The theory developed by H. Wagner for the computation of the landing impact on water for a rigid float is extended to include elastic floats by introducing the concept of an equivalent rigid bottom to substitute for the actual elastic bottom
ABSTRACTWing-in-Ground vehicles and aerodynamically assisted boats take advantage of increased lift ...
The extent of agreement of the theoretical impact computations with the actual phenomenon has not as...
This report gives the results of wind-tunnel tests with a seaplane model as a contribution to the so...
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...
This report begins with a brief resume of a theoretical consideration and its results. Then a descri...
For floats and hulls having V bottoms the impact force does not necessarily increase with increasing...
This report presents experiments and calculations for the purpose of determining the landing gear re...
The present investigation is an endeavor to express the jolting stresses, designated as landing impa...
This is the second of a series of investigations to determine water pressure distribution on various...
Tests were conducted to investigate the possibility of a serious accident arising from unintentional...
The previously employed method of extrapolating the total resistance to full size with lambda(exp 3)...
An analysis of available theory on seaplane impact and a proposed modification thereto are presented...
The investigation presented in this report was conducted for the purpose of determining the distribu...
An analytical method is presented for calculating the hydrodynamic impact loads and motions experien...
ABSTRACTWing-in-Ground vehicles and aerodynamically assisted boats take advantage of increased lift ...
The extent of agreement of the theoretical impact computations with the actual phenomenon has not as...
This report gives the results of wind-tunnel tests with a seaplane model as a contribution to the so...
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...
This report begins with a brief resume of a theoretical consideration and its results. Then a descri...
For floats and hulls having V bottoms the impact force does not necessarily increase with increasing...
This report presents experiments and calculations for the purpose of determining the landing gear re...
The present investigation is an endeavor to express the jolting stresses, designated as landing impa...
This is the second of a series of investigations to determine water pressure distribution on various...
Tests were conducted to investigate the possibility of a serious accident arising from unintentional...
The previously employed method of extrapolating the total resistance to full size with lambda(exp 3)...
An analysis of available theory on seaplane impact and a proposed modification thereto are presented...
The investigation presented in this report was conducted for the purpose of determining the distribu...
An analytical method is presented for calculating the hydrodynamic impact loads and motions experien...
ABSTRACTWing-in-Ground vehicles and aerodynamically assisted boats take advantage of increased lift ...
The extent of agreement of the theoretical impact computations with the actual phenomenon has not as...
This report gives the results of wind-tunnel tests with a seaplane model as a contribution to the so...