The take-off capacity of a flying boat depends upon the design of the hull bottom ahead as well as aft of the step. Systematic tests - largely made by industry itself - had proved the benefit accruing from a well designed hull bottom long before theoretical insight into the flow phenomena involved had been obtained. The theoretical framing of the problem was beset with serious difficulties and, though restricted to the processes within range of the planing bottom ahead of the step, the solutions do not yet afford a comprehensive survey
The previously employed method of extrapolating the total resistance to full size with lambda(exp 3)...
Flight tests were conducted on the OS2U-2 seaplane with simple circular-arc-type ailerons directly c...
The extension of wind tunnel tests of models of airship hulls to full scale requires an extension fr...
Experiments with planing surfaces are fundamental, hydrodynamic researches for the purpose of obtain...
The first part of this report shows the differences between commercial and war airships and then goe...
A previous report discusses the experimental program of a systematic exploration of all questions co...
In order to determine the effect of the surface conditions of a wing on the aerodynamic characterist...
Porpoising characteristics were observed on V-body fitted with tail surfaces for different combinati...
An investigation has been made at large scale of the characteristics of highly swept wings. Data wer...
For the purpose of solving all the problems involved, an investigation was made with flat, rectangul...
This report presents experiments and calculations for the purpose of determining the landing gear re...
The results of a complete tank test of a model of a flying-boat hull of unconventional form, having ...
The NACA model 11-B, which has a longitudinally concave planing bottom forward of the step, was test...
An investigation was made in the Langley 300 MPH 7- by 10-foot tunnel to determine the aerodynamic c...
Four planing surfaces, all having beams of 16 inches and lengths of 60 inches but varying in dead ri...
The previously employed method of extrapolating the total resistance to full size with lambda(exp 3)...
Flight tests were conducted on the OS2U-2 seaplane with simple circular-arc-type ailerons directly c...
The extension of wind tunnel tests of models of airship hulls to full scale requires an extension fr...
Experiments with planing surfaces are fundamental, hydrodynamic researches for the purpose of obtain...
The first part of this report shows the differences between commercial and war airships and then goe...
A previous report discusses the experimental program of a systematic exploration of all questions co...
In order to determine the effect of the surface conditions of a wing on the aerodynamic characterist...
Porpoising characteristics were observed on V-body fitted with tail surfaces for different combinati...
An investigation has been made at large scale of the characteristics of highly swept wings. Data wer...
For the purpose of solving all the problems involved, an investigation was made with flat, rectangul...
This report presents experiments and calculations for the purpose of determining the landing gear re...
The results of a complete tank test of a model of a flying-boat hull of unconventional form, having ...
The NACA model 11-B, which has a longitudinally concave planing bottom forward of the step, was test...
An investigation was made in the Langley 300 MPH 7- by 10-foot tunnel to determine the aerodynamic c...
Four planing surfaces, all having beams of 16 inches and lengths of 60 inches but varying in dead ri...
The previously employed method of extrapolating the total resistance to full size with lambda(exp 3)...
Flight tests were conducted on the OS2U-2 seaplane with simple circular-arc-type ailerons directly c...
The extension of wind tunnel tests of models of airship hulls to full scale requires an extension fr...