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Fast, On-Speed, Slow: A Common Language for Aircraft Control

@Vac - hey brother, getting off of the contentious stuff for a bit..... I have a question for you. What "speed" is your ON SPEED AOA setting calibrated for? Like for instance my Garmin G3X is calibrated based on Stall speed. So for instance The
  1. Minimum Visible AOA (1.5 xVs)): The bottom green band on the AOA indicator, typically flown around 1.5 times the stall speed.
  2. Caution Alert AOA (1.1 x Vs): The start of the yellow chevron, corresponding to roughly 1.1 times the stall speed.
  3. Stall Warning AOA (1.0 x Vs)): The upper red chevron, corresponding to a power-off stall speed.
So what speed is the Green Donut telling me?? Is it best AOA for the best Approach speed? Is that Vx, Vy or something else.

My real question is in an engine out situation is: Which of the AOA indications do I fly? Does the 1.5x Vs = Best Glide? Because at least for me, best glide in my RV-8 flaps up (~ 80-85 KIAS) tends to be faster than my normal approach speed of 70-75KIAS full flaps. So how do I translate best glide to an AOA?
NOTSO, I have mine set for 1.25-1.35 Vs (for each flap setting). Gives me a speed band about 5 knots wide. My IAS in the -4 is in MPH.
 
That's a very interesting document, making a lot of good points.

I think the description of the three aerodynamic states on p10 makes some assumptions about power availability that are only true in non-manoeuvring flight. In manoeuvring flight positive excess power can become unavailable in any of the three states, as shown in figure 4, which doesn't entirely match the description on p10.

Therefore, the slow/onspeed/fast aerodynamic state indicator is an essential part of your proposed operational method, but needs to be paired with an energy state indicator (a P_s gauge for example) to provide full information on which the pilot can make decisions (to know where the aircraft is on figure 4). This might be particularly relevant for general aviation aircraft with low thrust/weight ratios and correspondingly small power envelopes.

In general, I think your ideas are excellent, but I expect that standardisation of both instrumentation and instruction methods might be a fairly high barrier. I'd say that self-calibrating instrumentation systems are one of the keys to the approach.
Dan, thanks for taking the time to read the paper and for the thoughtful comments. I think we're actually saying the same thing. The intent isn't to suggest that the on-speed condition guarantees positive excess power. Rather, on-speed defines the aerodynamic state of the wing, while available power determines whether that condition can be sustained. That's what Figure 4 was intended to illustrate—the same reference AOA can correspond to sustained flight, deceleration, descent, or some combination thereof depending on the available power. If that wasn't as clear as it could have been, I'll revisit the wording in the next revision. Thanks for pointing it out.

Cheers,

Vac
 
I don't at all understand what you're trying to say here. Are you saying that you would fly the entire impossible turn at 80 kts regardless of the bank angle needed to get back to the runway/field? Or that you would never attempt the turn back in the first place?

Oh, nevermind. You answered it already. Don't take this the wrong way, but remind me never to fly with you as a pax.
I always scare people on the passenger brief when we talk about emergency canopy opening, getting clear of the aircraft, safety belt operation…what it might be like if we can’t reach one of the three bailout field choices…

But when we are done, they always thank me for the commitment to safety, planning, briefing etc…

In 35 years of flying RV’s never yet had to use one of those fields, thus far…but still good to have that plan.
 
Dan, thanks for taking the time to read the paper and for the thoughtful comments. I think we're actually saying the same thing. The intent isn't to suggest that the on-speed condition guarantees positive excess power. Rather, on-speed defines the aerodynamic state of the wing, while available power determines whether that condition can be sustained. That's what Figure 4 was intended to illustrate—the same reference AOA can correspond to sustained flight, deceleration, descent, or some combination thereof depending on the available power. If that wasn't as clear as it could have been, I'll revisit the wording in the next revision. Thanks for pointing it out.

Cheers,

Vac
I wish I could say I understand your whole paper…but I’m afraid it’s gonna take a few re-reads and some study…it is fascinating that this whole other realm Exists and I know almost nothing about it…you guys understand things us mere mortals don’t contemplate.

Pretty awesome.

The ability to see this technology get implemented into a practical safety solution into GA aircraft , alone is well worth watching…thank you!!!
 
I think it didn’t occur to me that you use AoA in lieu of airspeed entirely…I somehow kept thinking it was in addition to.
Not in lieu of ENTIRELY in ALL situations. We're not rotating, taking off, climbing out, and cruising using AOA - although you could if you had an AOA number to fly. As I said before, we used AOA Ref numbers in the Eagle for many phases of flight. But keep in mind that these basic AOA systems we're talking about in GA planes are not really set up to give you much info other than down at the bottom end approaching or at critical AOA. So when I and other say AOA replaces speed - we mean down at approach to stall regimes. Anything outside of that is airspeed. Essentially, once I make the base turn to final until the flare - AOA is king.
 
Flysto.net has a nice way to view your approach speed and IAS on touchdown which I review almost every flight.

Screenshot 2026-07-13 073130.png
 
@justa6ereh @Notso

I didn’t find the whole conversation so I’m making a presumption regarding 120 kts, was this someone’s target for a ground effect acceleration to zoom climb? A ground effect acceleration to climb at 120? An accelerating climb to 120 and sustain 120? Generally I am presuming this is a left of bang consideration.

I do think there is value in 120 as it is better airflow and nicer to the engine for cooling. Could 120 help in a sense of avoiding an engine out scenario in the first place? Suppose a mechanic and a mechanical engineer would be better to address this. I’m neither.
I didn't read his post as 120kts in the climb out on a normal takeoff (which I do for cooling as well), but rather he is going to pitch for 120 upon the motor quitting and look for a tree or fence to crash into. Maybe I read him wrong....
 
NOTSO, I have mine set for 1.25-1.35 Vs (for each flap setting). Gives me a speed band about 5 knots wide. My IAS in the -4 is in MPH.
Interesting..... So how does that equate to flying a "best glide AOA" if you had to do the 180 back to the runway or even a straight ahead engine out landing?

i.e. are you still flying the on-speed "donut" when engine out? Or something different?
 
I didn't read his post as 120kts in the climb out on a normal takeoff (which I do for cooling as well), but rather he is going to pitch for 120 upon the motor quitting and look for a tree or fence to crash into. Maybe I read him wrong....
No…I takeoff, accelerate to 120 to clear the trees usually with about 400ft clearance to the trees…about 3/4 of a mile off the end of our strip, which is surrounded by trees, wires etc…is a large open field…in an engine failure scenario right off the end of the strip which would require a 15 degree turn to the right…and then some form of abbreviated pattern…

The goal, would be to bleed airspeed from 120 mph ias over the trees and trade the energy available from the altitude to coast on down to the 80mph mark, then determine best course of action to attempt to fit in on the open, large farm field…

I have never actually shut the engine down, to see what the actual affects of the spinning, flat pitch blended airfoil Hartzell affords in terms of drag, but my gut feeling is….it’s a helluva lot of drag.

If this area is where AoA shines…then please educate me as to how so…the comment that you use it in lieu of airspeed boggles me…since Vacs video clearly shows an airspeed indicator, so I’m confused as to when to make the switch.

Steve
 
Not in lieu of ENTIRELY in ALL situations. We're not rotating, taking off, climbing out, and cruising using AOA - although you could if you had an AOA number to fly. As I said before, we used AOA Ref numbers in the Eagle for many phases of flight. But keep in mind that these basic AOA systems we're talking about in GA planes are not really set up to give you much info other than down at the bottom end approaching or at critical AOA. So when I and other say AOA replaces speed - we mean down at approach to stall regimes. Anything outside of that is airspeed. Essentially, once I make the base turn to final until the flare - AOA is king.

Actually, with pressure diff and also APM but not vane or stagnation pt we can and I do, believe Vac does as well, takeoff on AOA. Climb out is better figured with AOA than speeds though with the jets you get compressibility and Mach so there is a transition… both Vspeeds Vx and Vy are impacted altitude as is AOA but AOA still compensates for all the other stuff so really speeds are only needed for the high end don’t rip your plane apart sort of stuff. AOA is better for best rate and best angle and with pressure diff for rotation.

Note twins have alternate concerns and generally need to watch speed.
 
Interesting..... So how does that equate to flying a "best glide AOA" if you had to do the 180 back to the runway or even a straight ahead engine out landing?

i.e. are you still flying the on-speed "donut" when engine out? Or something different?

Yes, onspeed AOA as you’re predominantly doing the turn and aren’t really driving out straight anywhere
 
I'm enjoying the discussion and do truly appreciate everyone's thoughts.

RNB, it's been a pleasure watching your perspective evolve. Thank you :cool:

Absolutely great…GREAT example…of how not to do it. You have far more experience than I…and obviously are passionate about this and again, I applaud the sentiment. That demonstration done again 80ias would never occur. So training to stick to a conservative pattern speed and only bleed the speed over the fence, solves this problem. Having flown 4’s for the better part of 35 years, as well as 6, rocket etc…there is only one place I go, which is 800 feet, where a speed below 80 is required…we aren’t trying for 2 wires here…

VAC…I think if this could incorporate into an actual HUD type plate on the canopy…something you can see through…I have no idea how that works, but my wife’s Bentley does it…and it’s rather awesome.

And I agree with your assertion on aerobatics and all that…it’s still super cool you are doing something to make life better for an area that needs an update. While guys like me are gonna be a touch sell…time and video’s like that will help drag us old farts into new ways of thinking,
Actually, I'd respectfully point out we are trying for a 3 wire every time we land--I always want to control my touchdown point with precision, and I like having perfect kinetic energy for touchdown. Do I always manage to achieve that? Nope. The AOA tone is just one more tool that helps me get there most of the time. As far as the asymmetric departure, you are absolutely correct that won't occur with a properly coordinated rudder. I start the demo at normal pattern speed and configuration (flaps 40), and the accelerated stall occurs at about 67 MIAS. I can certainly force the airplane to depart at 80+ knots indicated. I can depart controlled flight at any airspeed. I don't demonstrate that because I want the airplane to remain serviceable :). High speed, asymmetric departures can cause airframe damage (ask me how I know that!) unless the airframe is built to be bullet-proof (e.g., GameBird or something similar). RV's have a 2 g limit with flaps deployed (not published, but Van designed to normal FAR23 requirements, so simply an assumption on my part). In this case, I'm pulling about 1.4 g's when I depart. None of us has a butt calibrated finely enough to tell the difference between 1.2 and 1.4 g's. And again--I really appreciate the conversation and the thought you've put into this!

We've spent a lot of time talking about AOA systems, displays, probes, calibration, audio cueing and even engine failure on takeoff (another pet project is doing the flight test for the TLAR app designed to help with pilot planning and decision making) . Those are all interesting topics, but they're implementation details. The paper is intentionally system agnostic. Its central premise is much simpler: would general aviation benefit from adopting a common operational language for aircraft control? Fast, On-Speed, and Slow are intended to describe the aerodynamic state of the wing, regardless of whether that information comes from airspeed, an AOA system, progressive audio, or some future technology.

v/r,

Vac
 
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Yes, onspeed AOA as you’re predominantly doing the turn and aren’t really driving out straight anywhere

But for those without AOA do not read that as Vref. Ok in an RV but some platforms have a no flap Vref trap in that no flap Vref may be less than 1.3 Vs. Vref in lieu is not ok.
 
No…I takeoff, accelerate to 120 to clear the trees usually with about 400ft clearance to the trees…about 3/4 of a mile off the end of our strip, which is surrounded by trees, wires etc…is a large open field…in an engine failure scenario right off the end of the strip which would require a 15 degree turn to the right…and then some form of abbreviated pattern…

The goal, would be to bleed airspeed from 120 mph ias over the trees and trade the energy available from the altitude to coast on down to the 80mph mark, then determine best course of action to attempt to fit in on the open, large farm field…

I have never actually shut the engine down, to see what the actual affects of the spinning, flat pitch blended airfoil Hartzell affords in terms of drag, but my gut feeling is….it’s a helluva lot of drag.

If this area is where AoA shines…then please educate me as to how so…the comment that you use it in lieu of airspeed boggles me…since Vacs video clearly shows an airspeed indicator, so I’m confused as to when to make the switch.

Steve

Vac shows airspeed for comparison purposes; he also has videos with airspeed completely blanked out. There is a bit of combining Aero for Naval Aviators here with the Glider books. Min power required is an AOA not a speed and is synonymous with max glide time AOA, again an AOA not a speed, consider how you optimize your gliding turn most degrees of turn for least altitude lost.
 
No…I takeoff, accelerate to 120 to clear the trees usually with about 400ft clearance to the trees…about 3/4 of a mile off the end of our strip, which is surrounded by trees, wires etc…is a large open field…in an engine failure scenario right off the end of the strip which would require a 15 degree turn to the right…and then some form of abbreviated pattern…

The goal, would be to bleed airspeed from 120 mph ias over the trees and trade the energy available from the altitude to coast on down to the 80mph mark, then determine best course of action to attempt to fit in on the open, large farm field…

I have never actually shut the engine down, to see what the actual affects of the spinning, flat pitch blended airfoil Hartzell affords in terms of drag, but my gut feeling is….it’s a helluva lot of drag.

If this area is where AoA shines…then please educate me as to how so…the comment that you use it in lieu of airspeed boggles me…since Vacs video clearly shows an airspeed indicator, so I’m confused as to when to make the switch.

Steve
Steve, I'm flying the same system as Vac has in his plane — I'm not a pro here but I'll venture an answer.

The OnSpeed system is audio-based (in addition to that display in the video), and the tones tell you where your are on the range from roughly Vy all the way to stall. If you engine dies on initial climb, you need to

- push the nose down, since your AoA's going to start climbing quick and you need to stop that from happening
- get into a 45 degree turn, so that you have a tight enough turn to get pointed back at the runway
- you'll be squeezed between your unexpected loss of power slowing you down, and the tight turn raising your stall speed...

So the familiar approach-speed reference sets a too-slow trap. If you fly the "OnSpeed" AoA (the solid tone), you can stay safely away from stall as you do this max-performance maneuver and your airspeed's all over the place.

The other nice thing about the wide range of AoA cueing is that you actually can fly AoA on rotation + takeoff. The tones start beeping at L/D max, which is ~roughly the same as Vy. And a solid tone ~roughly matches Vx.

So I fly the nosewheel off in my 10, hold the nose down until solid tone, then pitch for the start of the tone band. As the plane speeds up this has me increasing my pitch, and I can turn crosswind fairly aggressively for pattern work (with no one else around!), knowing that I am at constant AoA.

I glance at the airspeed as a "cross check" and it's nice to see that, yes, when I have less fuel on board, the speed's a bit lower than normal. Same thing on downwind — give a glance at the AoA to make sure the tones are roughly matching my airspeed expectation, then I don't really look at the panel again, other than a glance on final.

Anyway hopefully that's helpful, as some reflections from an AoA-newbie on how I really am flying tones + AoA.
 
@justa6ereh @Vac

Examples of how not to do it are the best form of instruction. Behavioral economics, humans tend to avoid risk more than seek reward but we’re not good at appreciating or assessing risk. We learn to avoid bad much quicker and more readily with longer retention than how to do well. Further, often there is no best practice, rather many options of good practice, so teaching best practice becomes bad practice as such limits students and fails to allow them to adapt with context.
 
No…I takeoff, accelerate to 120 to clear the trees usually with about 400ft clearance to the trees…about 3/4 of a mile off the end of our strip, which is surrounded by trees, wires etc…is a large open field…in an engine failure scenario right off the end of the strip which would require a 15 degree turn to the right…and then some form of abbreviated pattern…

The goal, would be to bleed airspeed from 120 mph ias over the trees and trade the energy available from the altitude to coast on down to the 80mph mark, then determine best course of action to attempt to fit in on the open, large farm field…

I have never actually shut the engine down, to see what the actual affects of the spinning, flat pitch blended airfoil Hartzell affords in terms of drag, but my gut feeling is….it’s a helluva lot of drag.

If this area is where AoA shines…then please educate me as to how so…the comment that you use it in lieu of airspeed boggles me…since Vacs video clearly shows an airspeed indicator, so I’m confused as to when to make the switch.

Steve
Ok, I read that wrong then, sorry.

One thing that occurs to me is your "emergency gameplan" seems like its only specifically tailored to your home strip. That's great if you never go anywhere else. And its also fine if you're always around farm fields with lots of open space. I always plan an "oh sh*t return gameplan to where I am currently - taking winds, off field environment (urban vs Rural) and any obstructions into account. For instance, if there are any crosswinds - all things being equal I would turn into the wind to minimize both my turn radius if I were trying to get back to the airfield and it reduces your GS for when you're going to land in a corn field somewhere.

I know of some people who shut down their engine to "test" actual glide. That literally gives me the Heebies just thinking about it. The one thing you can do to maximize your glide with a CS prop is to check and adjust if necessary your Static pitch stop settings. If its set wrong and the prop loses power and oil pressure - it could slam to a really fine/flat blade setting (unless you have an aerobatic prop) and act like a speed brake.

Sorry, but I digress. Not trying to get off topic here.
 
Steve, I'm flying the same system as Vac has in his plane — I'm not a pro here but I'll venture an answer.

The OnSpeed system is audio-based (in addition to that display in the video), and the tones tell you where your are on the range from roughly Vy all the way to stall. If you engine dies on initial climb, you need to

- push the nose down, since your AoA's going to start climbing quick and you need to stop that from happening
- get into a 45 degree turn, so that you have a tight enough turn to get pointed back at the runway
- you'll be squeezed between your unexpected loss of power slowing you down, and the tight turn raising your stall speed...

So the familiar approach-speed reference sets a too-slow trap. If you fly the "OnSpeed" AoA (the solid tone), you can stay safely away from stall as you do this max-performance maneuver and your airspeed's all over the place.

The other nice thing about the wide range of AoA cueing is that you actually can fly AoA on rotation + takeoff. The tones start beeping at L/D max, which is ~roughly the same as Vy. And a solid tone ~roughly matches Vx.

So I fly the nosewheel off in my 10, hold the nose down until solid tone, then pitch for the start of the tone band. As the plane speeds up this has me increasing my pitch, and I can turn crosswind fairly aggressively for pattern work (with no one else around!), knowing that I am at constant AoA.

I glance at the airspeed as a "cross check" and it's nice to see that, yes, when I have less fuel on board, the speed's a bit lower than normal. Same thing on downwind — give a glance at the AoA to make sure the tones are roughly matching my airspeed expectation, then I don't really look at the panel again, other than a glance on final.

Anyway hopefully that's helpful, as some reflections from an AoA-newbie on how I really am flying tones + AoA.
As before, I am a fan of AOA I. One form or another but again I will say that relying on one piece of info is an insidious trap that will be sprung when that piece of information, in this case, is not available.

This applies to really any of the available tools whether it is AOA, altitude callouts, or a HUD. It is exceptionally easy to get so reliant on one of these tools that when it is suddenly unavailable, pilots have forgotten how to use the other tools available, ie airspeed, vertical speed, etc.

At work, we call these guys HUD cripples; without the HUD, they appear to lose a substantial amount of flying skills…
 
Ok, I read that wrong then, sorry.

One thing that occurs to me is your "emergency gameplan" seems like its only specifically tailored to your home strip. That's great if you never go anywhere else. And its also fine if you're always around farm fields with lots of open space. I always plan an "oh sh*t return gameplan to where I am currently - taking winds, off field environment (urban vs Rural) and any obstructions into account. For instance, if there are any crosswinds - all things being equal I would turn into the wind to minimize both my turn radius if I were trying to get back to the airfield and it reduces your GS for when you're going to land in a corn field somewhere.

I know of some people who shut down their engine to "test" actual glide. That literally gives me the Heebies just thinking about it. The one thing you can do to maximize your glide with a CS prop is to check and adjust if necessary your Static pitch stop settings. If its set wrong and the prop loses power and oil pressure - it could slam to a really fine/flat blade setting (unless you have an aerobatic prop) and act like a speed brake.

Sorry, but I digress. Not trying to get off topic here.
Yep…guilty, I hardly ever go anywhere other than buzzing around like a dork. Tomorrow I’m running to the other side of the state and it always makes me study the day before…and really think through the good/great/bad/sucks scenarios before I go. So DEFINITELY a homebody. Probably on a ratio approaching 50:1 home vs. elsewhere’s.

The AoA discussion is very similar to our final glide computer in the sailplanes and I have used that for a long time.

Changing the way we think and challenging the instructional norms are very noble aspirations and I appreciate the willingness to field the questions, challenge the conceptual notions for utilization and honestly…put yourselves out there and defend your positions…

I think what you are doing is pretty awesome.

Steve
 
As before, I am a fan of AOA I. One form or another but again I will say that relying on one piece of info is an insidious trap that will be sprung when that piece of information, in this case, is not available.

This applies to really any of the available tools whether it is AOA, altitude callouts, or a HUD. It is exceptionally easy to get so reliant on one of these tools that when it is suddenly unavailable, pilots have forgotten how to use the other tools available, ie airspeed, vertical speed, etc.

At work, we call these guys HUD cripples; without the HUD, they appear to lose a substantial amount of flying skills…
To this end…I gave a ride to a young guy with an instrument rating who jumped into my 6, settled in and upon noticing the lack of a gps device legitimately asked how we were going to find our way to Yakima from the Seattle area…

So…I’m sure there’s happy mediums with lots of this.

Ps…my new Garmin Aera 660 is amazing and simple. The magenta line is slightly addicting.

Steve
 
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