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Way too much everything for me (cost, barrel burner, recoil, etc), but if you are going to get serious about ELR, then it may be a good option.
Agreed, too much for me as well. I don't shoot competitive ELR, so this doesn't move the needle for me. Way too much expense for casual shooting. 338 Lapua AI more than scratches my itch for heavy artillery.
What are the arguments for choosing an 37XC over a 375 Cheytac? Performance seems to be comparable. Peterson makes brass for both. Cheytac already has a strong ELR following and lots of industry support. Just curious why someone would choose an XC over a Cheytac.
. . . The reason Dave developed his new case is the Cheytac case was designed for the .408 and at .375 it is way overbore and u end up with a cartridge that has a low fill ratio with higher peak pressures. So, overbore, poor fill ratio, and high chamber pressure all lend themselves to less chance of broad stable nodes which equate to high ES and SD equalling poor accuracy at range. His goal was to design a cartridge with perfect fill ratio for .375 that's optimized for modern powders like H1000 that are less temp sensitive trying to get the best ES/SD
Let's see, intial development for the .338 Lapua was done in the US using a shortened .416 Rigby case. The principles abandoned development due to personal conflicts and it was subsequently picked up and finished by Lapua. The case was made stouter to enable higher pressures. So it looks like the new case is essentially a lengthened Rigby with (if I read it right, haven't seen a drawing) a case length of 3.139" vs the 2.90 of the parent Rigby case.
Probably fifty year back my old man knew a couple of guys playing with necking down the Rigby case. The only problem is the old Rigby cases were balloon heads (like original .220 Russian cases)and couldn't be loaded especially hot. Nor were the slow powders of today available.
Still, gotta give "El Reye" (David) credit for bringing it to market. It takes a sizable investment and big brass ones to bring a propriety cartridge to market as an individual. Fair amount of risk is assumed with any new venture but if anyone can pull it off. As it turns out I have a suitable action laying about and had been thinking of wildcatting a Rigby anyhow as some of the new brass wasn't old style balloon head. Hmmm.
Actually, I believe the XC case is a bit wider than the Rigby. Somewhere around .6" width at the base and using a rebated rim, I suspect the the base width is closer to the .378 Wby width measured at the belt.
Rigby - .589 rim, .590 base so if the Rigby wasn't the parent, I believe it at least provided a template
Although this is designed for ELR, I think this would make for a great bear, elk or safari gun if we could only could get a longer mag action.
Probably. The big CZ Safari action will handle a full length Rigby which would be suitable using conventional hunting bullets. Seems to me there used to be a European more or less standardized .375/.416 many years ago. Pre WWII?
Maybe we could coax Peterson or ADG to make a higher pressure capable version of the Rigby case available.....?
Any ideas on how the 33XC compares to the .338 Lapua Imp?
So Dave,here's the 33XC
So Dave,
Please correct me if I'm wrong but looking at the chamber print it appears that the cartridge is no longer a rebated design but basically a longer version of a 338 Lapua?
Great design! Seems like it would be a perfect fit for the Surgeon XL single feed action....
I will eventually rechamber my 338LM Surgeon XL rifle's Schneider 7.0-inch twist barrel for his Peterson 33XC brass. I also have in hand a Bartlein 5R 338 barrel with 6.6-inch twist (20 calibers per turn). The 33XC should be better than Lapua all the way around.
Hi,
@Lofty
Check the hyper-stabilization paper from Jim that is in the resource section here on the hide. It explains the fast twist rates better than any post can
Jim has his own projectile design also.
Sincerely,
Theis
Based on the 33XC velocities printed above with the 256 Flatline, it looks to be about 100-150fps faster than a Lapua Improved.
I shot Mr. Tubb's ( Purely out of respect for what David has accomplished ) 33 XC rifle on Sunday afternoon at the Precision Rifle Expo.
Lowlight's video interview gave me more insight into what was going on and some of the technology David is utilizing. I wish I had seen it before going to GA. so that I would have paid a bit more attention while I was up close and personal with him, the rifle and the ammo.
The rifle was impressive to shoot, in terms of recoil management with the brake and weight and accuracy. I did manage a sub MOA group at 1000 yards my first time firing the rifle.
The 33XC is the logical choice for anyone wanting a bit more performance over the 338LM. All that is necessary is to punch out the chamber and get a set of reloading dies. Given the cartridge length increase the 33XC will be a single load proposition in Lapua sized rifles. At the Precision Rifle Expo David and me ran several tests for bullet BC uniformity with ringed vs. non ringed bullets. The 33XC loads we shot were 300gr bullets at 3175fps. This setup shoots pretty flat, about 10 mils at 1500 yards in dense South GA air.
Theis,
We did not shoot 1500 yards while at Blakely. All the shooting we did was at 1000 yards. I was only using 1500 yards as a reference point for 10 mils of elevation with the 33XC combination. We were testing some 300gr bergers and some solids. We also did a good bit of testing with the Sierra DTAC 115gr bullet running 3200fps.
EJ
David Tubb's idea of ringing the noses of long-range rifle bullets is great for any bullets designed with tangent ogives, any multi-ogive bullets, and any secant-ogive bullets having RT/R ratios greater than about 0.5. This "turbulator" ring serves aerodynamically to "trip" the initially laminar flow boundary layer into turbulent flow at that ring location. The reason secant ogives with RT/R=0.5 fly so well is that they have a 4.75 to 5.0-degree "break angle" in the surface of the bullet where the base of the ogive joins the cylindrical shank of the bullet which reliably trips the boundary layer flow-fields at that location, at least for "small caliber" bullets. Thus, the lower skin-friction (drag) of laminar boundary layer flow pertains over the entire length of the secant ogive nose, but higher-drag turbulent flow reliably pertains over the afterbody of the bullet. This is how VLD rifle bullets fly.
Tangent ogive bullets meet the bullet shank with zero-degree break angles. Except for really small-caliber (<22 caliber), very short length, tangent ogive rifle bullets, Reynolds Number constraints inevitably cause fairly random axial-location tripping of the laminar flow into turbulent flow due to microscopic surface irregularities. This then causes small random variations in air drag from one shot to the next and destabilizes individual bullets in flight. The effect is similar to the attached versus detached flow aerodynamic effects which disrupt the trajectories of low-speed baseballs, etc. A conical ogive (RT/R=0) has the largest possible break angle for any given nose length without considering concave nose shapes. The 4.75-degree break angle of VLD bullets is large enough to guarantee tripping of the boundary layer at the typical nose lengths used for bullets up to about 20 mm in caliber. Doubling that angle with a conical nose design would have no additional benefit. All of the multi-ogive designs which I can imagine would produce several smaller break angles in the surface which might not cause reliable tripping of the boundary layer.
So, ring the noses of tangent-ogive Sierra MK's and Berger multi-ogive bullets, but not those of true VLD bullets nor of my prototype ULD bullets. I would suggest, however, based on Reynolds Numbers, ringing tangent-ogive rifle bullets at about 1-inch behind their noses for reliable boundary layer tripping with slightly less air-drag penalty.
Jim Boatright
David Tubb's idea of ringing the noses of long-range rifle bullets is great for any bullets designed with tangent ogives, any multi-ogive bullets, and any secant-ogive bullets having RT/R ratios greater than about 0.5. This "turbulator" ring serves aerodynamically to "trip" the initially laminar flow boundary layer into turbulent flow at that ring location. The reason secant ogives with RT/R=0.5 fly so well is that they have a 4.75 to 5.0-degree "break angle" in the surface of the bullet where the base of the ogive joins the cylindrical shank of the bullet which reliably trips the boundary layer flow-fields at that location, at least for "small caliber" bullets. Thus, the lower skin-friction (drag) of laminar boundary layer flow pertains over the entire length of the secant ogive nose, but higher-drag turbulent flow reliably pertains over the afterbody of the bullet. This is how VLD rifle bullets fly.
Tangent ogive bullets meet the bullet shank with zero-degree break angles. Except for really small-caliber (<22 caliber), very short length, tangent ogive rifle bullets, Reynolds Number constraints inevitably cause fairly random axial-location tripping of the laminar flow into turbulent flow due to microscopic surface irregularities. This then causes small random variations in air drag from one shot to the next and destabilizes individual bullets in flight. The effect is similar to the attached versus detached flow aerodynamic effects which disrupt the trajectories of low-speed baseballs, etc. A conical ogive (RT/R=0) has the largest possible break angle for any given nose length without considering concave nose shapes. The 4.75-degree break angle of VLD bullets is large enough to guarantee tripping of the boundary layer at the typical nose lengths used for bullets up to about 20 mm in caliber. Doubling that angle with a conical nose design would have no additional benefit. All of the multi-ogive designs which I can imagine would produce several smaller break angles in the surface which might not cause reliable tripping of the boundary layer.
So, ring the noses of tangent-ogive Sierra MK's and Berger multi-ogive bullets, but not those of true VLD bullets nor of my prototype ULD bullets. I would suggest, however, based on Reynolds Numbers, ringing tangent-ogive rifle bullets at about 1-inch behind their noses for reliable boundary layer tripping with slightly less air-drag penalty.
Jim Boatright
Jim,
Would you be willing to explain laminar flow vs. turbulent flow? I am picturing laminar as layered like an onion and turbulent as erratic and multi-directional. Are the results being seen with the "turbulator" ring specifically less vertical dispersion or less generalized dispersion? The reason I ask, ....are the results being seen from tripping the laminar flow into turbulent simply creating less friction/drag, through low pressure, over the area of the bullet with the most surface area--i.e creating more consistent MV's down range at target? Or is their possible effects of less aerodynamic jump--i.e. less weather vaning?
If my memory serves me right, when I talked to Dave, he was specifically seeing less vertical dispersion with the ring.
So this would place the ring right in front of the ogive/body junction? What is the effect of having the ring break up the laminar air flow so close to the ogive/body junction vs placing the ring further forward on the ogive?No, I meant to recommend placing the ring about 1 inch from the tip of the bullet. The maximum distance over which the boundary layer flow can remain laminar is about 1.25 to 1.50 inches, depending upon what value the "critical Reynolds Number" turns out to have. McCoy says one can safely assume laminar flow over the ogive (nose) and turbulent flow over the afterbody (or L/T flow transition skin friction drag) for rifle bullets up to about 20 mm in diameter.