ESTIMATION OF A CRITERION OF LOAD TO WHICH A STRUCTURAL COMPONENT OF AN AIRCRAFT IS SUBJECTED, AND ASSISTANCE FOR THE DETECTION OF A SO-CALLED "HARD" LANDING BY VIRTUE OF SUCH A CRITERION - diagram, schematic, and image 04
Back to ESTIMATION OF A CRITERION OF LOAD TO WHICH A STRUCTURAL COMPONENT OF AN AIRCRAFT IS SUBJECTED, AND ASSISTANCE FOR THE DETECTION OF A SO-CALLED HARD LANDING BY VIRTUE OF SUCH A CRITERION , All Patents .