Air Combat Maneuvering Thread

Air Force Brat

Brigadier
Super Moderator
Yeah. That's exactly what thrust-vectoring does, nothing more.

Think about it. If thrust-vectoring really adds to maneuverability, everyone would retrofit thrust-vectoring nozzles to legacy planes. There would be no need to design new aircraft when MiG-21 could compete with F-22 just by replacing the engine nozzle. So, it goes without saying that thrust-vectoring isn't a game changer, and is now nothing more than marketing gimmick.

While you have absolutely convinced me that the Chinese are not interested in OVT, and LockMart did not incorporate it on the JSF, I'm a believer in your thesis really, and if I were to redesign the F-22 as a 5.5 gen, I WOULD NOT include OVT. I'm going to diverge slightly from your thinking by noting the Raptor does benefit from OVT, The Russians are including it as SOP on the T-50, and certain Flankers, such as the Indian SU-30MKI, and SU-35 will continue to use it as a means of increasing the "rate" of positive pitch transition when you speed and energy levels are high>

They Raptor does use OVT when super-sonic to reduce trim drag.

When OVT increases weight, maintenance, probably fuel burn, and reduces thrust slightly, and opens up the likely hood that the novice will mis-use it and squander his energy, you have me convinced in principal and in practice for the majority of scenarios.
 

Brumby

Major
When OVT increases weight, maintenance, probably fuel burn, and reduces thrust slightly, and opens up the likely hood that the novice will mis-use it and squander his energy, you have me convinced in principal and in practice for the majority of scenarios.

It should be noted that the genesis of this thread was whether super maneuverability would be sufficient to break a lock from a AAM. This conversation is very different from that of a dog fight situation when only guns are involved. I can't help saying that occasionally both get thrown into the mix that doesn't differentiate the two entirely different scenarios.
 

b787

Captain
A non-stealth aircraft encounters a lot of drag due to external stores. Stealth aircraft has no such issue. So, a non-stealth fighter is aerodynamically inferior to a similar sized and powered stealth aircraft.
which shape will have more drag
this
KjGbXvf.jpg


or this?
Hnb8E3v.jpg


airliners are known to be smooth to have the least drag
see their shapes

v73aGWL.jpg



Stealth demands large aircraft with internal weapons bays, making for large aircraft in frontal cross sections, add faceting and the aircraft will add drag, F-22 then needs thrust vectoring, same PAKFA,
good shape for stealth but it was called hopeless diamond
Lvnf34c.jpg
 

Air Force Brat

Brigadier
Super Moderator
What is super maneuverability?

A very fine post Mr. Brumby, and getting to the nub of the issue, quoting Dr.R. A. "Bob" Hoover, a consummate showman, but also a very, very savvy practioner of the fine art of flying the wing, and managing energy! In the early 60s attending my very first airshow at Sewart AFB on Armed Forces Day, I observed Mr Hoover taking off on very short cross runway taxi-way, in the Aero Commander Shrike to start his show, he then maneuvered that aircraft to enough altitude to roll it, loop it, then he would feather one engine and do it all engine out??? amazing, (the Shrike has a very tall effective rudder), which Dr. Hoover used very nicely to compensate for the assymetric thrust?? amazing, but not done yet, Dr. Hoover then Feathered the other engine and did it all again as a large heavy "glider". The loop, the rolls and then popping the gear and flaps and landing on the very short taxiway he had departed from.

Dr. Hoover was a test pilot in the early days of the jet age, he had a compressor stall testing the F-100, and lost hydraulics, his back was broken in crash, but as soon as he healed, he jumped back in the HUN, and was able to test and solve the many very dangerous issues with the HUN.

Anyway very nice post, pointing out the Mig-21, F-4s, 104s, Mig-25s etc, etc, very bad manners once departed, all the newer aircraft have very superior aerodynamics, and the FCS allows them to be very safe, and very pleasant to fly.
 

Air Force Brat

Brigadier
Super Moderator
Will do.

...and done.

Thank you Jeff, now I wanted to pick your brain a little about the past??? I know that your Dad, Lee Head was Lead Engineer on both the F-8 Crusader, which featured the variable incidence wing, in order to make bringing it aboard the boat both easier and safer, it was at the time a very high performance aircraft. At a later date he was the Lead Engineer on the A-7E Corsair II, which was known as the "gun fighter", I believe the A-7E which was designated as Attack, as opposed to F-8, which was designated as a fighter.

After seeing an A-7E on a pedestal, passing by it for many days when I worked down in the Edwardsville/Collinsville Illinois area, over a period of years, I became very "taken" with the airplane, it has a very "classic" design, and began to study it a little, and also took my bike and a friend who was also a biker, and road the bike trails to get up close and personal. I took a dozen or so photo's, from all the angles, and for the first time, this airplane has become my favorite fighter from the Vietnam era, followed by the old F-100, which I was disappointed to discover?? was no lady?

The A-7 in contrast was a pilots airplane, with an internal gun, and really put the Migs on notice, as it became the real "top-gun" of the Vietnam era, as a very real bonus, the A-7 had the best safety record of all those early jet aircraft, and Jeff, I believe it had a very long service life for a fighter, serving with several overseas Air Forces.

So as I have been contemplating all of these aircraft, looking back to the Korean War, even WWII, do you recall your Dad having any of those conversations that young men cling to, about design of the A-7 as opposed to the F-8? I mean they are so close in appearance, that many likely don't even recognize the difference, yet the A-7 was a "perfect airplane" for its time, and had such a "nice" personality, kind of like the sweet girl next door, that one day you wake up and think, WOW!
 

Jeff Head

General
Registered Member
...do you recall your Dad having any of those conversations that young men cling to, about design of the A-7 as opposed to the F-8? I mean they are so close in appearance, that many likely don't even recognize the difference, yet the A-7 was a "perfect airplane" for its time, and had such a "nice" personality, kind of like the sweet girl next door, that one day you wake up and think, WOW!
The F-8 was a super sonic naval fighter...in fact the Navy's first super sonic fighter.

The A-7 was a sub-sonic ground pounder that was designed specifically for the Vietnam War to carry a lot of weight for its size, and yet be able to tango with the Migs if they tried to interdict it in its support role.

The A-7 was also the first US Navy aircraft with a HUD.

So, the outward appearance in terms of the intake and the high wing are very similar to the F-8, and it maneuverability is also very good.

But make no mistake, the F-8 was designed to be able to get their soonest and then hunt and kill enemy fighters. The A-7 was designed to carry munitions and drop them very accurately on enemy positions, equipment, and people...while retaining very good air combat capabilities. It also had a very good loiter capability which the ground troops loved.

My Dad talked with me about all of these qualities when I was a teenager. And to be clear, my Dad was a lead Dynamics Engineer. He delved into the deep math of flutter, and aerodynamic issues associated with the aircraft he worked on. He started on the F-7 Cutlass, moved to the F-8, then the A-7, XC-142A, the XF-8U3, etc.

The XF-8U3 was probably the best straight fighter he worked on and it outperformed the F-4 in nearly every way. It was a Mach 2+ aircraft...but the Navy wanted two pilots and two engines, so it was not selected...even though for years its prototypes, which flew for NASA, would engage in and defeat US Navy F-4s in mock combat...until the practice was forbidded by the brass.

Hehehe...back then the pilots were just doing it...not scheduled, when they would fly from base for other exercises or getting some hours in.

I was born in 56, The F-8 had flown the year before for the first time and it was put in service the year after. But it served in the US military until 1976 (19 years), and then on with the French until 1999 (over 40 years). Over 1,200 of them were built.

The A-7 first flew in 1965 and went into service in 1967. It was built to replace the A-4. It was built for and used by the US Navy and the US Air Force (A-7D). I served in US Service until 1993 (26 years), and served with the Greeks unitl 2014 (over 40 years). Well over 1,500 of them were built.
 
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Jeff Head

General
Registered Member
Brat, I might add, that a number of his papers are quoted to this day, for example, his, "Philosophy of Design for Flutter," which he originally presented at the proceedings of the National Specialists Meeting on Dynamics and Aeroelasticity, in 1958.

He also presented regularly to the Symposium on Aeroelastic and Dynamic Modeling, back in the 60s and 70s.

Finally, he was involved in the founding of the American Institute of Aeronautics and Astronautics (AIAA) in 1963, though he did not work directly for them (he was a Vought man all the way, from 1948-1995).
 

Scratch

Captain
So my main focus in creating this thread was not to be obtuse or obnoxious, but gain a real world understanding, of number one the threat?, even highly maneuverable four gens "bit the dust" due to AAA and SAMS?? while only Scott Speicher's F-18 fell to a Mig 25? I am fairly certain that 5 gens will fair better against the AAM threat, but how much better??? I was under the impression that AAM will continue to try to make the "kill" until their fuel is exhausted or the LOCK ON is broken, or decoyed by chaff?

I understand it is supposed that the Raptor and other 5th gens will operate inside the threat bubble with relative impunity, so my question is basically can you defeat an AAM with Air Combat Maneuvering, and if so, will the same Metric allow you to defeat SAMs or AAA?

I would guess that, historicly, the fact that SAMs & AAA were widely available in conflicts and that their successfull employmet is perhaps a bit less training intensive, played a role in them having been such a threat.
As I said earlier, a highly maneuverable aircraft will have better chances to outmaneuver anything then a less maneuverable one. And under certain circumstances, especially at the outer performance envelope of a missile can quiet realisticly do that. In the heart of a SAM / AAM performance envelope, maneuvering alone will mostly not be enough. Especially if you're surprised by the attack, which can happen in the intense, information rich environmet of areal combat. Even more so with AAA, were reaction times are so short due to short ranges.
Now, indeed, with VLO features you can affored to not go contour flying to hide from enemy med-long range SAMs, thusly stying out of the AAA envelope.

Maneuvering, energy conservation while depleting the energy of the missile, is a part of the whole set of ACT - Air Combat Tactics - employed to "fly, flight and win". And, for all I know apply to air & surface launched missiles in similar ways. AAA is different I'd say. It's aggrssive jinks quickly avoiding the stream of bullets from short range.

On a different note, once you "outmaneuver" a missile, i.e. it "overshoots", it will necessarily loose it's lock, since for all I know, no AAM has a true look over the shoulder capability.
Modern AAMs, can be fired "over the shoulder" by quickly turning into a direction to were the pilot looks with his HMS. And then perform a "lock on after launch". I don't know if that capability also allows for a "re-lock". But as I said, I see geometry standing in the way here.

So just for reference.

The inner ring is an object turning at 525KTAS or M0.85 @20.000ft (-24°C in an ISA) and 9G.
The middle ring 924KTAS or M1.5 and 20G.
The outer ring 1540KTAS or M2.5 and 30G.
Btw, all will take between 15 to 18 sec to complete 360°

29fva7d.jpg


In a max performance turn the missile will likely loose speed shrinking the radius. Should the motor have burned out, that will happen really fast.
Of course that is vastly simplified. The turn circles will in reality be offset, changing the geometry and so on.

Finally, again I would like to say that I don't see TVC as generally unnecessary or useless. Especially for stuff like trimming the aircraft, to reduce trim drag or RCS increase through controll surface deflection I see a place for simple & light TVC mechanisms.
Or maybe for relieving aerodynamic controll surfaces under certain circumstances, mainly slow speed maneuvering, but still above stall.
 

Engineer

Major
which shape will have more drag
Which can supercruise? This
5ajr7m6.png


or this
78tpNe2.jpg


Here is hint: the one that can supercruise is also stealthy.

airliners are known to be smooth to have the least drag
Airliners can't dog fight, stealth fighter can.

Stealth demands large aircraft with internal weapons bays, making for large aircraft in frontal cross sections,
Non-stealth aircraft demand weapons to be carried externally, and each weapon requires a pylon, making for large frontal cross section. It is not uncommon for the external stores to have larger frontal cross sections than the aircraft itself. Here is an example:
qeyOf8W.jpg


The above is not the only problem for non-stealth aircraft. External stores are fully exposed, contributing a huge amount of surface area for parasitic drag. That's not all, at supersonic speed, each of those external stores produce its own shockwave resulting in significant wave drag. A non-stealth aircraft with external stores is clearly inferior.

add faceting and the aircraft will add drag,
F-22 can supercruise, while aircraft without faceting such as F-15, F-16 and F-18 cannot supercruise. So no, adding faceting does not equate to more drag.

F-22 then needs thrust vectoring, same PAKFA, good shape for stealth but it was called hopeless diamond
F-22 does better in dog fight without trust-vectoring than with thrust-vectoring. This has been well documented. F-22 also have better acceleration compared to most non-stealth aircraft. This too has been well documented.
 
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b787

Captain
Which can supercruise? This




Here is hint: the one that can supercruise is also stealthy.


Airliners can't dog fight, stealth fighter can.


Non-stealth aircraft demand weapons to be carried externally, and each weapon requires a pylon, making for large frontal cross section. It is not uncommon for the external stores to have larger frontal cross sections than the aircraft itself. Here is an example:


The above is not the only problem for non-stealth aircraft. External stores are fully exposed, contributing a huge amount of surface area for parasitic drag. That's not all, at supersonic speed, each of those external stores produce its own shockwave resulting in significant wave drag. A non-stealth aircraft with external stores is clearly inferior.


F-22 can supercruise, while aircraft without faceting such as F-15, F-16 and F-18 cannot supercruise. So no, adding faceting does not equate to more drag.


F-22 does better in dog fight without trust-vectoring than with thrust-vectoring. This has been well documented. F-22 also have better acceleration compared to most non-stealth aircraft. This too has been well documented.
Supercrusing is related to the engine, why? Eurofighter supercruises and the same is Su-35

A few details Stealthy jets have larger cross sections, thus then they can not jettison the internal weapons bays but you can a fuel tank or a missile, also you can have semi recessed weapons stations like Eurofighter
sokHr4b.jpg


This makes for a thinner fuselage


this is the ideal low drag shape, no matter how you try to spin it
ttCeqz3.jpg
 
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