A static shape has a fixed relationship between all of its vertexes. A dynamic shape can vary the position of at least one of its vertexes in relation to the others.
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A static shape has a fixed relationship between all of its vertexes. A dynamic shape can vary the position of at least one of its vertexes in relation to the others.
Mass and damping are associated with the motion of a dynamic system. Degrees-of-freedom with mass or damping are often called dynamic degrees-of-freedom; degrees-of-freedom with stiffness are called static degrees-of-freedom. It is possible (and often desirable) in models of complex systems to have fewer dynamic degrees-of-freedom than static degrees-of-freedom.
Statistics refers to a mathematical analysis that deals with the collection and interpretation of data. Static can refer to a type of electricity, a lack of movement, or a crackling sound in a phone line.heck, I just want the definitions!
Static analysis can be seen as a stricter check of syntax made by an advanced compiler (that will not produce binary code but error messages). Dynamic analysis is a specific analysis done when the program is actually running. Thins kind of analysis, being done at runtime, can detect specific behaviors, like accessing deallocated memory, leaking memory, time spent in functions and so on. To put it roughly, is static analysis is advanced compilation, dynamic analysis is a particular form of testing that often requires your program to be "instrumented" for it (i.e., modified at the binary level). In Xcode, dynamic analysis is available through Instruments. You can found more information about it by googling for "xcode instruments tutorial". In short, you can run your program under dynamic analysis choosing "Running with Performance Tool" and choosing the kind of analysis you want to perform (memory leaks, memory allocation, performance, zombies, etc.). Instruments will show you in a graphical environment how memory usage evolves, or how long it takes for specific functions to perform, etc.
As we know the dynamic pressure over the wing is already weakened by the Skin friction drag, a further decrease in dynamic pressure ( e.g. due to adverse pressure gradient ) will cause the dynamic pressure to be lose further and a rise in static pressure. The loss of dynamic pressure will result in turbulent airflow over the wing to be increased and therefore the separation point to move forward. This will enhance the pressure difference between leading and trailing edge and therefore a more increase in Form Drag. So , further ahead the separation point towards leading edge, greater the Form drag.By , Karun :-)At your service ,have any doubts , let know at ,aviator161989@gmail.com