Just quoting from the link above, seems to be a rip from the same book as well. Do not know what are you talking about, what doesnt fit my argument? Please send a scan of that page where he explains that.
Don’t quote something if you don’t have the reference or understand the context. You quoted the book, now read the rest for yourself. Or get one of your pilot friends to explain it to you. I’ve already tried but you don’t want my ‘opinion’.
Anyway, I have the impression from your reply that you`re saying that Boyd became famous in the USAF because of “winning a bet only”, that he was a kind of jerk?
Quite the opposite. Boyd was one of the most influential tacticians and theorists of his or any other time, particularly for those of us who were his contemporaries.
Your ‘cut and paste’ quote is very close to the text in Coram’s book. If you took it from there, then you must have read the author’s explanation of Boyd’s maneuver. Could it be that you failed to mention that because that explanation doesn’t fit your argument?
just for a start, USAF Col John Boyd, one of famous combat pilots ever.
You have misunderstood what Boyd was doing.
He was not demonstrating a combat maneuver.
He was winning a bet. Boyd assumed that the opposing pilot would not be prepared for or probably even aware of what was going to happen. The surprised pilot overshot allowing Boyd to get into his six. Whether or not a “guns guns’ situation followed that is arguable.
At that time, fighter pilots were generally unaware of high AOA maneuvers…earlier fighters typically didn’t do maneuvers such as this.
Boyd’s maneuver was a one trick pony. It only worked once on an unsuspecting pilot. The counter is a simple yo-yo off into the vertical…a maneuver that Boyd would not be able to follow due to his low energy state.
I realize that little of this is going to convince those of you who want to believe this silliness. If you want to continue to be gobsmacked by airshow maneuvers designed to astound an uninformed audience, please have at it.
As i keep searching for any clue to your request, perhaps you could endulge me with my request?
I’m waiting for the original poster to provide those details.
Did you have a request?
I didn’t mention Cobra…..
I was talking about all the other maneouvres – falling leaf, backflips, high-afpha, relaxed stability, post-stall maneouvering etc etc.
The F-22 display now includes some of these – and it is suddenly the thing to have in your arsenal.
That’s all I’m saying….
Ken
Can you provide a reference where western pilots said that any of those maneuvers were legitimate combat maneuvers?
I also find it amusing that all those western pilots and press dismissed the Flankers manouvreability as just ‘airshow stunts’…….
Yet when the F-22 comes along (years later) and does the same thing – they are suddenly ‘legitimate combat maneouvres’.
Can you provide a reference that shows ‘western pilots’ describing this ‘cobra’ as a ‘legitimate combat maneuver’?
In the History Channel program “MiG Killers of the Midway” two F-4 pilot describes how they used a post-stall maneuver to get a MiG off his tail and, get the MiG in front of the F-4.
I don’t think so.
Speed brakes aren’t used in a ‘post-stall maneuver’. What the USN pilot described was a rapid pull into the vertical using the speed brakes to slow his speed. A rapid pull up is not a ‘post-stall’ maneuver. It is simply an unexpected and rapid change in the aircraft direction that is designed to surprise the opponent.
Kinda like what Maverick did in the movie.
We tended to avoid post-stall maneuvers in the F-4…bad things were often the result.
Here are some interesting TAC evaluation:
“ADC Evaluated the F-106 and found its radar capable of acquisition and that radar snap-up attack with all aspect armament should be used to exploit MiG-21 lack of fire control. The F-106 could use better acceleration to get beyond MiG-21 speed limit if not in an advantageous position. The F-106 should use missiles then close in to gun kill position. It was the consensus of ADC that the U.S. needed to expedite procurement of cannon for F-106, and replacement of its canopy bar with clear pane. It was concluded that the F-106 shouldn’t attempt a slow speed turning contest?? and should keep its speed from 400-450 KCAS during patrol and engagement.
The TAC evaluation of the F-5A revealed that within performance limits, the F-5 had considerable capability to engage the MiG-21. The F-5 had performance advantage below 15,000 feet, however the MiG-21 had higher Mach capability at higher altitude. Overall turn comparison was about equal and level acceleration was equal in military power, MiG-21 had a slight advantage in afterburner. They had comparable fire control systems. The F-5 controlled the tactical engagement effectively and if defensive separation was necessary, the F-5 could exceed the MiG-21 airspeed limit below 15,000 ft. The F-5 could closely simulate the MiG-21 up to Mach 1.2 for combat crew training in ACM, dissimilar aircraft engagements.
The USN evaluation of the F-8E found that the MiG-21 could out turn the F-8 in a close-in fight.Zoom performance was comparable below 25,000 ft and on station time was also comparable. Large size and prominent smoke trail was a disadvantage. The F-8E was capable of exceeding the MiG-21 speed limit at low altitude. Acceleration performance was better than the MiG-21 at low and medium altitudes below 1.2 Mach“
I’m not an expert, but even I can find some parts difficult to understand…how about you ?
Were those parts the ones in italics?
I have to wonder what model of the MiG-21 was used for comparison.
Dear Alfakilo, i took the liberty of transforming the pdf in pictures, so that you can see them without having to go through rapidshare.
http://img94.imageshack.us/img94/3299/39545754.png
Excellent! Thank you very much for taking the time!
These charts are different from the ones that I have for the F-104G…however the differences are minor.
The total sight setting includes the mil values in these tables plus the zero sight line (ZSL) angle of attack value. The ZSL is missing from these F-104C charts, consequently the sight settings from these charts are incomplete.
Mil settings for the Mk-83 will be quite similar to those for the M-117…for example, for a 45 degree release from 5000′ and 400KIAS, no more than 5 mils or so…relatively insignificant. Pilot error and wind effects produce larger differences than this.
AK, you can download it from rapidshare as a free user, presuming the file isn’t massive it shouldn’t take that long.
Thanks…I’ve tried several times but the download isn’t coming through on my end.
For the original question…use of weapons release tables is very specific…entry parameters include type of aircraft and weapon, aircraft configuration (flap position, for example), dive angle, release altitude and speed, number of weapons to be released, etc.
Something like this one https://rapidshare.com/files/345822242/dive_bombing.pdf but for Mk83 and rockets??
Diego
Sorry…I don’t have rapidshare.
I am looking for the Mk83 table and the rockets too for the F104G ( well I guess that all zipper versions have the same tables…)
Diego
I need more info. The ballistics tables cover a wide range of release speeds and altitudes.
Thank you!
I have been investigating. Data related with the aircraft seems to be named horizontal and vertical PARALLAX corrections. They are caused by the distance from the bomb to the pilot`s eyes. Now I am trying to get some numbers for the zipper…
Diego
What numbers do you need for the F-104?
I have a doubt about old sights. They calculate the depresion in mils. But, are the mils a universal unit of measure?
Imagine that I have the sight depresion in mils for a F4C, dropping a MK82 at a 30º dive and 450 knots over a target a 0 ft MSL, and a setting for the sight of 121 mils; could I use the same settings in mils for another plane, like a F104 or a F105? ( i guess than the rest of the serttings are the same, because a Mk82 is always a Mk82, and it once dropped it flies always the same pattern)
Thank you!
A ‘mil’ is a universal unit of measurement…it’s a measurement of angle, and about 17 mils equal one degree.
A ‘mil setting’, however, is not going to be the same for different aircraft using the same release parameters and weapon. The settings may be reasonably close, but that is strictly coincidental as the computation of that angle also takes into account factors unique to the design of the individual aircraft. These other factors include line of sight relationships as measured from both the cockpit and the location of the weapon when mounted on the aircraft.
In many cases, we are still flying the aircraft of yesteryear!!