In order to make a stress analysis of seaplane floats, and especially of the members connecting the floats with the fuselage, it is of great importance to determine the maximum pressure acting on the floats during landing. Here, the author gives a formula for maximum pressures during landing that permits one to apply experimental results to different bodies and different velocities. The author notes that the formula checks very well with experimental results
An analytical method is presented for calculating the hydrodynamic impact loads and motions experien...
This report contains the results of tank tests carried out at free trim on seventeen hulls and float...
Powered models of three different flying boats were landed in oncoming waves of various heights and ...
In order to make a stress analysis of seaplane floats, and especially of the members connecting the ...
The theory of landing impact is briefly stated and the applicability of a previously suggested formu...
The present investigation is an endeavor to express the jolting stresses, designated as landing impa...
In order to make a stress analysis of seaplane floats, and especially of the members connecting the ...
This report begins with a brief resume of a theoretical consideration and its results. Then a descri...
The investigation presented in this report was conducted for the purpose of determining the distribu...
For floats and hulls having V bottoms the impact force does not necessarily increase with increasing...
An analysis of available theory on seaplane impact and a proposed modification thereto are presented...
The theory developed by H. Wagner for the computation of the landing impact on water for a rigid flo...
This is the second of a series of investigations to determine water pressure distribution on various...
This report gives the results of wind-tunnel tests with a seaplane model as a contribution to the so...
The extent of agreement of the theoretical impact computations with the actual phenomenon has not as...
An analytical method is presented for calculating the hydrodynamic impact loads and motions experien...
This report contains the results of tank tests carried out at free trim on seventeen hulls and float...
Powered models of three different flying boats were landed in oncoming waves of various heights and ...
In order to make a stress analysis of seaplane floats, and especially of the members connecting the ...
The theory of landing impact is briefly stated and the applicability of a previously suggested formu...
The present investigation is an endeavor to express the jolting stresses, designated as landing impa...
In order to make a stress analysis of seaplane floats, and especially of the members connecting the ...
This report begins with a brief resume of a theoretical consideration and its results. Then a descri...
The investigation presented in this report was conducted for the purpose of determining the distribu...
For floats and hulls having V bottoms the impact force does not necessarily increase with increasing...
An analysis of available theory on seaplane impact and a proposed modification thereto are presented...
The theory developed by H. Wagner for the computation of the landing impact on water for a rigid flo...
This is the second of a series of investigations to determine water pressure distribution on various...
This report gives the results of wind-tunnel tests with a seaplane model as a contribution to the so...
The extent of agreement of the theoretical impact computations with the actual phenomenon has not as...
An analytical method is presented for calculating the hydrodynamic impact loads and motions experien...
This report contains the results of tank tests carried out at free trim on seventeen hulls and float...
Powered models of three different flying boats were landed in oncoming waves of various heights and ...