Hi:
I looking for help in this matter:
In my horizontal tail load calculation I have decided to use Appendix "A" chapter A23:11
c)Surface loading conditions. Each surface loading condition must be investigated as follows:
(1) Simplified limit surface loadings for the horizontal tail, vertical tail, aileron, wing flaps, and trim tabs are specified in figures 5 and 6 of this appendix.
The question is : The "Average Surface Loading" obtained via fig. A5 is all I need? or I must add to the Balancing Loads.
Best regards.
I looking for help in this matter:
In my horizontal tail load calculation I have decided to use Appendix "A" chapter A23:11
c)Surface loading conditions. Each surface loading condition must be investigated as follows:
(1) Simplified limit surface loadings for the horizontal tail, vertical tail, aileron, wing flaps, and trim tabs are specified in figures 5 and 6 of this appendix.
The question is : The "Average Surface Loading" obtained via fig. A5 is all I need? or I must add to the Balancing Loads.
Best regards.
