I don't remember that. I was but a young ENS, griping that, "that's not what I learned in my BSAE..."Didn’t the H60 Chapter 11 get rewritten around the same time by the same guy?
How interesting. I wonder if VRS could be generalized into a rule-of-thumb for each helo based on disc loading, diameter, and Nr (or something along those lines). I’m amazed someone hasn’t tested that- or have they?One thing that comes to mind is Vortex Ring State. The mindless caveat of < 40 kts and greater than 800 fpm rate of descent was regurgitated across every helo's NATOPS. From my understanding it was based on a single engine Huey from way back when.
Actual TPS dudes published charts that showed those numbers were not even close for a 53-E...but alas it never translated into our NATOPS while I was in.
Calling SevenHelmet...
(Yeah, I know you're not a Rotary Guy... but you have a lot of Nerdology knowledge, I figure)
VRS has a generalized/referred model. JJ taught it to us at TPS as an advanced topic at the end of helo perf. IIRC, it's just not quite as awesome at predictions as the rest of the perf models are.How interesting. I wonder if VRS could be generalized into a rule-of-thumb for each helo based on disc loading, diameter, and Nr (or something along those lines). I’m amazed someone hasn’t tested that- or have they?
Up and ready! But rotary aero is… different. I understand a lot of the concepts, but a powered-lift V-speed buildup is definitely in the category or “ask an expert” for me.
So the problem is one needs some advanced engineering knowledge to really understand helicopter aerodynamics and most of the Army IPs don't have it...? Do the IPs of the Navy/Marine Corps/Air Force have it or is this an Army thing?There's a big difference between "pull collective = go up" and understanding just how crazy helicopter aerodynamics are or how performance charts are made. TPS mostly taught me I don't understand it and to go ask someone who does.
I remember HT aero circa 2007 was pretty terrible. IIRC, they let some random O-4 with a BSAE rewrite the aero book, and it was a combination of (1) dumbing down the science to the point of being misleading, and (2) just being wrong.
No.So the problem is one needs some advanced engineering knowledge to really understand helicopter aerodynamics...?
Do the IPs of the Navy/Marine Corps/Air Force have it or is this an Army thing?
Just ask any Chinook pilot. They ALL wear t-shirts or own car stickers that depict a Chinook long-lining a Black Hawk. It's a rivalry thing. My response was always, "That shirt is only accurate when your helo is out of the hangar and doesn't have a red X in the status block."
What's Vy of a Chinook long-lining an H-60 ? (why doesn't platform show full embedded previews of posts on X?)
What is it about how it is designed to operate that makes the Army more by-the-book vs the others?No.
The Army is significantly more locked into institutional dogma than the Navy/Marines. If the book says so, it must be true. Whereas the Navy/Marines tends to breed a more questioning attitude.
This makes sense given how each service was designed to operate.
I think what he is getting at is that the army operates on doctrine. Pushed down from there everything from planning to TTPs (tactics, techniques, and procedures) reflect this. As individuals my experience (from the backseat perspective) is that army CWOs are very willing to flex the rules and try something difficult or different when needed, but typically they reflect their doctrine based training.What is it about how it is designed to operate that makes the Army more by-the-book vs the others?
USNTPS 😜Side note: If you can go to HAATS, DO IT!!!! It is fun, exciting and very educational. Plus, where else can you fly a stripped down 60A with T700-GE-401D engines? IGE hover at 6540' in those scalded dogs was less than 60% sometimes.
4,000fpm was my recollection. Those Blackhawks were awesome, even to a jet puke like like me.USNTPS 😜
I'm rusty, but I remember 3,000-fpm climbs ... at 0 KIAS.
This is essentially the Navy MDG for a max torque t/o or running t/o, except we don’t really test like you mentioned. However, if you have a student that doesn’t get you above 50 KIAS (maneuver completion standard), you feel the aircraft working harder than necessary.Restrict your Q to whatever setting you do to simulate rolling takeoff requirements. We use 10% below IGE hover power in the Army. Perform a rolling takeoff and accelerate to Vy once clear of the ground. Use whatever technique is required based on your desired profile. Note your altitude crossing the predesignated "obstacle".
I didn't say that. I said there is an unwillingness from many (but not all) of the IPs I'm having to deal with that won't think beyond what their gouge is saying when teaching the training manual.OMG Army IPs are for the most part dip shits!