Add to ORKGThe theory of landing impact is briefly stated and the applicability of a previously suggested formula is extended. Theoretical considerations regarding impact measurements on models and actual seaplanes are followed by a brief description of the instruments used in actual flight tests. The report contains a description of the strength conditions and deals exhaustively with force measurements on the float gear of an "HE 9a" with flat-bottom and with V-bottom floats. The experimental data are given and compared with the theoretical results
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...
The models, apparatus, and instrumentation developed for investigations of the rough-water character...
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 ...
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...
The extent of agreement of the theoretical impact computations with the actual phenomenon has not as...
An analysis of available theory on seaplane impact and a proposed modification thereto are presented...
For floats and hulls having V bottoms the impact force does not necessarily increase with increasing...
An analytical method is presented for calculating the hydrodynamic impact loads and motions experien...
Powered models of three different flying boats were landed in oncoming waves of various heights and ...
An analysis of available theory on seaplane impact and a proposed modification thereto are presented...
A smooth-water-landing investigation was conducted with a small seaplane to obtain experimental wing...
Experimental data, such as the results of tank tests of models, render it possible to predict, at le...
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...
The models, apparatus, and instrumentation developed for investigations of the rough-water character...
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 ...
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...
The extent of agreement of the theoretical impact computations with the actual phenomenon has not as...
An analysis of available theory on seaplane impact and a proposed modification thereto are presented...
For floats and hulls having V bottoms the impact force does not necessarily increase with increasing...
An analytical method is presented for calculating the hydrodynamic impact loads and motions experien...
Powered models of three different flying boats were landed in oncoming waves of various heights and ...
An analysis of available theory on seaplane impact and a proposed modification thereto are presented...
A smooth-water-landing investigation was conducted with a small seaplane to obtain experimental wing...
Experimental data, such as the results of tank tests of models, render it possible to predict, at le...
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...
The models, apparatus, and instrumentation developed for investigations of the rough-water character...