voko
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Height in your case is y, not x. Good otherwise.
The discussion centers on calculating the trajectory of a glider performing a back-loop maneuver at an initial speed of 60 m/s and a centripetal acceleration of 30 m/s². Participants emphasize the application of Newton's second law and the relationship between lift force and velocity squared. The conversation highlights the importance of integrating second-order differential equations numerically to determine the position, velocity, and acceleration of the aircraft throughout the loop. Ultimately, the consensus is that the glider will complete the loop, returning to its original position and speed, assuming no air resistance.
PREREQUISITESAerospace engineering students, physics learners, and software developers working on simulations of flight dynamics will benefit from this discussion.
StudentTM said:Somebody suggested to me that
a_x = ( 30 (centripetal acceleration) * v * v_x1 ) / 60*60
a_y = (( 30 (centripetal acceleration) * v * v_y1 ) / 60*60 ) - 9,8
would be correct.
a_x = -39.8 * V_t * Vy_1 / (60 * 60);
a_y = 39.8 * V_t * Vx_1 / (60 * 60) - 9.8;
is wrong.
Sorry guys, for dummy question, I really respect your patience with me, but .. How can I learn to understand these final equation? Where to start?
But how do I know V_x is constant?
voko said:It is not constant. But when you integrate differential equations using Euler's method, you assume that during the very small time interval of each integration step, all your variables do not change appreciably. This is the source of the error intrinsic to the method. You should have been paying attention to your professor, this has certainly been explained in the class.