I'm in the middle of a project for my university to design a low altitude (10,000ft) rocket. My role is the 'fin aerodynamics' portion of the rocket. I'm struggling to evaluate which fin shape and cross section is actually the best for any specific rocket case (mine is subsonic, M~0.8) for my report. I've found very conflicting results, and most of the literature is on aircraft wings/fins, which are much higher aspect ratio than rocket fins.
From what I've gathered so far, a trapezoid or clipped delta seems to be the best for this case, but I can't really explain why. Swept wings bring back the aerodynamic centre so the rocket becomes more stable but less manoeuvrable? Rectangular wings have the highest induced drag and lowest lift coefficient? Elliptical wings have low induced drag but low lift coefficient? I'm not even sure how to calculate lift coefficients for rocket fins because of their low aspect ratio.
Any tips on textbooks, papers or reports giving a bit more detailed information on fin planform shapes would be fantastic. What's more, our rocket will have static rear fins but active canard fins, which makes things more complex (albeit more interesting). Any help would be greatly appreciated!
From what I've gathered so far, a trapezoid or clipped delta seems to be the best for this case, but I can't really explain why. Swept wings bring back the aerodynamic centre so the rocket becomes more stable but less manoeuvrable? Rectangular wings have the highest induced drag and lowest lift coefficient? Elliptical wings have low induced drag but low lift coefficient? I'm not even sure how to calculate lift coefficients for rocket fins because of their low aspect ratio.
Any tips on textbooks, papers or reports giving a bit more detailed information on fin planform shapes would be fantastic. What's more, our rocket will have static rear fins but active canard fins, which makes things more complex (albeit more interesting). Any help would be greatly appreciated!