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#201 | |
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Join Date: March 2, 2014
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When flying a glider close to the surface on a mountain ridge the glider pilot often turns back into the ridge in order to work the the uplifted air next to the ridge. on the leg flying towards the ridge, the glider's airspeed will remain unchanged (unless the glider pilot deliberately changes it) but because the glider is flying with a tailwind, the pilot's reference to the ground rushing by can trick him into believing he is flying very fast, and because the ground reference is moving by fast it seems like the control input to roll the glider is having no effect. In reality, the glider is rolling and turning just as it would into the wind, but because the terrain is looming fast and a collision is imminent if the turn isn't completed, the pilot can erroneously increase pitch believing that it will slow the glider down relative to the ground and better coordinate the turn. That often just makes matters worse because this can put the glider or the glider's wing into an incipient stall. I've known pilots who have died because of this.
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"Everyone speaks gun."--Robert O'Neill I am NOT an expert--I do not have any formal experience or certification in firearms use or testing; use any information I post at your own risk! Last edited by stagpanther; January 22, 2024 at 11:59 AM. |
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#202 | |
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Join Date: January 13, 2018
Posts: 1,520
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If you look at the math of the ballistic coefficient currently used to explain bullet behavior it is easy to see the enormous shortcomings of the system. BC is the mathematical equivalent of hand tools and levers. That is not to say you cannot do great things with hand tools and levers, just look at the engineering works of Rome. BC is accurate but not precise. As our wind tunnel technology advances into the realm of compressible aerodynamics and our Computational Fluid Dynamics models become more accurate I think BC will go the way of the sundial in predicting bullet behavior as CFD based computations will be more accurate and precise. |
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#203 | |
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Join Date: January 13, 2018
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You can see the concepts we discussed in this solver:
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I am going to borrow Unclenicks excellent illustration: The path of the bullet thru the air is the same regardless of wind. In this case, we are using a "zero value" headwind and tailwind which nicely illustrates the fact the bullet does not feel the wind in flight. At 400 yards our bullet drop is 354.9 inches. In a zero wind situation if we move the target close along the ground our bullet drop will be less. Subsequently if we move the target farther away along the ground in a zero wind situation, our bullet drop will increase. Since the bullet does not feel the wind but is inside a moving volume of air the movement of that air will effect the impact of an object that is not moving with that air and on the ground. We have a "Compound Frame of Reference" problem. Our headwind is a volume of air moving AWAY from the target. The bullet moves with that air experiencing the same aerodynamic forces it felt in the zero wind situation. Just like the passenger on a train, the bullet moves with the volume of air that is moving away from a point relative to the ground that is the target. We see the result is a larger value of bullet drop at 361.1 inches. We would get the same effect in the zero wind situation of we moved the target on the ground farther away. In the tail wind situation our volume of air is moving TOWARDS the target. The bullet moves with that air experiencing the same aerodynamic forces it felt in the zero wind situation. Just like the passenger on a train, the bullet moves with the volume of air the bullet is traveling in and is moving towards a point relative to the ground that is the target. We see the result is a smaller value of bullet drop at 349.2 inches. We would get the same effect in the zero wind situation of we moved the target on the ground closer. |
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#204 | |
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Join Date: February 12, 2001
Location: DFW Area
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#205 |
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Join Date: September 28, 2013
Posts: 4,854
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Sorry I haven't been following the "aviation model" discussions till now. I wouldn't think it is applicable to flight of bullet though, i.e. the bullet does feel the wind.
Pilot flies his plane by maintaining certain air speed, regardless the wind. With that, the plane indeed doesn't feel the wind. The ground speed is vector sum of this heading and the wind direction, which is varying with the wind. This method makes sense as it makes the pilot's job much easier. The plane is assumed to have unlimited source of energy to maintain its flight path. A bullet cannot maintain air speed. Actually its air speed is the apparent wind, which is vector difference of its velocity and the wind's velocity. So it always feels the wind. I was a private pilot myself in my previous life. When I got into the more affordable hobby of firing guns, I also use this method, thinking the bullet is just a flying object moving with the air mass. I lost quite some number of hairs when I read books on external ballistics. It took a bit of efforts to knock the old habits. Going back to wind deflection. W=Vw * Tlag =Vw * (TOF - D/Vo) W: wind deflection Vw: cross wind speed D: target distance Vo: bullet's MV If the bullet moves with the air mass, the wind deflection would have been W=Vw*TOF which is incorrect. -TL Sent from my SM-N960U using Tapatalk |
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#206 |
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Join Date: March 2, 2014
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I'm just playing devil's advocate, and not arguing the physics of it (way over my head), just a logic thing based on my "boots on the ground" experience.
![]() Except when the value of crosswind is equal to 0--in nature it is almost never a constant velocity, nor at a constant angle, that it is being "felt" or "pushed" at. How does this model account for that?
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"Everyone speaks gun."--Robert O'Neill I am NOT an expert--I do not have any formal experience or certification in firearms use or testing; use any information I post at your own risk! |
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#207 |
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Join Date: June 17, 2010
Location: Virginia
Posts: 7,163
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Which is why I always wondered how BC played a part in drift calculations
(since BC is frontal, not side angle) |
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#208 | ||||||
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Join Date: January 13, 2018
Posts: 1,520
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Quote:
What I said yesterday is still true today: Quote:
In the Relative Wind, the bullet does not feel the Ground Frame Reference wind and acts exactly like any other aerial vehicle. The very Definition of Relative Wind is "The Speed and Direction of Air impinging on a body passing thru it. It is equal and opposite in direction to the flight path velocity" A bullet does not feel the same wind you and I do on the ground, it only feels the Relative Wind and it moves thru a volume of air as a part of that volume of air until it encounters the target or the ground. Quote:
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In an M24 SWS, One click to the right at a target 500 meters or more tells me where the bullet will be due to spindrift but it tells me nothing about what caused it to be there. That click is your math in action. Your Tlag is a ratio of a theoretical flight thru a vacuum and the actual flight. So there is some very simplistic aerodynamics that gets covered up in late 17th Century math. Your formula lumps everything into a crude ratio to approximate a prediction not on what the forces are acting on the bullet are doing but where the bullet will be..... It is not the math for telling you what is going on but rather the math to tell you where it will be.... Quote:
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From the Frame of Reference of the ground, the trajectory is different. From the Frame of Reference of the Air the trajectory is the same and since the volume of air is moving.... the bullet strikes the target at a different point along that same trajectory. Last edited by davidsog; January 23, 2024 at 06:44 PM. |
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#209 | |
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Join Date: January 13, 2018
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It is a tool to cobble crude math and pound it into a shape that delivers results that approximate reality. It tells you nothing about the forces acting upon that bullet. It fills a similar role as Equivalent Flat Plate does but the two are not directly comparable. EFP is much more accurate when used correctly. Last edited by davidsog; January 23, 2024 at 05:48 PM. |
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#210 |
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Join Date: June 17, 2010
Location: Virginia
Posts: 7,163
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I still don't see (in any way) how a frontal BC has any effect on side impact fluid flow.
Perhaps someone can shed light on that ? |
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#211 | |
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Join Date: January 13, 2018
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It is a reference area to approximate and represent the shape. The math corrects itself when describing motion as energy cannot be created or destroyed. I know that sounds confusing. Aircraft Performance math uses the area of the wing to describe Lift, drag, and aircraft motion. External Ballistics uses a method first developed in the late 1600's of using a ratio of theoretical bullet behavior to measured bullet. Yes, it is a super confusing set of formulas that skirts the edges of actual Aerodynamics because it is rooted in a time when Aerodynamics was poorly understood. It works because it is based on conservation of energy too. It is not exact but it gives an approximation. |
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#212 |
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Join Date: January 13, 2018
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This might help.
Frame of Reference is a very important concept to understand if we are to understand what our bullet is doing. As we sit at our computers, We are all passengers on a train moving at approximately 1.3 million miles per hour. If you add all the motion of the earth, the Solar system, and the Milky Way Galaxy we are in constant motion at over 1 million mph. We don't' perceive that motion because everything in our evolution has adapted us to be creatures of the earth. Once the bullet leaves the barrel, it becomes a creature of the air. The only thing it feels is the Relative Wind and that is NOT wind you and I experience. It does not feel the wind you and I experience. Last edited by davidsog; January 23, 2024 at 07:40 PM. |
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#213 | |
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Join Date: September 28, 2013
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It is not my formulation. It is result of solving system of 3D differential equations, and has been proven by experiments of all sorts. We are entitled to our opinions, but I'm not quite ready to call generations of ballisticians obselete just yet, some of them are still with us today. -TL Sent from my SM-N960U using Tapatalk |
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#214 | |
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Join Date: January 13, 2018
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#215 | |
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Join Date: January 13, 2018
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It is two different things and two different questions. For almost half the history of Aviation we did not have to answer the same question. It was not until the 1940's that the speed and power of aircraft reached a point stability and control performance was necessary or even a science beyond the basics. Up until then, pilots flew aircraft routinely with stability and control characteristics that would be deadly in todays aircraft. We haven't had the tools to dissect the external ballistic problem much further nor any real need too. That is changing as our tools become much more refined and our understanding more complete. |
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#216 | |
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Join Date: June 17, 2010
Location: Virginia
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(But) that BC aspect will go as the cosine of wind impact angle -- effectively decreasing to zero/no role as wind reaches 90°, and defection maximizes. |
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#217 | |
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Join Date: January 13, 2018
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I see what you are asking. In regards to sideforce calculation the reference area remains the same "frontal aspect" just like it remains wing area most commonly in Aircraft Performance. That sideforce is what rotates the bullet about its CG to align with the Relative Wind the moment it leaves the barrel. We don't need to know the exact area of the side profile of the bullet as the math will compensate. Energy cannot be created or destroyed and if we know the given force input we will get a good approximation of the output. It won't be the exact same forces on the actual aerial vehicle but the result of those forces will be the same. Understand? It's a confusing concept and one Aerodynamics Professors spend some time on when introduced in class, lol. Last edited by davidsog; January 23, 2024 at 10:51 PM. |
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#218 | ||
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#219 |
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I think what David is trying to say is that once an object becomes "detached" from the surface of the earth it becomes behaviorally influenced by the atmosphere--which really is dynamic and is much more like water in an ocean than a vacuum or uniform element. As shooters--or anyone on the surface--our frame of reference is "anchored" to observations and interpreted relative to our being on surface. But once we or any object is launched into the air the reference becomes "anchored" to the movement of the air masses it's entrained in.
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"Everyone speaks gun."--Robert O'Neill I am NOT an expert--I do not have any formal experience or certification in firearms use or testing; use any information I post at your own risk! |
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#220 |
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Join Date: January 13, 2018
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That's it Stagpanther. Just like a passenger on a train does not feel the movement of the train, the bullet does not feel the movement of the volume of air it is in.
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#221 | |
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Unless the air and the bullet are equilibrium as far as relative motion, both perceive the motion of the other. In the case of forward motion, equilibrium never happens In the case of lateral deflection, equilibrium would only happen if/when the bullet finally assumes the same lateral speed as the lateral wind speed vector. (which for practical purposes, is again never) (Am I missing something here?) Last edited by mehavey; January 24, 2024 at 06:06 PM. |
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#222 | ||||
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Just like an airplane does not feel "turbulence" as it is a torque on the CG and not a positional jump...the bullet is the same. Quote:
Last edited by davidsog; January 24, 2024 at 02:35 PM. |
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#223 | ||
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Join Date: January 13, 2018
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With a bullet, the only axis not in equilibrium is the drag axis. All other axis achieve equilibrium. Aerodynamically, it is exactly like a glider shot into the sky with a rubber band. Granted, a glider with very poor wings and powerful rubber band but the physics is the exact same. |
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#224 |
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We need to be careful about describing the bullet as moving together with the volume of air. If it did that, wind deflection would be calculated as the time of flight times the wind speed. Bullets don't deflect nearly that far. Instead, the fact there is constant drag on the bullet throughout its trip to the target shows it has a significant speed differential with respect to the air. It does, however, deflect in the direction of the air. In that sense, its slowing speed is a rearward deflection, of which wind deflection is a vector component.
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#225 | |
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Join Date: September 28, 2013
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But Mr Sog believes we have entered a brand new era that all the classical results in ballistics have become obselete. -TL Sent from my SM-N960U using Tapatalk |
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