Broncazonk
What the hell?
- Joined
- 29 August 2011
- Messages
- 134
- Reaction score
- 5
Let's analyze this.
1) A simple question was asked. "By the way, what kind of acceleration and turn performance would we get out of an F-35A and F-35C if the aircraft were area ruled?"
2) TaiidanTomcat responds, "You do realize that even with the reduced acceleration the F-35A is still faster transonically than than an F-16/F-18 in a similar load out/fuel carriage right?"
3) In the academic world, TT's response is known as a 'derailment.' When the derailment is unintentional, it's a sign of cognitive impairment. When the derailment is intentional, that's a sign of deception and evasion. F-35 supporters, Lockheed Martin, and con men are VERY good at using the derailment technique. Misdirection and technobabble are also stock in trades.
4) In this case, the derailment was not a good one: the F-16/F-18 are 40-year old designs, whose prototypes competed in a "lightweight fighter competition," and were not even designed to drop bombs. In effect, how bad can the F-35 be when LM and it's supporters rush to compare it with 40-year old light fighters?
5) For a fair comparison, let's go to Lackland AFB and take the F-105 gate guard down. As a categorical statement, the flight and mission kinematics of a vintage F-105 are better than a F-35 doing anything. The F-105 literally crushes the F-35, out performs it from A to Z all day long, AND the F-105 will not even blow up sitting on the tarmac in a rain storm. (In reply, we will get to hear another derailment: "What about stealth?" "What about the shiny new helmet and sensor fusion?"
How can a F-105 spank a F-35 like a circus monkey? Because the F-35 is not area ruled like every fighter and fighter-bomber since 1952 and the F-102. The below comes from here: http://www.flightglobal.com/blogs/the-dewline/2013/01/pentagon-lowers-f-35-performan.html
"The F-35's sustained turn rate requirements have been slashed as have its transonic acceleration requirements. Most impacted is the Navy's F-35C, which has had more than 43 seconds added to its Mach 0.8 to Mach 1.2 acceleration times. But this wasn't exactly unexpected, as almost exactly one year ago Lockheed's Tom Burbage told me this when I was still at Defense News:
"Based on the original spec, all three of the airplanes are challenged by that spec," said Tom Burbage, Lockheed's program manager for the F-35. "The cross-sectional area of the airplane with the internal weapons bays is quite a bit bigger than the airplanes we're replacing."
The sharp rise in wave drag at speeds between Mach 0.8 and Mach 1.2 is one of the most challenging areas for engineers to conquer. And the F-35's relatively large cross-sectional area means, that as a simple matter of physics, the jet can't quite match its predecessors.
"We're dealing with the laws of physics. You have an airplane that's a certain size, you have a wing that's a certain size, you have an engine that's a certain size, and that basically determines your acceleration characteristics," Burbage said. "I think the biggest question is: are the
acceleration characteristics of the airplane operationally suitable?"
Some of the backstory, according to an industry source is that originally the designers had intended the F-35 to be somewhat longer and more slender--in keeping with the principles of the Whitcomb area rule. Back then, the weapons bays were placed one behind the other--AMRAAMs in one bay, JDAMs in another. Apparently, the tail-end of the jet started to get heavy, and Lockheed had to change the configuration as a result--which is how we got the current weapons bays. They were kinda squished together--to use a technical description."
Unlike every other fighter and fighter bomber since 1952, our very own F-35, the most expensive weapons program in history, fails to incorporate the most important design feature since the swept wing.
:-[ ??? :-\
Let the derailment, misdirection and technobabble begin.
Bronc
1) A simple question was asked. "By the way, what kind of acceleration and turn performance would we get out of an F-35A and F-35C if the aircraft were area ruled?"
2) TaiidanTomcat responds, "You do realize that even with the reduced acceleration the F-35A is still faster transonically than than an F-16/F-18 in a similar load out/fuel carriage right?"
3) In the academic world, TT's response is known as a 'derailment.' When the derailment is unintentional, it's a sign of cognitive impairment. When the derailment is intentional, that's a sign of deception and evasion. F-35 supporters, Lockheed Martin, and con men are VERY good at using the derailment technique. Misdirection and technobabble are also stock in trades.
4) In this case, the derailment was not a good one: the F-16/F-18 are 40-year old designs, whose prototypes competed in a "lightweight fighter competition," and were not even designed to drop bombs. In effect, how bad can the F-35 be when LM and it's supporters rush to compare it with 40-year old light fighters?
5) For a fair comparison, let's go to Lackland AFB and take the F-105 gate guard down. As a categorical statement, the flight and mission kinematics of a vintage F-105 are better than a F-35 doing anything. The F-105 literally crushes the F-35, out performs it from A to Z all day long, AND the F-105 will not even blow up sitting on the tarmac in a rain storm. (In reply, we will get to hear another derailment: "What about stealth?" "What about the shiny new helmet and sensor fusion?"
How can a F-105 spank a F-35 like a circus monkey? Because the F-35 is not area ruled like every fighter and fighter-bomber since 1952 and the F-102. The below comes from here: http://www.flightglobal.com/blogs/the-dewline/2013/01/pentagon-lowers-f-35-performan.html
"The F-35's sustained turn rate requirements have been slashed as have its transonic acceleration requirements. Most impacted is the Navy's F-35C, which has had more than 43 seconds added to its Mach 0.8 to Mach 1.2 acceleration times. But this wasn't exactly unexpected, as almost exactly one year ago Lockheed's Tom Burbage told me this when I was still at Defense News:
"Based on the original spec, all three of the airplanes are challenged by that spec," said Tom Burbage, Lockheed's program manager for the F-35. "The cross-sectional area of the airplane with the internal weapons bays is quite a bit bigger than the airplanes we're replacing."
The sharp rise in wave drag at speeds between Mach 0.8 and Mach 1.2 is one of the most challenging areas for engineers to conquer. And the F-35's relatively large cross-sectional area means, that as a simple matter of physics, the jet can't quite match its predecessors.
"We're dealing with the laws of physics. You have an airplane that's a certain size, you have a wing that's a certain size, you have an engine that's a certain size, and that basically determines your acceleration characteristics," Burbage said. "I think the biggest question is: are the
acceleration characteristics of the airplane operationally suitable?"
Some of the backstory, according to an industry source is that originally the designers had intended the F-35 to be somewhat longer and more slender--in keeping with the principles of the Whitcomb area rule. Back then, the weapons bays were placed one behind the other--AMRAAMs in one bay, JDAMs in another. Apparently, the tail-end of the jet started to get heavy, and Lockheed had to change the configuration as a result--which is how we got the current weapons bays. They were kinda squished together--to use a technical description."
Unlike every other fighter and fighter bomber since 1952, our very own F-35, the most expensive weapons program in history, fails to incorporate the most important design feature since the swept wing.
Let the derailment, misdirection and technobabble begin.
Bronc