Add to ORKGFollowing a summary of the multiplicity of domestic and foreign floats and a brief enumeration of the requirements of floats, the essential form parameters and their effect on the qualities of floats are detailed. On this basis a standard float design is developed which in model families with varying length/beam ratio and angle of dead rise is analyzed by an experimental method which permits its best utilization on any airplane
Tests were made to fill partly the need for information on the effect of afterbody dimensions on the...
The present report includes a description of the making of three-component measurements on a full-si...
At the request of the Bureau of Aeronautics, Navy Department, the National Advisory Committee for Ae...
Following a summary of the multiplicity of domestic and foreign floats and a brief enumeration of th...
Tests were made in the NACA tank and in the NACA 7 by 10 foot wind tunnel on two models of transvers...
Large models of the Mark V and Mark VI floats used for single float seaplanes (National Advisory Com...
This report contains the results of tank tests carried out at free trim on seventeen hulls and float...
The drag of five models of side floats was measured in the N.A.C.A. 7- by 10-foot wind tunnel. The m...
At the request of the Bureau of Aeronautics, Navy Department, a study of the design of floats especi...
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...
Three models of V-bottom floats for twin-float seaplanes (N.A.C.A. models 57-A, 57-B, and 57-C) havi...
Basic lift data on planing surfaces have been analyzed and the data applied to the design of flying-...
The following report contains the most essential data for the hydrodynamic portion of the twin-float...
Experimental data, such as the results of tank tests of models, render it possible to predict, at le...
Tests were made to fill partly the need for information on the effect of afterbody dimensions on the...
The present report includes a description of the making of three-component measurements on a full-si...
At the request of the Bureau of Aeronautics, Navy Department, the National Advisory Committee for Ae...
Following a summary of the multiplicity of domestic and foreign floats and a brief enumeration of th...
Tests were made in the NACA tank and in the NACA 7 by 10 foot wind tunnel on two models of transvers...
Large models of the Mark V and Mark VI floats used for single float seaplanes (National Advisory Com...
This report contains the results of tank tests carried out at free trim on seventeen hulls and float...
The drag of five models of side floats was measured in the N.A.C.A. 7- by 10-foot wind tunnel. The m...
At the request of the Bureau of Aeronautics, Navy Department, a study of the design of floats especi...
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...
Three models of V-bottom floats for twin-float seaplanes (N.A.C.A. models 57-A, 57-B, and 57-C) havi...
Basic lift data on planing surfaces have been analyzed and the data applied to the design of flying-...
The following report contains the most essential data for the hydrodynamic portion of the twin-float...
Experimental data, such as the results of tank tests of models, render it possible to predict, at le...
Tests were made to fill partly the need for information on the effect of afterbody dimensions on the...
The present report includes a description of the making of three-component measurements on a full-si...
At the request of the Bureau of Aeronautics, Navy Department, the National Advisory Committee for Ae...