Author: Donald E. Hewes
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 36
Book Description
Free-flight Investigation of Radio-controlled Models with Parawings
Author: Donald E. Hewes
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 36
Book Description
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 36
Book Description
Gust-tunnel Investigation of a Flexible-wing Model with Semichord Line Swept Back 45°
Author: Thomas D. Reisert
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 20
Book Description
An investigation was made in the Langley gust tunnel of a flexible-wing model with the semichord line swept back 45 degrees to obtain experimental data on the amount of gust-load alleviation that might be expected as a result of the wings flexing under load. The results indicated that unless adverse pitching motion could be eliminated or reduced the over-all load reduction would be small. The net reduction in bending moment, however, may be appreciable.
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 20
Book Description
An investigation was made in the Langley gust tunnel of a flexible-wing model with the semichord line swept back 45 degrees to obtain experimental data on the amount of gust-load alleviation that might be expected as a result of the wings flexing under load. The results indicated that unless adverse pitching motion could be eliminated or reduced the over-all load reduction would be small. The net reduction in bending moment, however, may be appreciable.