I'm trying to reduce the amount of fin flex on landing (it's causing hairline cracks in the paint along the fillet) by reducing the size of the fin's trailing end. I started by chopping off 1.25" in OpenRocket, then running simulations that would indicate any reduction in stability, focusing on plots that include pitch rates.
Below are screen shots of the rocket with the unmodified fins. The first is the rocket profile in OR, showing a stability of 1.47 calibers. Next to it are plots with pitch rates—the first deviation being ~21.5 degrees.
Next, screen shots of the modified fins with 1.25" cut off the trailing ends. The stability has decreased to 1.41 calibers, with a pitch rate of ~21 degrees—a slight improvement.
Then I ran simulations with the fins shortened enough to allow the motor nozzle to extend below the trailing edges, thereby absorbing some of the landing impact. I also trimmed the corner of the trailing edge, thinking this might help absorb ground impact by tipping the rocket onto its side quicker than it would with a flat-bottomed fin.
The stability dropped to 1.38 (still good), with a significant reduction in pitch rate—down to about 16.5 degrees.
Is that fin shape workable? OpenRocket tells me it is, but I'm reminded of OR's trouble modeling certain design aspects (unusual transitions or stubby fins up by the nose cone come to mind). I'd hate to cut these fins down, thinking the design will be stable, only to have it do somersaults right off the rail.
I appreciate any input I can get—advice, criticism, suggestions. Thanks in advance.
Below are screen shots of the rocket with the unmodified fins. The first is the rocket profile in OR, showing a stability of 1.47 calibers. Next to it are plots with pitch rates—the first deviation being ~21.5 degrees.
Next, screen shots of the modified fins with 1.25" cut off the trailing ends. The stability has decreased to 1.41 calibers, with a pitch rate of ~21 degrees—a slight improvement.
Then I ran simulations with the fins shortened enough to allow the motor nozzle to extend below the trailing edges, thereby absorbing some of the landing impact. I also trimmed the corner of the trailing edge, thinking this might help absorb ground impact by tipping the rocket onto its side quicker than it would with a flat-bottomed fin.
The stability dropped to 1.38 (still good), with a significant reduction in pitch rate—down to about 16.5 degrees.
Is that fin shape workable? OpenRocket tells me it is, but I'm reminded of OR's trouble modeling certain design aspects (unusual transitions or stubby fins up by the nose cone come to mind). I'd hate to cut these fins down, thinking the design will be stable, only to have it do somersaults right off the rail.
I appreciate any input I can get—advice, criticism, suggestions. Thanks in advance.
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