Jump to content

Aircraft Super Thread Mk.VII


Recommended Posts

Just out of curiosity, why is this? Is it because of thrust vectoring engines or that the idea of variable geometry wings are too cumbersome and heavy to make it worthwhile?

Mainly, it's because advances in wing design, fly-by-wire, and high thrust engines made the need for VG wings unnecessary.

Link to comment
Share on other sites

The VG wings were also one of the significant nails in the F-14 service life's coffin, from what I recall. Besides all the stresses of carrier operations in general, the entire wing was mounted on a giant bearing, and all the parts within the wing support structure had to absorb stresses and flexing from varying directions. The entire problem of designing a variable geometry wing is kind of an aeroelastic nightmare.

VG wings still can and do give some great advantages to certain aircraft, but you pay a very high cost in maintenance and general wear and tear for those benefits, especially on a carrier-based aircraft.

Link to comment
Share on other sites

Just out of curiosity, why is this? Is it because of thrust vectoring engines or that the idea of variable geometry wings are too cumbersome and heavy to make it worthwhile?

I think that the general consensus is that advanced static wing shapes can match enough of the aerodynamic versatility of variable geometry wings without the massive penalties in weight, volume, and mechanical complexity.

Also - relevant to the F-14/F-23 hybrid concept - variable geometry is basically incompatible with stealth, because stealth shaping relies in part on limiting radar reflectivity to specific aspects. This is why on stealth aircraft you typically see that any shapes which aren't curved and blended have edges that align with (that is, are parallel to) a few specific angles. The leading edges of the wings match the leading edges of the tail, the edges of the intakes, the edges of the sawtooth cuts on any panels, etc. Having wings that change angle would mess this up in a big way.

Edited by Nekko Basara
Link to comment
Share on other sites

I'm not convinced passive stealth is effective enough for all of the aerodynamic compromises it entails. Not for a fighter/attacker.

VG wings are decidedly unnecessary because it's possible to use computers to give control surface dynamics that allow more swept-back profiles to have lower stall speeds and better manners at a wide range of speeds. That wasn't the case in 1972, so the F-14 made sense. There are still unique advantages to the VG wing, but they're often outweighed by the disadvantage of mass and maintenance. Like Chronocidal said, the wings rest on a massive bearing that has to withstand most of the lift load of the aircraft, as well as withstand the load of the wings' weight during landing, and all of the g-loading during flight. It can do that, for awhile, but it needs frequent maintenance. Non-carrier VG aircraft can sometimes get away with this- look at the Tornado and F-111. But the F-14 was a large carrier aircraft with them.

With that said, the ASF-14 would have been a significant redesign of the airframe, similar to the F/A-18E over the CF-18C/D. It would have involved changes to the wing profile and variable geometry design, as well as the replacement of traditional controls with fly-by-wire systems. While these wouldn't have negated the disadvantages of the VG wing, they would have helped.

Mostly I'm just sad they scrapped all of the tomcats. Shoulda left a few for aerial demonstrators.

Link to comment
Share on other sites

Weight. Weight weight weight. Always an issue, but even more so nowadays---weight affects range, weight affects payload. Both civil and military planes are going for more range and more payload with a high priority. Even flap and aileron designs are being simplified in the name of weight. Sure, triple-slotted fowler-flaps inherently give more drag and lift for landing---but they're heavier than single or double-slotted ones. Triples replaced with doubles, doubles replaced with singles... Pneumatic vs electric vs hydraulics systems, wires vs fiber optics---none are being chosen in the name of raw performance, but purely by "what weighs less for this section of the plane".

A swing-wing mechanism is heavy, regardless of any aerodynamic gains it offers. And almost everything nowadays is "yeah, it may be better---but it's heavier!". "Almost as good but lighter" is the big trend lately. Even 2D vs 3D vectoring---guess which is superior, but which one is almost as good but lighter?

Link to comment
Share on other sites

You can blame Iran for that one. The U.S. didn't want any spare parts to fall into their hands.

It's politics. Even if Iran somehow managed to get spare parts from USAF demonstrator squadron or USANG patrol squadrons, they wouldn't be able to wage any kind of meaningful combat against anyone with those planes. Otherwise, they might have actually tried at some point in the 42 years they've owned the planes.

Link to comment
Share on other sites

It's politics. Even if Iran somehow managed to get spare parts from USAF demonstrator squadron or USANG patrol squadrons, they wouldn't be able to wage any kind of meaningful combat against anyone with those planes. Otherwise, they might have actually tried at some point in the 42 years they've owned the planes.

Actually, I believe they did manage to acquire some spare parts back in the '80s, as part of the Iran-Contra scandal. Also, it is known that Iran looked to the Soviets at one point for technical assistance, with at least one Tomcat ending up in Russian hands.

Link to comment
Share on other sites

Even if Iran somehow managed to get spare parts from USAF demonstrator squadron or USANG patrol squadrons, they wouldn't be able to wage any kind of meaningful combat against anyone with those planes. Otherwise, they might have actually tried at some point in the 42 years they've owned the planes.

They did, actually.

http://en.wikipedia.org/wiki/Jalil_Zandi

http://en.wikipedia.org/wiki/Islamic_Republic_of_Iran_Air_Force

Link to comment
Share on other sites

Actually, I believe they did manage to acquire some spare parts back in the '80s, as part of the Iran-Contra scandal. Also, it is known that Iran looked to the Soviets at one point for technical assistance, with at least one Tomcat ending up in Russian hands.

Ofcourse in exchange, the Soviets got their hands on the AIM-54A which probably played a huge role in the development of the R-33 Amos used on the MiG-31.

I would have preferred to have seen all of the F-14A and B models retired in 06 and kept the remaining Ds in service until 2018 or so. Atleast until the messiah that is the F-35 enters Naval service. :rolleyes:

Edited by Shadow
Link to comment
Share on other sites

It's politics. Even if Iran somehow managed to get spare parts from USN demonstrator squadron or USNR squadrons, they wouldn't be able to wage any kind of meaningful combat against anyone with those planes. Otherwise, they might have actually tried at some point in the 42 years they've owned the planes.

Just a quick fix. :)

Link to comment
Share on other sites

I would like to thank the previous seven posters for slamming those dusty memoires out from the back of my cluttered mind, and making a boring day totally awesome.

In return, I offer this:

https://www.google.ca/search?hl=en-GB&site=imghp&tbm=isch&source=hp&biw=980&bih=1185&q=cobra+raven+jet&oq=cobra+raven+jet&gs_l=img.12...3894.17244.0.20526.25.19.4.2.2.0.689.5683.2j7j3j1j0j6.19.0....0...1c.1.55.img..10.15.1841.eZPLgdtIhZE

Link to comment
Share on other sites

Join the conversation

You can post now and register later. If you have an account, sign in now to post with your account.

Guest
Reply to this topic...

×   Pasted as rich text.   Paste as plain text instead

  Only 75 emoji are allowed.

×   Your link has been automatically embedded.   Display as a link instead

×   Your previous content has been restored.   Clear editor

×   You cannot paste images directly. Upload or insert images from URL.

×
×
  • Create New...