudinally concave planing bottom forward of the step, was tested over a wide range of loading. The results of the tests are presented as curves of resistance and trimming moment plotted against speed for various trim angles and as curves of resistance coefficient at best trim angle, and trimming-moment coefficient. The characteristics of the form at the optimum trim are compared with those of NACA model 11-C which has the same form with the exception of a planing bottom longitudinally straight near the step. Photographs of the models being towed in the tank are included for a comparison of the spray patterns. At the best angles of trim in each case model 11-B has lower resistance at high speeds, a highe...
The NACA model 11-G flying-boat hull, a modification of NACA model 11-A was tested over a range of l...
The hydrodynamic characteristics of a flying-boat incorporating a low-drag, planing-tail hull were d...
A 1/10-size model of the hull of the French flying boat Latecoere 521 was tested in the NACA tank. T...
The NACA model 11-G flying-boat hull, a modification of NACA model 11-A was tested over a range of l...
The results of a general tank test model 11-C, a conventional pointed afterbody type of flying-boat ...
Model No. 11-A was designed as an improvement over N.A.C.A. Model No. 11, a complete test of which i...
Four models with longitudinal steps on the forebody were developed by modification of a model of a c...
Four planing surfaces, all having beams of 16 inches and lengths of 60 inches but varying in dead ri...
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...
Tests were conducted in Langley Tank no. 2 on models of an unconventional flying-boat hull called a ...
The results of tank tests of three models of flying-boat hulls of the pointed-step type with differe...
The results of a general tank test of a 1/6 full-size model of the hull of the Pem-1 flying boat (N....
Data taken from tests at constant speed to establish trim limits of stability, tests at accelerated ...
NACA model 11-C was tested according to the general method with the angle of afterbody keel set at f...
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...
The NACA model 11-G flying-boat hull, a modification of NACA model 11-A was tested over a range of l...
The hydrodynamic characteristics of a flying-boat incorporating a low-drag, planing-tail hull were d...
A 1/10-size model of the hull of the French flying boat Latecoere 521 was tested in the NACA tank. T...
The NACA model 11-G flying-boat hull, a modification of NACA model 11-A was tested over a range of l...
The results of a general tank test model 11-C, a conventional pointed afterbody type of flying-boat ...
Model No. 11-A was designed as an improvement over N.A.C.A. Model No. 11, a complete test of which i...
Four models with longitudinal steps on the forebody were developed by modification of a model of a c...
Four planing surfaces, all having beams of 16 inches and lengths of 60 inches but varying in dead ri...
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...
Tests were conducted in Langley Tank no. 2 on models of an unconventional flying-boat hull called a ...
The results of tank tests of three models of flying-boat hulls of the pointed-step type with differe...
The results of a general tank test of a 1/6 full-size model of the hull of the Pem-1 flying boat (N....
Data taken from tests at constant speed to establish trim limits of stability, tests at accelerated ...
NACA model 11-C was tested according to the general method with the angle of afterbody keel set at f...
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...
The NACA model 11-G flying-boat hull, a modification of NACA model 11-A was tested over a range of l...
The hydrodynamic characteristics of a flying-boat incorporating a low-drag, planing-tail hull were d...
A 1/10-size model of the hull of the French flying boat Latecoere 521 was tested in the NACA tank. T...