Add to ORKGAn analytical study of the effects of wing flexibility on wing strains due to gusts has been made for four spanwise stations of a four-engine bomber airplane, and the results have been correlated with results of a previous flight investigation
An investigation was made in the Langley gust tunnel of a flexible-wing model with the semichord lin...
A series of calculations of the dynamic response of airplane wings to gusts were made with the purpo...
Comprehensive aeroelastic analyses and wind tunnel tests have been conducted on a model of a typical...
Studies made to evaluate the influence of wing bending flexibility on the structural response to gus...
An analysis is made of the structural response to gusts of an airplane having the degrees of freedom...
A flight investigation was made on a large sweptback-wing bomber airplane and the results are compar...
Some results on the effects of wing flexibility on wing bending strains as determined from flight te...
An analytical study of the effects of wing flexibility on wing strains due to gusts has been made fo...
An analysis is made of the structural response to gusts of an airplane having the degrees of freedom...
Some results on the effects of wing flexibility on wing bending strains as determined from flight te...
Results are given of an analysis of wing and horizontal-tail spar strains measured on a twin-engine ...
Wind-tunnel tests are described, in which the angle of attack of a wing model was suddenly increased...
An evaluation of the effect of structural flexibility in aircraft loads is presented. The assessmen...
This project presents work performed by the Institute of Aerospace Engineering, Brno University of T...
This report gives the results of a detailed study of the flutter characteristics of four representat...
An investigation was made in the Langley gust tunnel of a flexible-wing model with the semichord lin...
A series of calculations of the dynamic response of airplane wings to gusts were made with the purpo...
Comprehensive aeroelastic analyses and wind tunnel tests have been conducted on a model of a typical...
Studies made to evaluate the influence of wing bending flexibility on the structural response to gus...
An analysis is made of the structural response to gusts of an airplane having the degrees of freedom...
A flight investigation was made on a large sweptback-wing bomber airplane and the results are compar...
Some results on the effects of wing flexibility on wing bending strains as determined from flight te...
An analytical study of the effects of wing flexibility on wing strains due to gusts has been made fo...
An analysis is made of the structural response to gusts of an airplane having the degrees of freedom...
Some results on the effects of wing flexibility on wing bending strains as determined from flight te...
Results are given of an analysis of wing and horizontal-tail spar strains measured on a twin-engine ...
Wind-tunnel tests are described, in which the angle of attack of a wing model was suddenly increased...
An evaluation of the effect of structural flexibility in aircraft loads is presented. The assessmen...
This project presents work performed by the Institute of Aerospace Engineering, Brno University of T...
This report gives the results of a detailed study of the flutter characteristics of four representat...
An investigation was made in the Langley gust tunnel of a flexible-wing model with the semichord lin...
A series of calculations of the dynamic response of airplane wings to gusts were made with the purpo...
Comprehensive aeroelastic analyses and wind tunnel tests have been conducted on a model of a typical...