Presented here are the summary charts of the collapsed results of general tank tests of about 100 flying boat hull models. These summary charts are intended to be used as an engineering tool to enable a flying boat designer to grasp more quickly the significance of various hull form parameters as they influence his particular airplane. The form in which the charts are prepared is discussed in some detail in order to make them clearer to the designer. This is a data report, and no attempt has been made to produce conclusions or correlations of the usual sort. However, some generalizations are put forward on the various methods in which summary charts may be used
J ~General tank tests of a ~-size model of the hull of the B6eing W313-1 flying boat were made in”La...
This report is a compilation of test data on airplane fuselages, nacelles, airship cars, seaplane fl...
The hydrodynamic characteristics of a model of the hull of the Short Calcutta (N.A.C.A. Model 47) ar...
The results of a general tank test of a 1/6 full-size model of the hull of the Pem-1 flying boat (N....
Report presents the results of a survey of problems encountered in applying general test data to the...
Presented here are the summary charts of the collapsed results of general tank tests of about 100 fl...
Model No. 11-A was designed as an improvement over N.A.C.A. Model No. 11, a complete test of which i...
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 results of tank tests of three models of flying-boat hulls of the pointed-step type with differe...
Measurements of aerodynamic drag were made in the 20-foot wind tunnel on a representative group of 1...
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 results of a general tank test model 11-C, a conventional pointed afterbody type of flying-boat ...
Report presents the results of a survey of problems encountered in applying general test data to the...
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...
J ~General tank tests of a ~-size model of the hull of the B6eing W313-1 flying boat were made in”La...
This report is a compilation of test data on airplane fuselages, nacelles, airship cars, seaplane fl...
The hydrodynamic characteristics of a model of the hull of the Short Calcutta (N.A.C.A. Model 47) ar...
The results of a general tank test of a 1/6 full-size model of the hull of the Pem-1 flying boat (N....
Report presents the results of a survey of problems encountered in applying general test data to the...
Presented here are the summary charts of the collapsed results of general tank tests of about 100 fl...
Model No. 11-A was designed as an improvement over N.A.C.A. Model No. 11, a complete test of which i...
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 results of tank tests of three models of flying-boat hulls of the pointed-step type with differe...
Measurements of aerodynamic drag were made in the 20-foot wind tunnel on a representative group of 1...
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 results of a general tank test model 11-C, a conventional pointed afterbody type of flying-boat ...
Report presents the results of a survey of problems encountered in applying general test data to the...
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...
J ~General tank tests of a ~-size model of the hull of the B6eing W313-1 flying boat were made in”La...
This report is a compilation of test data on airplane fuselages, nacelles, airship cars, seaplane fl...
The hydrodynamic characteristics of a model of the hull of the Short Calcutta (N.A.C.A. Model 47) ar...