At the request of the Bureau of Aeronautics, Navy Department, the National Advisory Committee for Aeronautics at Langley Field is investigating the get-away characteristics of an N-9H, a DT-2, and an F-5l, as representing, respectively, a single float, a double float, and a boat type of seaplane. This report covers the investigation conducted on the N-9H. The results show that a single float seaplane trims aft in taking off. Until a planing condition is reached the angle of attack is about 15 degrees and is only slightly affected by controls. When planing it seeks a lower angle, but is controllable through a widening range, until at the take-off it is possible to obtain angles of 8 degrees to 15 degrees with corresponding speeds of 53 to 41...
This report presents experiments and calculations for the purpose of determining the landing gear re...
This report gives the results of wind-tunnel tests with a seaplane model as a contribution to the so...
This note discusses the limitations of the conventional tank test of a seaplane model. The advantage...
This report, on the planing and get-away characteristics of the F-5-L, gives the results of the seco...
Committee for Aeronautics at Langley Field is investigating the pkmkg a~d get-away charac-teristics ...
This report presents the results of an investigation of the planing and get-away characteristics of ...
The investigation presented in this report was conducted for the purpose of determining the distribu...
This is the second of a series of investigations to determine water pressure distribution on various...
Porpoising characteristics were observed on V-body fitted with tail surfaces for different combinati...
A model of the F-5-L seaplane was made, verified, and tested at 40 miles an hour in the 8' x 8' tunn...
This report, on the planing and get-away characteristics of the F-5-L, gives the results of the seco...
The take-off stability characteristics of a Consolidated Vultee Aircraft Corporation Skate 7 seaplan...
The hydrodynamic characteristics of a flying-boat incorporating a low-drag, planing-tail hull were d...
Tests were made to fill partly the need for information on the effect of afterbody dimensions on the...
The resistance of water, even at low speeds, may be such as to render it impossible to take off. For...
This report presents experiments and calculations for the purpose of determining the landing gear re...
This report gives the results of wind-tunnel tests with a seaplane model as a contribution to the so...
This note discusses the limitations of the conventional tank test of a seaplane model. The advantage...
This report, on the planing and get-away characteristics of the F-5-L, gives the results of the seco...
Committee for Aeronautics at Langley Field is investigating the pkmkg a~d get-away charac-teristics ...
This report presents the results of an investigation of the planing and get-away characteristics of ...
The investigation presented in this report was conducted for the purpose of determining the distribu...
This is the second of a series of investigations to determine water pressure distribution on various...
Porpoising characteristics were observed on V-body fitted with tail surfaces for different combinati...
A model of the F-5-L seaplane was made, verified, and tested at 40 miles an hour in the 8' x 8' tunn...
This report, on the planing and get-away characteristics of the F-5-L, gives the results of the seco...
The take-off stability characteristics of a Consolidated Vultee Aircraft Corporation Skate 7 seaplan...
The hydrodynamic characteristics of a flying-boat incorporating a low-drag, planing-tail hull were d...
Tests were made to fill partly the need for information on the effect of afterbody dimensions on the...
The resistance of water, even at low speeds, may be such as to render it impossible to take off. For...
This report presents experiments and calculations for the purpose of determining the landing gear re...
This report gives the results of wind-tunnel tests with a seaplane model as a contribution to the so...
This note discusses the limitations of the conventional tank test of a seaplane model. The advantage...